United States of America as represented by the Secretary of the Air Force (USA)
Inventor
Rogers, Travis
Abstract
A laser guided alignment system for facilitating installation of an aircraft engine into an engine bay of an aircraft is disclosed herein. A laser assembly may be attached to one or more rails of an engine trailer or rails of an engine bay. A laser receiving assembly may be attached to one or more of the rails of the engine bay or the rails of the trailer. The engine can be moved from the trailer to the engine bay when the laser guide assembly is aligned on target.
B64F 5/10 - Manufacturing or assembling aircraft, e.g. jigs therefor
G01B 11/27 - Measuring arrangements characterised by the use of optical techniques for measuring angles or tapersMeasuring arrangements characterised by the use of optical techniques for testing the alignment of axes for testing the alignment of axes
United States of America as represented by the Secretary of the Air Force (USA)
Inventor
Mcclearn, Michael
Huff, Riley
Hoke, John
Fotia, Matthew
Abstract
A rotating detonation combustor (RDC) and an associated system is disclosed herein. The RDC can be operably coupled with a vehicle to provide additional power capability over the primary motive power source. The RDC can be operated on demand to provide power to a turbine connected to an electrical power generator in some forms. The RDC can be used in stationary systems as well as moving vehicle systems.
F02C 5/02 - Gas-turbine plants characterised by the working fluid being generated by intermittent combustion characterised by the arrangement of the combustion chamber in the plant
F02C 6/00 - Plural gas-turbine plantsCombinations of gas-turbine plants with other apparatusAdaptations of gas-turbine plants for special use
F02C 7/32 - Arrangement, mounting, or driving, of auxiliaries
United States of America as represented by the Secretary of the Air Force (USA)
Inventor
Ahern, Austin
Dittman, Eric
Anderson, Michael
Cabigas, Iii, Acierto
Barnes, Ashton
Weiler, Elliott
Rochester, David
Abstract
A system for asset inventory and resupply for supplying individuals in remote locations is disclosed. The individuals may be people and/or machines. The system and method involve providing multiple individuals in the field with sensors that automatically collect data on the expenditure of their supplies. In some cases, wearable sensors are provided to people in the field. The data is sent to a central depository which tracks their inventory of supplies and anticipates needed supplies, compiles and packages additional supplies so that the additional supplies can be delivered to the individuals in the field. A precision supply delivery system is provided for delivering the supplies.
G06Q 10/087 - Inventory or stock management, e.g. order filling, procurement or balancing against orders
F42B 12/02 - Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect
F42B 12/58 - Cluster or cargo ammunition, i.e. projectiles containing one or more submissiles
F42B 15/08 - Self-propelled projectiles or missiles, e.g. rocketsGuided missiles for carrying measuring instruments
G16Y 20/30 - Information sensed or collected by the things relating to resources, e.g. consumed power
G16Y 40/35 - Management of things, i.e. controlling in accordance with a policy or in order to achieve specified objectives
H04L 67/12 - Protocols specially adapted for proprietary or special-purpose networking environments, e.g. medical networks, sensor networks, networks in vehicles or remote metering networks
4.
Cathodes having carbon nanotube (CNT) fibers wound onto metallic substrates
United States of America as represented by the Secretary of the Air Force (USA)
Inventor
Fairchild, Steven
Tsentalovich, Dmitri
Lockwood, Nathaniel
Abstract
A field emission (FE) cathode for a vacuum electronic device (VED) includes a metallic substrate configured to be connected to one of an electrical power supply and an electrical ground, and at least one continuous carbon nanotube (CNT) fiber in tension around at least a portion of the metallic substrate. The substrate can be a cylinder, hoop, plate, stub etc. The at least one continuous CNT fiber can include a filament, yarn, braided yarn, film, fabric, or combination thereof. The at least one continuous CNT fiber is secured to the electrically conductive substrate by vacuum brazing or any other suitable means. Also, a continuous CNT fabric can be secured in either tension or compression to maintain a uniform height of the continuous CNT fabric.
United States of America as represented by the Secretary of the Air Force (USA)
Inventor
Neely, Jared
Joo, James
Topp, Russel
Abstract
A morphing airfoil includes a dynamic flexible skin system that is capable of carrying high level aerodynamic (or fluid) pressure loads over a structural surface. The structural surface can morph and bend in response to control inputs to change a lift force without separate movable control surfaces. A plurality of standoff mounts are attached to an inner surface of anisotropic skin. The standoff mounts include through apertures for receiving a flexible stringer. The anisotropic skin is attached to underlying structure through the flexible stringers. The flexible stringers interface with actuated position control ribs and passive compliant support ribs. A control system causes the underlying support structure to move to a desired location which in turn causes the skin to bend and/or flex without exceeding a stress threshold and thus vary the lift and drag distributions along a span of the airfoil without separate control surfaces.
United States of America as represented by the Secretary of the Air Force (USA)
Inventor
Pankonien, Alexander
Deaton, Joshua
Durscher, Ryan
Abstract
A method and system for measuring strain in a 3D printed part is disclosed herein. The printed part can be formed with internal features that can be analyzed with a digital image correlation system to determine strain levels in internal regions of the part. The features are visually identifiable due to a different color, shape, design or other visually distinguishable characteristics relative to that of the base structural material. The features can be the formed from the same material or a different material from that of the base structure material.
United States of America as represented by the Secretary of the Air Force (USA)
Inventor
Anderson, Michael
Klinke, Christopher
Abstract
A finger strengthening device (FSD) includes a plurality of finger strengthening elements formed therewith. The FSD is attachable to a structure in a plurality of different orientations to permit a variation in finger exercise techniques.
A63B 23/16 - Exercising apparatus specially adapted for particular parts of the body for limbs, i.e. upper or lower limbs, e.g. simultaneously for upper limbs for hands or fingers
A63B 21/00 - Exercising apparatus for developing or strengthening the muscles or joints of the body by working against a counterforce, with or without measuring devices
United States of America as represented by the Secretary of the Air Force (USA)
Inventor
Schlichting, Grant Sharp
Abstract
Apparatuses, systems, and methods for towing an aircraft mid-flight are disclosed. The apparatuses include a tow line receiver that is configured for releasably mechanically joining to an aircraft connector on an aircraft to be towed. The aerial vehicle towing system includes an aircraft connector on the aircraft to be towed, a tow line receiver, a tow line, and a winch. Several methods are also provided. These include: a method of towing or retrieving an aircraft in flight; a method of recharging an electrically-powered aircraft in flight; methods of towing and refueling aircraft in flight; a method of communicating between a tow aircraft and an aircraft being towed; and combinations of these methods.
B60L 53/00 - Methods of charging batteries, specially adapted for electric vehiclesCharging stations or on-board charging equipment thereforExchange of energy storage elements in electric vehicles
United States of America as represented by the Secretary of the Air Force (USA)
Inventor
Silver, Arthur
Abstract
A hypersonic missile defense system for protecting a target from a hypersonic weapon, wherein the system includes a plurality of globule spheres in a defensive formation between the target and the hypersonic weapon. The globule sphere may include a proximity fuse; a plurality of fission spheres; a capacitor capsule; and a membrane separating a first formation material from a second formation material, both contained within the globule sphere.
United States of America as represented by the Secretary of the Air Force (USA)
Inventor
Turgut, Zafer
Abstract
A unique rotor assembly for an electrical machine is disclosed herein. The rotor assembly includes a shaft having an axis of rotation extending within the electrical machine. A central support is connected to the shaft at an intermediate position and a pair of opposing end plates are configured to clamp a plurality of laminate plates therebetween. The laminate plates and a sidewall of the end plates have a non-linear cross-sectional shape such that radial loading due to centrifugal force is transmitted from the laminate plates to the end plates during operation.
H02K 1/2781 - Magnets shaped to vary the mechanical air gap between the magnets and the stator
H02K 15/03 - Processes or apparatus specially adapted for manufacturing, assembling, maintaining or repairing of dynamo-electric machines of stator or rotor bodies having permanent magnets
United States of America as represented by the Secretary of the Air Force (USA)
Inventor
Jones, Tanner
Myers, Gabriel
Abstract
A stand for holding a flight control surface of an aircraft wing. The stand has a longitudinal spine supported by plural uprights and supporting at least two hanger assemblies. Each hanger assembly has attachment points transversely outboard of the spine. Rods articulably depend downwardly from the respective attachment points to be articulably connected at a cradle. The cradle is configured to fixedly hold an aircraft flight control surface for maintenance. By adjusting the transverse spacing of the rods from the spine, the attitude of the flight control surface can be adjusted as needed for a particular maintenance task.
F16M 13/02 - Other supports for positioning apparatus or articlesMeans for steadying hand-held apparatus or articles for supporting on, or attaching to, an object, e.g. tree, gate, window-frame, cycle
12.
Microfluidic flow process for making linear polymers
United States of America as represented by the Secretary of the Air Force (USA)
Inventor
Ghiassi, Kamran B.
Redeker, Neil D.
Abstract
The present invention relates to a microfluidic flow process for making polymers, polymers made by such processes, and methods of using such polymers. In such process, a novel reagent delivery setup is used in conjunction with microfluidic reaction technology to synthesize anionic polymerization reaction products from superheated monomer orders of magnitude faster than is possible in batch and continuous syntheses. The aforementioned process does not require the cryogenic temperatures which are required for such syntheses in batch or bulk continuous. Thus the aforementioned process is more economically efficient and reduces the environmental impact of linear polymer production.
United States of America as represented by the Secretary of the Air Force (USA)
Inventor
Tan, Loon-Seng
Wang, David H.
Yu, Zhenning
Koerner, Hilmar
Abstract
The invention relates to cross-linkable oligoimides, processes of making such cross-linkable oligoimides and products comprising such cross-linkable oligoimides. Such cross-linkable oligoimides provide articles made by an AM process with the desired process ability that permits filament formation, post cure increased strength, the desired in use temperature stability and the desired thermo-oxidative stability.
C08G 73/10 - PolyimidesPolyester-imidesPolyamide-imidesPolyamide acids or similar polyimide precursors
B33Y 70/00 - Materials specially adapted for additive manufacturing
C07D 209/50 - Iso-indolesHydrogenated iso-indoles with oxygen and nitrogen atoms in positions 1 and 3
B29C 64/118 - Processes of additive manufacturing using only liquids or viscous materials, e.g. depositing a continuous bead of viscous material using filamentary material being melted, e.g. fused deposition modelling [FDM]
B29C 64/153 - Processes of additive manufacturing using only solid materials using layers of powder being selectively joined, e.g. by selective laser sintering or melting
B29K 79/00 - Use of other polymers having nitrogen, with or without oxygen or carbon only, in the main chain, as moulding material
B29K 105/24 - Condition, form or state of moulded material cross-linked or vulcanised
United States of America as represented by the Secretary of the Air Force (USA)
Inventor
Mcintire, John P
Srnoyachki, Matt
Sopko, Jason D
Adducchio, Adam C
Abstract
A remotely controlled inswing portable door lock apparatus having a blade including a barb at a distal end and a tang at a proximal end. The barb being configured to be disposed within an aperture of a strike plate. The body having a top and a bottom, wherein the body is operably coupled to the tang of the blade. A paddle being moveably coupled to the body and configured to selectively move between a first orientation substantially flush with the top of the body and a second orientation protruding from the top of the body. The apparatus further including a remotely controllable electronics module coupled to the body and configured to operate an electromechanical electromechanical actuator in cooperation with the paddle, and configured to remotely and selectively position the paddle between the first orientation and the second orientation.
United States of America as represented by the Secretary of the Air Force (USA)
Inventor
Allison, Jonathan
Abstract
A system for managing propellant and pressurant for in-space propulsion of a spacecraft is provided. The system includes a conformal fuel tank having an ullage operatively connected for pressurization and a propellant management device (PMD) to wick propellant to a liquid port of the conformal fuel tank. The system further includes a pneumatic circuit including a tank pressurant vent valve for adjustment of operating pressure prior to refueling operations; a vent to release excess pressurant; a pressurant metering vent valve to provide control and safety relief for the pressurant; a check valve to prevent backflow; a pressurant cat bed for decomposing propellant into pressurant; a repressurizing valve to release pressurant once cooled; a burst disk to provide overpressure safety relief; a series of propellant extraction valves to intake a predetermined quantity of propellant for decomposition; and a pressure regulator that delivers proper pressure to a series of thrusters.
United States of America as represented by the Secretary of the Air Force (USA)
Inventor
Anderson, Joseph
Black, Nicholas
Anderson, Michael
Abstract
A repeater for maintaining wireless line of sight communications. The repeater is autonomously repositional in both absolute location and azimuthal orientation. The repeater has at least two vibratory motors, or other vibration sources, which provide oscillations to depending legs against a support surface. By selectively operating one or more of the vibration sources together or independently, the repeater may be moved as helpful to maintain line of sight communication with another repeater or other operational hardware. A command signal from a remote base station controls the locomotion of the repeater to provide both a change in absolute position relative to the surroundings and a rotational change in azimuthal orientation as necessary to maintain communication under dynamic conditions.
United States of America as represented by the Secretary of the Air Force (USA)
Inventor
Tan, Loon-Seng
Wang, David H.
Abstract
The invention generally relates to polymer nanocomposite films that possess shape memory properties at elevated temperatures. Such films can absorb microwaves, are thermally conductive, are electrically conductive and have increased mechanical strength. In addition, the present invention relates to methods of fabricating such films into 3D objects. Due to the improved properties of such films more advanced sensors and microwave shields can be constructed.
United States of America as represented by the Secretary of the Air Force (USA)
Inventor
Roman, Abdeel
Abstract
A unique cooling system for an aircraft is designed to provide extremely low temperature cooling airflow. The system includes an air source, a first system compressor and a second system compressor positioned in series for compressing and heating the air. A least one heat exchanger can be used to cool the air at predefined locations. A condenser for condensing water out of the air is positioned downstream of the second compressor. The water can be removed with a water separator and at least a portion of any remaining water in the form of liquid or vapor is removed from the air in a membrane dehydration device. The air is expanded in at least one system turbine to bring the air temperature to a subfreezing temperature. The subfreezing air is then used to cool electronic components and mechanical components within the aircraft.
United States of America as represented by the Secretary of the Air Force (USA)
Inventor
Vega-Irizarry, Alfredo
Abstract
A method of detecting starting positions, sizes, and number of records of fields within a bit stream, by formatting the bit stream into a frame using positive logic, then performing decimal conversion of different predetermined field lengths on the framed bit stream, to produce channels. Noise is either removed or amplified from the framed bit stream, and the frame and the channels are input to an image detection module to identify fields within the framed bit stream.
G06T 7/32 - Determination of transform parameters for the alignment of images, i.e. image registration using correlation-based methods
H03M 7/12 - Conversion to or from weighted codes, i.e. the weight given to a digit depending on the position of the digit within the block or code word having two radices, e.g. binary-coded-decimal code
H03M 7/30 - CompressionExpansionSuppression of unnecessary data, e.g. redundancy reduction
H04N 19/126 - Details of normalisation or weighting functions, e.g. normalisation matrices or variable uniform quantisers
20.
Detachable buoyant component for making a watercraft self-righting
United States of America as represented by the Secretary of the Air Force (USA)
Inventor
Azatyan, Hayk
Erwin, William
Ligouri, Anthony
Rennich, Travis
Shald, David
Warren, Adam
Abstract
A component that can be detachably fitted to a watercraft to shift the center of buoyancy of the watercraft and render the watercraft self-righting. The component uses quick release attachment and detachment fixtures so that a person can easily remove the component and thereby free-up space for passengers on the watercraft. The component includes a non-inflatable buoyant structure made of a buoyant material or materials arranged into a buoyant configuration. A watercraft with the detachable component is also disclosed, as is a method for converting a non-self-righting watercraft into a self-righting watercraft.
B63B 39/02 - Equipment to decrease pitch, roll, or like unwanted vessel movementsApparatus for indicating vessel attitude to decrease vessel movements by displacement of masses
B63B 1/04 - Hydrodynamic or hydrostatic features of hulls or of hydrofoils deriving lift mainly from water displacement with single hull
United States of America as represented by the Secretary of the Air Force (USA)
Inventor
Visbal, Miguel
Garmann, Daniel
Abstract
A micro-cavity passive actuator is configured to delay dynamic stall of an airfoil. The micro-cavity actuator is formed in the pressure sidewall surface proximate the leading edge of the airfoil. This cavity remains essentially inactive at low incidence. However, as the wing's effective angle of attack dynamically increases and the stagnation point displaces past the micro-cavity, the accelerating flow grazing the cavity induces a high-frequency resonance phenomenon (known as Rossiter modes). The self-generated small-scale disturbances are carried around the leading-edge through the boundary layer to the wing's upper side where the laminar separation bubble (LSB) amplifies these disturbances. This process delays LSB bursting and dynamic stall. The micro-cavity must be sized such that its naturally emitting oscillations are in a range of frequencies that can be amplified by the LSB.
United States of America as represented by the Secretary of the Air Force (USA)
Inventor
Tassev, Vladimir
Abstract
3 (ammonia), and HF (hydrogen fluoride); flowing the carrier gas over the Group II/III element; exposing the substrate to the ternary-forming gasses in a predetermined ratio of first ternary-forming gas to second ternary-forming gas (1tf:2tf ratio); and changing the 1tf:2tf ratio over time.
United States of America as represented by the Secretary of the Air Force (USA)
Inventor
O'Brien, Courtney Jane
Abstract
A tool box with vertically stacked monolithic trays. Each tray has pockets specifically shaped to receive complementary tools. The trays have upstanding cantilevered posts, which can space apart the superjacent tray. Alternatively, the posts can be received in complementary sockets of superjacent trays to prevent undue lateral movement while in the tool box. The post and socket geometry can be constructed to index the order in which trays are stacked and index how individual trays are oriented for optimal and sequenced access to the tools.
United States of America as represented by the Secretary of the Air Force (USA)
Inventor
Luu, Jonathan W.
Fenton, Kevin P.
Simske, Steve
Abstract
An apparatus for automated safety data sheet (SDS) processing that translates the entire SDSs from numerous chemical vendors, and in various formats (.pdf, .doc, .txt, .jpg, gif, .png, etc) to machine-encoded text by employing optical, RFID, and infrared scanning, reading and writing devices. The apparatus reads and assess documents as a human would; ensuring that the documents are compliant, ensuring reported values are within expected thresholds, and that there are no conflicts in hazardous material classification, and comparing to similar products for more environmentally friendly alternatives. The apparatus further employs a processor that computes meta-algorithms as trainable neural networks that allow the invention to “learn” and appropriately classify values and calculate statistical probabilities for output accuracy and precision.
United States of America as represented by the Secretary of the Air Force (USA)
Inventor
Sherburne, Michael D.
Abstract
The present invention relates to devices for measuring property changes via in-situ micro-viscometry and methods of using same. The aforementioned device is inexpensive and can be used to quickly and accurately measure numerous physical and chemical property changes, including but not limited to the rate of chemical cure, change in tack, and rate of mass loss, for example, rate of moisture, solvent and/or plasticizer change.
C09K 11/88 - Luminescent, e.g. electroluminescent, chemiluminescent, materials containing inorganic luminescent materials containing selenium, tellurium or unspecified chalcogen elements
B05D 3/06 - Pretreatment of surfaces to which liquids or other fluent materials are to be appliedAfter-treatment of applied coatings, e.g. intermediate treating of an applied coating preparatory to subsequent applications of liquids or other fluent materials by exposure to radiation
B05D 7/00 - Processes, other than flocking, specially adapted for applying liquids or other fluent materials to particular surfaces or for applying particular liquids or other fluent materials
C09D 163/00 - Coating compositions based on epoxy resinsCoating compositions based on derivatives of epoxy resins
G01N 21/33 - Investigating relative effect of material at wavelengths characteristic of specific elements or molecules, e.g. atomic absorption spectrometry using ultraviolet light
B82Y 30/00 - Nanotechnology for materials or surface science, e.g. nanocomposites
B82Y 40/00 - Manufacture or treatment of nanostructures
26.
Remotely operable cover for aircraft refueling boom
United States of America as represented by the Secretary of the Air Force (USA)
Inventor
Helzer, Jacob
Abstract
A boom cover for covering a refueling boom, particularly a flying boom, of a refueling aircraft. The boom has a closure which has a shield sized to cover the open end of the refueling boom, to prevent intrusion of debris, animals, etc. The closure has a hoop for circumscribing the boom and drawing the shield taut for remaining on the boom and flaccid for attachment to and removal from the boom. The closure may be attached to and removed from the boom by a longitudinally rotatable handle which is manipulated by a ground operator. Optionally the handle may be removable from the closure for use on subsequent aircraft or storage.
United States of America as represented by the Secretary of the Air Force (USA)
Inventor
Hausgen, Paul E.
Wilt, David M.
Abstract
In accordance with various embodiments of the disclosed subject matter, a system and method is configured for scheduling and invoking power sharing among satellites within a constellation of satellites such that energy storage systems at a target satellite may by charged prior to the use of electric propulsion thrust activation or other high electricity demand operations (or such operations contemporaneously augmented) by power beams transmitted from other (source) satellites within the constellation.
United States of America as represented by the Secretary of the Air Force (USA)
Inventor
Tan, Loon-Seng
Yu, Zhenning
Abstract
The invention relates to bis(aniline) compounds containing multiple arylethynyl, alkylethynyl, ethynyl groups or their combinations, processes of making such compounds and materials comprising such compounds. Such, bis(aniline) compounds preferably comprise multiple phenylethynyl (PE) groups, i.e. 2-4 PE moieties. Such compounds are useful monomers for the preparation of polyimides, polyamides and poly(amide-imides) whose post-fabrication crosslinking chemistry (i.e. reaction temperature) can be controlled by the number of PE per repeat unit as well as finding utility in thermosetting matrix resins, 3D printable resins, and as high-carbon-content precursors to carbon-carbon composites.
C07C 211/50 - Compounds containing amino groups bound to a carbon skeleton having amino groups bound to carbon atoms of six-membered aromatic rings of the carbon skeleton having amino groups bound to only one six-membered aromatic ring having at least two amino groups bound to the carbon skeleton with at least two amino groups bound to carbon atoms of six-membered aromatic rings of the carbon skeleton
C07C 209/06 - Preparation of compounds containing amino groups bound to a carbon skeleton by substitution of functional groups by amino groups by substitution of halogen atoms
C07C 209/36 - Preparation of compounds containing amino groups bound to a carbon skeleton by reduction of nitrogen-to-oxygen or nitrogen-to-nitrogen bonds by reduction of nitro groups by reduction of nitro groups bound to carbon atoms of six-membered aromatic rings
29.
Disk engine with circumferential swirl radial combustor
United States of America as represented by the Secretary of the Air Force (USA)
Inventor
Bohan, Brian
Polanka, Marc
Staton, Bennett
Abstract
A disk engine and system configured to provide high power at a reduced axial length is disclosed herein. The disk engine includes a radial compressor, a compressor discharge manifold positioned circumferentially about compressor, a combustion chamber positioned within the discharge manifold and a radial turbine positioned radially inward of the combustion chamber.
F02C 3/08 - Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor the compressor comprising at least one radial stage
United States of America as represented by the Secretary of the Air Force (USA)
Inventor
Tabor, Christopher E
Watson, Alexander M
Cook, Alexander B
Abstract
An extrusion printing process for conductive materials and a conductive material extrusion system. The process includes attaching a counter-electrode to a first side of a substrate. A drive voltage is applied to the counter-electrode and to a conductive material to be extruded onto a second side of the substrate, opposite the first side. The conductive material is extruded onto the second side of the substrate while the drive voltage is being applied to the counter-electrode and conductive material. The conductive material is selected from a metal having a melting point ranging from about −20° C. to about 150° C.
B33Y 30/00 - Apparatus for additive manufacturingDetails thereof or accessories therefor
B33Y 70/00 - Materials specially adapted for additive manufacturing
H05K 3/12 - Apparatus or processes for manufacturing printed circuits in which conductive material is applied to the insulating support in such a manner as to form the desired conductive pattern using printing techniques to apply the conductive material
United States of America as represented by the Secretary of the Air Force (USA)
Inventor
Rutledge, James
Fuqua, Matthew
Bryant, Carol
Abstract
A method and system for cooling an engine and/or vehicle using energy separation is disclosed herein. An energy separation device is operable for separating a compressed gaseous coolant stream into a first relatively cooler coolant flow stream and a second relatively hotter coolant flow stream. The relative cooler coolant flow stream is directed to a first region requiring increased cooling and the relative hotter coolant flow stream is directed to a second region requiring lower cooling than the first region in the engine or vehicle.
United States of America as represented by the Secretary of the Air Force (USA)
Inventor
Claflin, Bruce B.
Grzybowski, Gordon J.
Kiefer, Arnold M.
Abstract
A method for depositing a monocrystalline or polycrystalline tin alloy layer on an amorphous or crystallographically mis-matched substrate. The method includes selecting tin halide as the tin source; selecting an alloying metal precursor from germanium precursors, silicon precursors, and mixtures of germanium and silicon precursors; selecting a substrate from amorphous substrates and crystallographically mis-matched substrates; generating an inert gas plasma in a remote plasma generation reactor; contacting the inert gas plasma with the tin halide to provide an activated tin halide flow stream; contacting the inert gas plasma with the alloying metal precursor to provide an activated alloying metal flow stream; directing the activated tin halide flow stream and activated alloying metal flow stream to an alloy deposition chamber physically remote from the plasma chamber; and depositing the monocrystalline or polycrystalline tin alloy layer on the substrate in the deposition chamber.
H01L 21/3205 - Deposition of non-insulating-, e.g. conductive- or resistive-, layers, on insulating layersAfter-treatment of these layers
C23C 16/06 - Chemical coating by decomposition of gaseous compounds, without leaving reaction products of surface material in the coating, i.e. chemical vapour deposition [CVD] processes characterised by the deposition of metallic material
C23C 16/50 - Chemical coating by decomposition of gaseous compounds, without leaving reaction products of surface material in the coating, i.e. chemical vapour deposition [CVD] processes characterised by the method of coating using electric discharges
C30B 25/10 - Heating of the reaction chamber or the substrate
United States of America as represented by the Secretary of the Air Force (USA)
Inventor
Puglisi, Joseph
Black, Nicholas
Hood, Mary
Anderson, Michael
Anderson, Joseph
Abstract
A drone for delivering plural repeaters in a hostile environment and method of delivering plural repeaters from the drone. The drone is controllable from a remote base station and carries a payload of repeaters on a round tray. The tray has a dispensing hole, complementary to the geometry of the repeater for dispensing the repeaters as needed. Repeaters are consecutively dispensed at stations as determined by an operator. A central radial arm sweeps each repeater around the tray, in turn, until the hole is encountered and the repeater gravity drops to a surface below. The drone may have two or more vertically stacked trays to increase payload without increasing footprint.
United States of America as represented by the Secretary of the Air Force (USA)
Inventor
Burnett, Gregory
Romigh, Griffin
Thompson, Eric
Abstract
Provided herein are novel methods for providing an enhanced audio signal adapter. The invention provides an in-line audio adapter that digitally enhances bi-directional radio communication for dismounted and mounted operators. The adapter may be customizable to the hearing ability of the radio user, and compatible with both standard military audio connectors and commercial audio connectors enhancing the operator's in-field capabilities to process, record, share, replay, and operate radio communications.
United States of America as represented by the Secretary of the Air Force (USA)
Inventor
Mahoney, Clare M.
Vaia, Richard A.
Park, Kyoungweon
Abstract
The present invention relates to processes for selective reshaping of nanoparticles in three dimensional articles, three dimensional articles produced by such processes, and methods of using such three dimensional articles. As a result of the aforementioned process, such three dimensional articles can have selective tuning that arises, at least in part, from the reshaped nanoparticles found in such articles. Such tuning provides the aforementioned articles with superior performance that can be advantageous in the areas including such as optical filters, multi-functional composites and sensing elements.
B33Y 70/00 - Materials specially adapted for additive manufacturing
B33Y 80/00 - Products made by additive manufacturing
C09D 11/101 - Inks specially adapted for printing processes involving curing by wave energy or particle radiation, e.g. with UV-curing following the printing
C09D 11/106 - Printing inks based on artificial resins containing macromolecular compounds obtained by reactions only involving carbon-to-carbon unsaturated bonds
C09D 11/107 - Printing inks based on artificial resins containing macromolecular compounds obtained by reactions only involving carbon-to-carbon unsaturated bonds from unsaturated acids or derivatives thereof
37.
Aerospace vehicle comprising module for method of terrain, terrain activity and material classification
United States of America as represented by the Secretary of the Air Force (USA)
Inventor
Nussbaum, Matthew Edward
Herron, Marissa Sachiko
Abstract
A method of classifying terrain, terrain activity and materials through panchromatic imagery a module programmed to provide such classification and aerospace vehicles comprising such module is provided. Panchromatic images of known materials terrains and terrain activities are taken and processed to form a multiband texture cube, that due it amount of data, is stored as a computer data base. New panchromatic images of unclassified materials, terrains and/or terrain activities are processed and compared via computer with such database that allows for inexpensive, quick and efficient classification of such new images.
United States of America as represented by the Secretary of the Air Force (USA)
Inventor
Azatyan, Hayk
Erwin, William
Ligouri, Anthony
Rennich, Travis
Shald, David
Warren, Adam
Abstract
An aquatic rescue vehicle formed by adding directional and speed controls to a watercraft along with an autonomous control system to guide the vehicle to specified waypoints is disclosed. The rescue vehicle includes search devices such as a radio direction finder (RDF) and an infrared sensor (or camera) to be used to narrow the search for an isolated person (IP). The rescue vehicle may be discharged from a larger watercraft or an airplane and autonomously set out on its rescue mission. The vehicle may first navigate to a designated waypoint near an IP, and then use signals gathered from the RDF and infrared sensor to finally locate, assist, and retrieve the IP. The vehicle also includes a self-righting mechanism so that the vehicle can complete its mission even under the most adverse conditions.
B63B 79/40 - Monitoring properties or operating parameters of vessels in operation for controlling the operation of vessels, e.g. monitoring their speed, routing or maintenance schedules
B63B 35/00 - Vessels or similar floating structures specially adapted for specific purposes and not otherwise provided for
B63C 9/02 - Lifeboats, life-rafts or the like, specially adapted for life-saving
G05D 1/00 - Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
G05D 1/02 - Control of position or course in two dimensions
39.
Systems, methods and apparatus for coupling solar cells
United States of America as represented by the Secretary of the Air Force (USA)
Inventor
Bradshaw, Geoffrey Keith
Abstract
Systems, methods and apparatus related to a multijunction solar cell. The apparatus comprises a first sub-solar cell, a second sub-solar cell in series with the first sub-solar cell and one or more quantum wells. At least some of the quantum wells are disposed in a region of the first sub-solar cell, and have a thickness and a bandgap sized such that a bandgap in selected quantum wells are less than a bandgap of a material of the first sub-solar cell and greater than a bandgap of a material of the second sub-solar cell resulting in radiative coupling between the first sub-solar cell and the second sub-solar cell.
H01L 31/0352 - SEMICONDUCTOR DEVICES NOT COVERED BY CLASS - Details thereof characterised by their semiconductor bodies characterised by their shape or by the shapes, relative sizes or disposition of the semiconductor regions
H01L 31/0304 - Inorganic materials including, apart from doping materials or other impurities, only AIIIBV compounds
H01L 31/05 - Electrical interconnection means between PV cells inside the PV module, e.g. series connection of PV cells
40.
Multi-gateway multi-beam satellite communication system with precoding feedback controllers
United States of America as represented by the Secretary of the Air Force (USA)
Inventor
Pham, Khanh
Abstract
A multi-gateway multi-beam satellite communication system. The system has a satellite a plurality of gateways for providing broadband services to users and being in bilateral communication with the satellite by a like plurality of feeder links and a second plurality of clusters of coverage areas in bilateral communication with the satellite by a like plurality of service links. The system has a precoder for allocating power to either or both of the feeder links and service links. Precoding can be based on signal to noise plus interference ratio or interference temperature. Precoding can be based on discrete-time dynamical feedback system frameworks with real-time feedback signaling comprised of signal-to-noise plus interference ratio, signal-to-leakage-plus-noise ratio, interference temperatures and/or tracking errors.
H04B 7/0456 - Selection of precoding matrices or codebooks, e.g. using matrices for antenna weighting
H04B 7/06 - Diversity systemsMulti-antenna systems, i.e. transmission or reception using multiple antennas using two or more spaced independent antennas at the transmitting station
H04B 17/336 - Signal-to-interference ratio [SIR] or carrier-to-interference ratio [CIR]
United States of America as represented by the Secretary of the Air Force (USA)
Inventor
Sauder, Ii, Gene David
Strout, Bon
Abstract
An air deployable buoyant device for transmitting data on its location and the conditions in the air as it descends to the surface of a body of water, and on conditions on a body of water on a real-time basis is disclosed. The device includes a buoy and a plurality of sensors and a transmitter associated with the buoy. The transmitter transmits data on the location of the device and the conditions in the air and on a body of water on a real-time basis to at least one receiver. The receiver may be located over the horizon or in line of sight with the device. The sensors are in communication with the transmitter, and each sensor measures at least one condition in the air and/or on a body of water to assist in locating a person in the water and provide information on the water conditions to a rescue team. Methods of deploying and using the buoyant device are also disclosed herein.
United States of America as represented by the Secretary of the Air Force (USA)
Inventor
Ligouri, Anthony
Azatyan, Hayk
Erwin, William
Rennich, Travis
Shald, David
Warren, Adam
Abstract
A method of determining the location of an object in a camera field of view is disclosed. The method may utilize a camera system that includes a digital video camera and a computer that runs image analysis software for analyzing images received from the camera. The image analysis software is configured to isolate pixel groups in each image. The method includes the steps of locating an object in the camera's field of view in which the object is represented by a set of pixels; identifying the centroid of the set of pixels representing the object; and calculating the location of the object relative to the camera based upon known parameters including the focal plane and camera lens location.
United States of America as represented by the Secretary of the Air Force (USA)
Inventor
Tan, Loon-Seng
Yu, Zhenning
Zheng, Bingqian
Koerner, Hilmar
Abstract
A family of low-molecular-weight, main-chain thermotropic liquid-crystalline co-polyimides (TLC-CoPI) that are crosslinkable, and based on a unique, liquid-crystallinity (LC)-enabling diamine, namely, 1,3-bis[4-(4′-aminophenoxy)cumyl]benzene (BACB) and two or more mesogenic dianhydrides, at least one of which is a diphthalic dianhydride (DPA) that contains one or more thermally reactive and crosslinkable moieties similar to that of phenylethynyl (PE) is disclosed. Processes of making and using such low-molecular-weight, main-chain thermotropic liquid-crystalline co-polyimides are also provided.
United States of America as represented by the Secretary of the Air Force (USA)
Inventor
Tan, Loon-Seng
Yu, Zhenning
Abstract
Applicants disclose a family of rod-like dianhydrides that contain two phthalic anhydride moieties linked by a bridge that is comprised of at least one ethynyl and one paraphenylene group and processes of making and using such rod-like dianhydrides. Such rod-like dianhydrides can endow net-work structures with improved mechanical and thermal properties in the crosslinked-polymer products.
United States of America as represented by the Secretary of the Air Force (USA)
Inventor
Moore, Levi Michael Joseph
Marcischak, Jacob C.
Haddad, Timothy S.
Ghiassi, Kamran B.
Yandek, Gregory R.
Abstract
The present invention relates to articles comprising crosslinked polymer network comprising thioether crosslinks and process of making and using same. Such thiol-ene crosslinking reactions not only make the isocyanate crosslinking reaction unnecessary, but they also improve the article's strength due to chemical crosslinking between the article's resin layers, and reduce or eliminate post curing. Thus resulting in a sufficiently cured article in a much shorter time.
C08F 2/46 - Polymerisation initiated by wave energy or particle radiation
C08C 19/20 - Incorporating sulfur atoms into the molecule
C08C 19/28 - Reaction with compounds containing carbon-to-carbon unsaturated bonds
C08F 2/50 - Polymerisation initiated by wave energy or particle radiation by ultraviolet or visible light with sensitising agents
C08G 61/04 - Macromolecular compounds containing only carbon atoms in the main chain of the macromolecule, e.g. polyxylylenes only aliphatic carbon atoms
United States of America as represented by the Secretary of the Air Force (USA)
Inventor
Neely, Jared
Joo, James
Abstract
The present disclosure defines a morphing airfoil having a dynamic flexible skin system that is capable of carrying high level aerodynamic (or fluid) pressure loads over a structural surface. The structural surface can morph and deflect in response to control inputs to change a lift force without separate movable control surfaces. The anisotropic skin is attached to underlying structure that is both actively controlled and passively supported. A control system causes the underlying support structure to move to a desired location which in turn causes the skin to bend and/or flex without exceeding a stress threshold and thus vary the lift profile along a span of the airfoil.
United States of America as represented by the Secretary of the Air Force (USA)
Inventor
Smith, Paul
Reynolds, Tina
Abstract
An instrumented wind tunnel. The wind tunnel receives a test subject which can be a model of an object to be tested with dynamic airflow. The test subject is fitted with at least one sensor to deliver data to a chassis, which in turn uses a network having at least 10 Gb/s capability to deliver the data to a RAM cache. The RAM cache can push the data to multiple viewers for real time monitoring of wind tunnel tests. The operator can then make live adjustments of the test conditions.
United States of America as represented by the Secretary of the Air Force (USA)
Inventor
O'Brien, Courtney
Abstract
A tool box with vertically stacked monolithic trays. Each tray has pockets specifically shaped to receive complementary tools. The trays have upstanding cantilevered posts, which can space apart the superjacent tray. Alternatively, the posts can be received in complementary sockets of superjacent trays to prevent undue lateral movement while in the tool box. The post and socket geometry can be constructed to index the order in which trays are stacked and index how individual trays are oriented for optimal and sequenced access to the tools.
United States of America as represented by the Secretary of the Air Force (USA)
Inventor
Beblo, Richard
Cruz-Gonzalez, Tizoc
Tidball, Mackenzie
Reich, Gregory
Dickinson, Benjamin
Abstract
The present disclosure is directed to a missile having a main body and an articulating nosecone connected to the main body. An actuation system is operable for moving the nosecone relative to the main body via one or more electric motors and associated components. A central aperture is formed through electric motors and the associated components between the main body and the nosecone. One or more cables for transmitting electrical power, sensor data, control signals and the like extend through the central aperture between the main body and the nosecone to provide means for controlling the actuation system.
United States of America as represented by the Secretary of the Air Force (USA)
Inventor
Bales, John
Orsi, Alexander
Okeefe, James
Schory, Kyle
Baker, Stuart
Abstract
A device and method for remote-controlled explosive ordnance disposal using an explosive ordnance disposal device that includes a carriage adjustably attached to a device frame having a rotatable bar. The rotatable bar including at least a laser face, an x-ray face, and a disarm device face; the rotatable bar rotated by a servo motor, the servomotor being remotely operable. The laser face having a laser capable of a laser beam visible to a remote viewing device. The remote viewing device co-mounted to the laser face and remotely viewable. The x-ray face having an x-ray device attached to it. The disarm device face having a bomb disarming device attached; wherein the carriage and the rotatable bar may be remotely adjusted such that upon remote rotation the laser, x-ray and bomb disarming device share an aligned orientation and placement for operation.
F42D 5/04 - Rendering explosive charges harmless, e.g. destroying ammunitionRendering detonation of explosive charges harmless
G01N 23/04 - Investigating or analysing materials by the use of wave or particle radiation, e.g. X-rays or neutrons, not covered by groups , or by transmitting the radiation through the material and forming images of the material
The Regents of the University of Colorado, a body corporate (USA)
The United States of America as represented by the Secretary of the Air Force (USA)
Inventor
Daughety, Nathan
Pendleton, Marcus
Xu, Shouhuai
Njilla, Laurent L.
Reuther, Tyler
Abstract
A cross-domain solution architecture includes a higher-security domain and a lower-security domain. The higher-security domain (i) processes data on a higher-security level, and (ii) includes a hardware-based trusted executed environment (TEE) running a formally verified microkernel. The lower-security domain (i) processes data on a lower-security level having lower security than the higher-security level, and (ii) includes a trusted computer base (TCB). The TCB operates in the higher-security domain and the lower-security domain to pass data from the lower-security domain to the higher-security domain through a first data diode, and to pass data from the higher-security domain to the lower-security domain through a second data diode.
United States of America as represented by the Secretary of the Air Force (USA)
Inventor
Fairchild, Steven B.
Boeckl, John J.
Dion, Genevieve
Amanatides, Chelsea
Abstract
An electrode comprising a conductive textile structure having an inner surface that is connected to one of an electrical power supply and an electrical ground; the conductive textile structure having an outer surface, the outer surface comprising a carbon nanotube (CNT) fiber fabric fixed thereon, the CNT fiber fabric having continuous CNT fiber on the outer surface, wherein the CNT fiber fabric comprises at least one of a CNT fiber, and is at least one of knitted, woven, sewn, and embroidered. The continuous CNT fiber may be a yarn, ribbon, or thread. The CNT fiber fabric includes at least one face having a looped or interlaced structure made from the continuous CNT fiber. The CNT fiber yarn, ribbon, or thread is knitted, woven, sewn, and/or embroidered so that at least one surface comprises a textile made with CNT fiber yarns, ribbons, or threads.
United States of America as represented by the Secretary of the Air Force (USA)
Inventor
Williams, Timothy K
Neff, Lucas Paul
Abstract
Endovascular variable aortic control catheters (EVACC) are provided that are adapted to augment upstream blood pressure and regulate downstream blood flow for patients in shock. The EVACC devices provide improved treatment for truncal wounds, which may be used for example on a battlefield, thereby increasing survivability of injured soldiers. The devices are a catheter-based system having a proximal hand piece for controlled deployment of the device through a delivery sheath. A collapsible, wire framework supports an expandable and collapsible occlusion barrier. The wire basket and occlusion barrier expand to fit within the lumen of the aorta. Various movable elements are used to adjust an adjustable passageway to regulate controlled anterograde blood flow.
A61B 17/12 - Surgical instruments, devices or methods for ligaturing or otherwise compressing tubular parts of the body, e.g. blood vessels or umbilical cord
A61M 60/13 - Implantable pumps or pumping devices, i.e. the blood being pumped inside the patient’s body implantable via, into, inside, in line, branching on, or around a blood vessel by means of a catheter allowing explantation, e.g. catheter pumps temporarily introduced via the vascular system
A61M 60/139 - Implantable pumps or pumping devices, i.e. the blood being pumped inside the patient’s body implantable via, into, inside, in line, branching on, or around a blood vessel inside a blood vessel, e.g. using grafting inside the aorta, e.g. intra-aortic balloon pumps
A61M 60/295 - Balloon pumps for circulatory assistance
United States of America as represented by the Secretary of the Air Force (USA)
Inventor
Gillaugh, Daniel
Kaszynski, Alexander
Brown, Jeffrey
Abstract
The present disclosure is directed to a method and system for repairing a blade for a turbomachine that has been damaged due to foreign object impact. Machine learning algorithms are used to determine an amount of material to be removed from one or more damage locations and determine an amount of material addition to the damaged portion(s) and/or at other locations on the blade to keep the natural frequencies of the repaired blade within design limits during operation.
United States of America as represented by the Secretary of the Air Force (USA)
Inventor
Mercier, Robert
Gruber, Mark
Milligan, Ryan
Abstract
A scramjet engine with a novel isolator is disclosed herein. The scramjet includes an air inlet configured to receive and direct air into the engine and a combustor operable to receive air from the air inlet and combust fuel therein as is conventional. An isolator is positioned between the air inlet and the combustor. The isolator includes a primary flow path separated into a plurality of separate secondary flow channels formed therethrough. The smaller secondary flow channels prevent shockwaves from propagating upstream from the combustor to the inlet that can occur during some operating conditions of a supersonic combustion flow process.
F02K 7/14 - Plants in which the working-fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fanControl thereof characterised by having ram-action compression, i.e. aero-thermo-dynamic-ducts or ram-jet engines with external combustion, e.g. scram-jet engines
F02C 7/04 - Air intakes for gas-turbine plants or jet-propulsion plants
United States of America as represented by the Secretary of the Air Force (USA)
Inventor
Hoppe, Christopher
Ehler, Andrew
Snyder, Matthew
Abstract
A missile comprises a generally cylindrical body having a distal end and a proximal end; a nosecone having a pointed distal end and a proximal end, wherein the proximal ends of the body and nosecone are oriented toward each other; a forward angled section rotatably attached to the proximal end of the nosecone at its forward edge, the opposite end of the forward angled section having an angled edge perpendicular to the longitudinal axis except for the angle defined by the edge; a rear angled section rotatably attached to the proximal end of the body at its rear edge, the opposite end of the forward angled section having an angled edge matching the angled edge of the forward angled section, the angled edges of the forward angled section and the rear angled section being rotatably attached.
United States of America as represented by the Secretary of the Air Force (USA)
Inventor
Rodriguez, Dilia E.
Abstract
Systems and associated methods for constructing neural networks (NN) without the benefit of predefined output spike times or predefined network architecture. Functions are constructed from other functions determined from an input construction training set of output variable type. Method aspects of the neural network modeler may comprise partitioning the construction training set, representing the partitions, restricting the representations, constructing subfunctions from the restrictions, and combining the subfunctions to model the target function. Specifically, subfunctions represented from partition-specific neural networks of output value type are created using two fundamental composition operations: same-constant composition and different-constants composition. Different choices of weights and delays lead to different NNs with different output spikes that implement the same function.
United States of America as represented by the Secretary of the Air Force (USA)
Inventor
Adorno, Ruben
Palazotto, Anthony
Abstract
An apparatus for lifting a load to a desired altitude using an evacuated hollow lift body is disclosed. Once evacuated, the apparatus is lighter than the surrounding atmosphere. The lift body can be formed as a hollow fluid tight structure with a tube wound and sealed in a helical pattern or a dual membrane structure with a pressurized intermediate volume sandwiched between inner and outer membranes. A load can be attached to the apparatus and lifted to an altitude where the effective density of the apparatus and load is equivalent to the density of the surrounding atmosphere.
United States of America as represented by the Secretary of the Air Force (USA)
Inventor
Anderson, Michael
Klinke, Christopher
Abstract
A finger strengthening device (FSD) includes a plurality of finger strengthening elements formed therewith. The FSD is attachable to a structure in a plurality of different orientations to permit a variation in finger exercise techniques.
A63B 23/16 - Exercising apparatus specially adapted for particular parts of the body for limbs, i.e. upper or lower limbs, e.g. simultaneously for upper limbs for hands or fingers
A63B 21/00 - Exercising apparatus for developing or strengthening the muscles or joints of the body by working against a counterforce, with or without measuring devices
United States of America as represented by the Secretary of the Air Force (USA)
Inventor
Nicholson, Brian
Abstract
An exo-bearing system for a turbomachine is operable to improve aerodynamic efficiency and mechanical limits of rotor blades for fans, compressors, turbines, pumps and the like. The exo-bearing system is positioned between the tips of the blades and a surrounding structural housing. The exo-bearing system eliminates the air gap that is formed in prior art turbomachines and causes the blades to load in compression during operation which increases mechanical operability of the blades.
United States of America as represented by the Secretary of the Air Force (USA)
Inventor
Tan, Loon-Seng
Wang, David H.
Yu, Zhenning
Koerner, Hilmar
Abstract
The invention relates to cross-linkable thermoplastics, processes of making such cross-linkable thermoplastics and products comprising such cross-linkable thermoplastics. Such cross-linkable thermoplastics provide articles made by the additive manufacturing (AM) process with increased strength, the desired in use temperature stability and the desired thermo-oxidative stability.
B29C 64/118 - Processes of additive manufacturing using only liquids or viscous materials, e.g. depositing a continuous bead of viscous material using filamentary material being melted, e.g. fused deposition modelling [FDM]
B29C 64/153 - Processes of additive manufacturing using only solid materials using layers of powder being selectively joined, e.g. by selective laser sintering or melting
B29K 79/00 - Use of other polymers having nitrogen, with or without oxygen or carbon only, in the main chain, as moulding material
B29K 105/00 - Condition, form or state of moulded material
C07D 209/50 - Iso-indolesHydrogenated iso-indoles with oxygen and nitrogen atoms in positions 1 and 3
United States of America as represented by the Secretary of the Air Force (USA)
Inventor
Mendez, Edgar
Abstract
A piston actuated cartridge valve (PACV) can be formed within a fluid fitting such as a tee or cross member in a fluid piping system. The PACV includes a base mount extending between first and second ends having a stop and a slide positioned therein. The slide is movable between a closed position and a fully open position by an actuation piston and spring working in combination. The slide permits fluid flow therethrough in the open position and restricts fluid flow in the closed position.
F16K 11/18 - Multiple-way valves, e.g. mixing valvesPipe fittings incorporating such valvesArrangement of valves and flow lines specially adapted for mixing fluid with two or more closure members not moving as a unit operated by one actuating member, e.g. a handle with separate operating movements for separate closure members
F16K 31/52 - Mechanical actuating means with crank, eccentric, or cam
F16K 11/16 - Multiple-way valves, e.g. mixing valvesPipe fittings incorporating such valvesArrangement of valves and flow lines specially adapted for mixing fluid with two or more closure members not moving as a unit operated by one actuating member, e.g. a handle which only slides, or only turns, or only swings in one plane
United States of America as represented by the Secretary of the Air Force (USA)
Inventor
Neely, Jared
Joo, James
Topp, Russel
Abstract
A morphing airfoil includes a dynamic flexible skin system that is capable of carrying high level aerodynamic (or fluid) pressure loads over a structural surface. The structural surface can morph and bend in response to control inputs to change a lift force without separate movable control surfaces. A plurality of standoff mounts is attached to an inner surface of anisotropic skin. The standoff mounts include through apertures for receiving a flexible stringer. The anisotropic skin is attached to underlying structure through the flexible stringers. The flexible stringers interface with actuated position control ribs and passive compliant support ribs. A control system causes the underlying support structure to move to a desired location which in turn causes the skin to bend and/or flex without exceeding a stress threshold and thus vary the lift and drag distributions along a span of the airfoil without separate control surfaces.
United States of America as represented by the Secretary of the Air Force (USA)
Inventor
Anderson, Joseph
Black, Nicholas
Anderson, Michael
Abstract
A repeater for maintaining wireless line of sight communications. The repeater is autonomously repositional in both absolute location and azimuthal orientation. The repeater has at least two vibratory motors, or other vibration sources, which provide oscillations to depending legs against a support surface. By selectively operating one or more of the vibration sources together or independently, the repeater may be moved as helpful to maintain line of sight communication with another repeater or other operational hardware. A command signal from a remote base station controls the locomotion of the repeater to provide both a change in absolute position relative to the surroundings and a rotational change in azimuthal orientation as necessary to maintain communication under dynamic conditions.
United States of America as represented by the Secretary of the Air Force (USA)
Inventor
Mcintire, John P.
Srnoyachki, Matthew
Abstract
The emergency egress apparatus includes a protuberance mated to a first portion of the door barricade and a keeper mated to a second portion of the door barricade. A retainer is selectively disposed between one of two positions. A first position defines the placement of the retainer that establishes an interference fit between the protuberance and the keeper. A second position defines the placement of the retainer such that it is not in contact with the protuberance or the keeper. The first position secures the first portion of the door barricaded with respect to the second portion of the door barricade, and the second position decouples the first portion of the door barricade with respect to the second portion of the door barricade.
E05C 17/08 - Devices for holding wings openDevices for limiting opening of wings or for holding wings open by a movable member extending between frame and wingBraking devices, stops or buffers, combined therewith by mechanical means with a movable bar or equivalent member extending between frame and wing with special means for release, e.g. automatic release by further opening
67.
Passive characterization of high power optical fiber average power and LP01 and LP11 modes by detecting MIE scattered light
United States of America as represented by the Secretary of the Air Force (USA)
Inventor
Jones, John G
Zelmon, David E.
Hopkins, Frank K.
Mcnamara, Arianna M.
Martin, Michael D.
Ncnamara, Shamus P.
Abstract
A scattered light detector comprises a first photodiode array comprising one or more photodiodes arranged in a planar, semicircular pattern on a substrate, each of the one or more photodiodes having an outer edge and an inner edge; and a notch perpendicular to the substrate and located adjacent the inner edge of each of the one or more diodes, and equidistant from the outer edges of each of the one or more photodiodes, the notch configured to accept an optical fiber oriented perpendicular to the plane of the one or more photodiodes. When there are two or more photodiodes, the photodiodes may be divided into two or more segments extending outwardly from the notch. Each of the photodiodes shares a common electrical ground. The planes of the one or more photodiodes of the first and second photodiode arrays are oriented parallel to each other and spaced a predetermined distance apart.
United States of America as represented by the Secretary of the Air Force (USA)
Inventor
Bishop, Morgan A.
Nagy, James M.
Pottenger, William M.
Hoogs, Anthony
Tong, Tuanjie
Abstract
A video information extraction system includes a memory to store a video; a textual information extraction module to obtain information about terms, entities, relations, and events from a ground truth caption corresponding to the video; and a video captioning module including an encoder (i) to receive the information about the terms, entities, relations, and events from the textual information extraction module, and (ii) to extract video features from the video; and a decoder to generate a text caption based on the extracted video features.
United States of America as represented by the Secretary of the Air Force (USA)
Inventor
Apostolov, Zlatomir D.
Abstract
The present disclosure includes a system and method for monitoring degradation of a high temperature composite component (HTC). The HTC is defined by a volume that includes a matrix material and a fiber formed from at least one of ceramic and carbon material. One or more electrical conductors are disposed within the volume and connected directly or indirectly to a monitoring system.
United States of America as represented by the Secretary of the Air Force (USA)
Inventor
Vu, Daniel
Abstract
A mounting device that is used to suspend items in a specific location inside the cavity of a tubular structure, such as a munition, is disclosed. The mounting device includes: a pedestal for leading the insertion of the mounting device into a cavity of a munition and a skeletal frame. The skeletal frame defines an opening therein for holding an article inside the outermost portion of the skeletal frame. In some cases, the skeletal frame may have a fixed configuration. In other cases, the skeletal frame may be collapsible and expandable so that it may be inserted into a cavity of a munition having an obstruction therein. Methods of inserting and mounting an article inside an internal explosive cavity of a munition are also disclosed.
F42B 33/00 - Manufacture of ammunitionDismantling of ammunitionApparatus therefor
F42B 30/00 - Projectiles or missiles, not otherwise provided for, characterised by the ammunition class or type, e.g. by the launching apparatus or weapon used
F42B 12/36 - Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect for dispensing materialsProjectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect for producing chemical or physical reactionProjectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect for signalling
F42B 30/08 - Ordnance projectiles or missiles, e.g. shells
F42B 12/20 - Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect of high-explosive type
United States of America as represented by the Secretary of the Air Force (USA)
Inventor
Mcintire, John P.
Srnoyachki, Matthew
Abstract
The emergency egress apparatus includes a protuberance mated to a first portion of the door barricade and a keeper mated to a second portion of the door barricade. A retainer is selectively disposed between one of two positions. A first position defines the placement of the retainer that establishes an interference fit between the protuberance and the keeper. A second position defines the placement of the retainer such that it is not in contact with the protuberance or the keeper. The first position secures the first portion of the door barricaded with respect to the second portion of the door barricade, and the second position decouples the first portion of the door barricade with respect to the second portion of the door barricade.
E05C 19/18 - Portable devices specially adapted for securing wings
E05B 17/20 - Means independent of the locking mechanism for preventing unauthorised opening, e.g. for securing the bolt in the fastening position
E05C 17/08 - Devices for holding wings openDevices for limiting opening of wings or for holding wings open by a movable member extending between frame and wingBraking devices, stops or buffers, combined therewith by mechanical means with a movable bar or equivalent member extending between frame and wing with special means for release, e.g. automatic release by further opening
United States of America as represented by the Secretary of the Air Force (USA)
Inventor
Thrasher, Carl J.
Tabor, Christopher E.
Farrell, Zachary J.
Morris, Nicholas J.
Abstract
The present invention relates to core shell liquid metal encapsulates comprising multi-functional ligands, networks comprising such encapsulates and processes of making and using such encapsulates and networks. When subjected to strain, such network's conductivity is enhanced, thus allowing the network to serve as a healing agent that restores at least a portion of the conductivity in an adjacent conductor.
G06F 21/55 - Detecting local intrusion or implementing counter-measures
G06F 21/75 - Protecting specific internal or peripheral components, in which the protection of a component leads to protection of the entire computer to assure secure computing or processing of information by inhibiting the analysis of circuitry or operation, e.g. to counteract reverse engineering
H01B 1/08 - Conductors or conductive bodies characterised by the conductive materialsSelection of materials as conductors mainly consisting of other non-metallic substances oxides
H01B 1/22 - Conductive material dispersed in non-conductive organic material the conductive material comprising metals or alloys
United States of America as represented by the Secretary of the Air Force (USA)
Inventor
Overby, Kaleb D.
Gabriel, Jonathon L.
Steiner, Matthew H.
Budig, Joshua L.
Clingenpeel, Eric R
Broshkevitch, Adam T.
Anderson, Michael L
Niebuhr, Jason H.
Abstract
The present invention relates to spacecraft shielding, articles comprising such shielding as well as processes of making and using spacecraft shielding and articles comprising such shielding. Such shields are made by a 3D process that provides significant shield geometry and composition flexibility and yields shields that have significantly improved shield performance. Such shields may be efficiently be manufactured in space.
United States of America as represented by the Secretary of the Air Force (USA)
Inventor
Liu, Hsiang H.
Hardin, Iv, James O.
Berrigan, John D.
Abstract
The present invention relates to 3-D structures having high temperature stability and improved micro-porosity as well as processes of making and using same. The disclosed 3-D are advantageous because they have low densities and low permittivities. When compared to previous 3-D structures, the present structures maintain their low permittivities over a broader range of electromagnetic frequencies. Thus, when used in communication devices such as array antennas, can provided higher communication performance in high temperature environments.
B29C 64/165 - Processes of additive manufacturing using a combination of solid and fluid materials, e.g. a powder selectively bound by a liquid binder, catalyst, inhibitor or energy absorber
B33Y 70/00 - Materials specially adapted for additive manufacturing
B33Y 40/20 - Post-treatment, e.g. curing, coating or polishing
United States of America as represented by the Secretary of the Air Force (USA)
Inventor
Apostolov, Zlatomir D.
Abstract
The present disclosure includes a system and method for monitoring degradation of a high temperature composite component (HTC). The HTC is defined by a volume that includes a matrix material and a fiber formed from at least one of ceramic and carbon material. One or more electrical conductors are disposed within the volume and connected directly or indirectly to a monitoring system.
United States of America as represented by the Secretary of the Air Force (USA)
Inventor
Slocik, Joseph M
Naik, Rajesh R.
Dennis, Patrick B
Abstract
B. subtilus, Pichia pastoris; growing the cells at between 28-40° C. to achieve a desired cell density; harvesting the cells; adding a protein ionic liquid consisting of at least one of green fluorescent protein (GFP), ferritin, rabbit IgG antibodies, and photosystem II from spinach ionic liquid to the cells; suspending the cells in the protein ionic liquid; freezing the suspended cells between −20 to −212° C.; and removing at least 99% of water from the frozen suspended cells to make a cell powder. The cell powder may be reconstituted in Tris HCl buffer and mixed to obtain uniform cell suspension; and centrifuged to obtain cell pellet.
United States of America as represented by the Secretary of the Air Force (USA)
Inventor
Lentz, Joshua K
Abstract
The systems and methods provided herein are directed to a flight motion simulator. The target axes are replaced by a system of Risley pairs. Light is projected to the unit under testing at a range of angles by rotating elements within the Risley pairs.
G02B 26/08 - Optical devices or arrangements for the control of light using movable or deformable optical elements for controlling the direction of light
United States of America as represented by the Secretary of the Air Force (USA)
Inventor
Caban, Ii, Daniel Robert
Abstract
A cover for an aircraft opening or equipment formed from a collapsible material having programmable magnets encapsulated on at least one edge portion to adhere the cover to an aircraft surface is provided. The programmable magnets have a close field strength sufficient to maintain the cover in place during high winds while not damaging the aircraft surface coatings during installation and removal while not interfering with electric signals or nearby electrical equipment.
United States of America as represented by the Secretary of the Air Force (USA)
Inventor
Cumby, Brad L
Tabor, Christopher
Abstract
A deformable yet mechanically resilient microcapsule having electrical properties, a method of making the microcapsules, and a circuit component including the microcapsules. The microcapsule containing a gallium liquid metal alloy core having from about 60 to about 100 wt. % gallium and at least one alloying metal, and a polymeric shell encapsulating the liquid core, said polymeric shell having conductive properties.
H01B 1/02 - Conductors or conductive bodies characterised by the conductive materialsSelection of materials as conductors mainly consisting of metals or alloys
C22C 28/00 - Alloys based on a metal not provided for in groups
H01B 13/00 - Apparatus or processes specially adapted for manufacturing conductors or cables
80.
Method of risk-sensitive rate correction for dynamic heterogeneous networks
United States of America as represented by the Secretary of the Air Force (USA)
Inventor
Pham, Khanh Dai
Abstract
A dynamic heterogeneous network for transmitting media. The network has plural sources sending signals through various links and routers to plural destinations. Upon identifying a bottleneck link the network matches actual demand rate to actual service rate. A buffer setpoint is established to accommodate the difference between the demand rate and the service rate. The network determines an epoch having a penalty for deviation from the buffer setpoint. The rate allowance is reallocated to reduce the media bottleneck.
H04L 47/76 - Admission controlResource allocation using dynamic resource allocation, e.g. in-call renegotiation requested by the user or requested by the network in response to changing network conditions
H04L 47/129 - Avoiding congestionRecovering from congestion at the destination endpoint, e.g. reservation of terminal resources or buffer space
United States of America as represented by the Secretary of the Air Force (USA)
Inventor
Iacono, Scott T.
Friesen, Chadron M
Abstract
The present invention relates to a mechanochemical based synthesis of perfluoropyridine monomers, polymers made using such monomers and methods of making and using articles comprising such polymers. Such perfluoropyridine monomers are easily chemically tuned have the strength needed for high temperature applications and the flexibility needed for low temperature applications. In addition, to the aforementioned monomers, a mechanochemical based synthesis for such perfluoropyridine monomers is provided. All of the aforementioned performance application advantages are also found in polymers comprising Applicants' perfluoropyridine monomers.
C08G 73/06 - Polycondensates having nitrogen-containing heterocyclic rings in the main chain of the macromoleculePolyhydrazidesPolyamide acids or similar polyimide precursors
C10G 71/00 - Treatment by methods not otherwise provided for of hydrocarbon oils or fatty oils for lubricating purposes
C10M 147/04 - Monomer containing carbon, hydrogen, halogen and oxygen
C10M 169/04 - Mixtures of base-materials and additives
C10N 50/08 - Form in which the lubricant is applied to the material being lubricated solid
82.
System and method for disabling multi-rotor aircraft
United States of America as represented by the Secretary of the Air Force (USA)
Inventor
Wilmer, Adam
Jochmans, Derrick
Fleckenstein, Matthew
Westfall, James
Roberts, James
Pingel, Nicholas
Anderson, Michael
Abstract
A drone disabling device includes a plurality of streamer launch tubes having at least one streamer device positioned therein. A barrel housing is configured to hold the plurality of launch tubes within streamer launch barrels. An ignition system is configured to ignite propellant within the launch tubes and launch the streamer devices from the barrel housing such that one or more propellers of a hostile drone will become entangled and disabled. A parachute connected to the streamer device is deployed as the drone descends to protect people and property on the ground and to preserve the drone for intelligence gathering after landing.
United States of America as represented by the Secretary of the Air Force (USA)
Inventor
Sanders, Mitchell
Minkiewicz, Gregory
Abstract
An air cooled machine is formed with a housing and a plurality of heat rejecting fins with a heat pipe system disposed therein. The heat pipe system includes a primary passageway and a plurality of leg passageways extending through the housing and into each fin. A working fluid is disposed within the heat pipe system and is operable to receive heat from a heat source, change material phase at a threshold temperature and transfer the heat through the fins to a surrounding atmosphere.
F01P 3/22 - Liquid cooling characterised by evaporation and condensation of coolant in closed cyclesLiquid cooling characterised by the coolant reaching higher temperatures than normal atmospheric boiling-point
F02F 1/06 - Shape or arrangement of cooling finsFinned cylinders
B33Y 80/00 - Products made by additive manufacturing
F01P 3/02 - Arrangements for cooling cylinders or cylinder heads
84.
Method and apparatus for imaging with reduced level of off-axis artifacts
United States of America as represented by the Secretary of the Air Force (USA)
Inventor
Barnes, Ronald A
Beier, Hope T
Ibey, Bennett L
Roth, Caleb
Abstract
An acoustic imaging system responsive to an acoustic wave emitted from an object is disclosed. The system detects a deflection angle of an electromagnetic probe beam as it passes through a coupling element. The coupling element also couples the acoustic wave emitted from the object to an acoustic detector. The probe beam deflection angle is related to an angle of propagation of the acoustic wave through the coupling element. A filtering unit is configured to remove components of the signal from the acoustic detector that are outside of a range of angles, thereby improving the angular resolution of the acoustic detector. The acoustic wave may be generated by an acoustic source, such as an ultrasound transmitter, or an electromagnetic source such as a laser.
United States of America as represented by the Secretary of the Air Force (USA)
Inventor
Anderson, Michael
Appel, Grant
Bowen, Nathaniel
Briggs, Hugh
Flint, Spencer
Konig, Seth
Leslie, Erin
Abstract
A method of establishing a system for gathering surveillance data in a hostile environment. The method comprises the steps of providing a movable tractor for ground hauling a trailer, and providing a drone which can be operated independently from the tractor. The trailer has a floor pan for supporting a relay sensor dispensing mechanism and a platform above the floor pan, with a hole for dispensing relay sensors therethrough. The relay sensor dispensing mechanism has an elevator for holding a stockpile of relay sensors, and elevating the relay sensors through the hole. The method comprises disposing at least one relay sensor in the elevator, elevating the relay sensor to a pickup position at or above the platform and retrieving the relay sensor with a drone for subsequent deposition in the hostile environment. The relay sensor then gathers and transceives surveillance data for use and interpretation by an operator. Optional a conveyor chute may replenish the elevator when it is depleted of relay sensors.
B60P 1/10 - Vehicles predominantly for transporting loads and modified to facilitate loading, consolidating the load, or unloading with a tipping movement of load supporting or containing element actuated by mechanical gearing only with screw and nut
B60P 1/38 - Vehicles predominantly for transporting loads and modified to facilitate loading, consolidating the load, or unloading using endless chains or belts thereon forming the main load supporting or containing element or part thereof
B64C 39/02 - Aircraft not otherwise provided for characterised by special use
G05D 1/00 - Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
B64U 101/60 - UAVs specially adapted for particular uses or applications for transporting passengersUAVs specially adapted for particular uses or applications for transporting goods other than weapons
86.
Microfluidic flow process for making linear polymers
United States of America as represented by the Secretary of the Air Force (USA)
Inventor
Ghiassi, Kamran B.
Redeker, Neil D.
Abstract
The present invention relates to a microfluidic flow process for making polymers, polymers made by such processes, and methods of using such polymers. In such process, a novel reagent delivery setup is used in conjunction with microfluidic reaction technology to synthesize anionic polymerization reaction products from superheated monomer orders of magnitude faster than is possible in batch and continuous syntheses. The aforementioned process does not require the cryogenic temperatures which are required for such syntheses in batch or bulk continuous. Thus the aforementioned process is more economically efficient and reduces the environmental impact of linear polymer production.
United States of America as represented by the Secretary of the Air Force (USA)
Inventor
Turgut, Zafer
Abstract
A unique rotor assembly for an electrical machine is disclosed herein. The rotor assembly includes a shaft having an axis of rotation extending within the electrical machine. A central support is connected to the shaft at an intermediate position and a pair of opposing end plates are configured to clamp a plurality of laminate plates therebetween. The laminate plates and a sidewall of the end plates have a non-linear cross-sectional shape such that radial loading due to centrifugal force is transmitted from the laminate plates to the end plates during operation.
H02K 15/03 - Processes or apparatus specially adapted for manufacturing, assembling, maintaining or repairing of dynamo-electric machines of stator or rotor bodies having permanent magnets
H02K 1/2781 - Magnets shaped to vary the mechanical air gap between the magnets and the stator
United States of America as represented by the Secretary of the Air Force (USA)
Inventor
Posada, Natalia
Abstract
A portable tracer fluid injection system. The system has a vapor cloud generator which vaporizes a vapor cloud generating liquid. The vapor cloud generator is uses a sub-ohm resistive heater to vaporize small volumes of the vapor cloud generating liquid, allowing for a relatively small tracer fluid injection system. This system has the benefit of being able to target specific regions of a test object within a wind tunnel and being usable for different positions within the test section of a wind tunnel.
United States of America as represented by the Secretary of the Air Force (USA)
Inventor
Schroer, Thorsten G.
Lecroy, Gregory E.
Aguila, Miguel
Rodriguez, Mayra R.
Downard, Tyler J.
Macleod, Brianna L.
Abstract
pumping a solution comprising a compound of Formula I
performing oxidative addition to create a geminal dipseudohalide or halide-pseudohalide compound of the general Formula II
C25B 9/19 - Cells comprising dimensionally-stable non-movable electrodesAssemblies of constructional parts thereof with diaphragms
C25B 11/091 - Electrodes formed of electrocatalysts on a substrate or carrier characterised by the electrocatalysts material consisting of at least one catalytic element and at least one catalytic compoundElectrodes formed of electrocatalysts on a substrate or carrier characterised by the electrocatalysts material consisting of two or more catalytic elements or catalytic compounds
United States of America as represented by the Secretary of the Air Force (USA)
Inventor
Anderson, Michael
Appel, Grant
Bowen, Nathaniel
Briggs, Hugh
Flint, Spencer
Konig, Seth
Leslie, Erin
Abstract
A system for sending surveillance signals from a hostile environment to an operator. The system comprises an operably movable tractor for ground hauling a trailer and an independently operable drone. The trailer has an actuatable elevator for holding a stockpile of relay sensors and comprising a pair of co-acting elevator belts defining a chute therebetween. The elevator holds a stack of relay sensors for elevation to a pickup-position by the drone. Optionally a conveyor chute may replenish the stack of relay sensors in the elevator.
United States of America as represented by the Secretary of the Air Force (USA)
Inventor
Anderson, Michael L.
Froembling, Zachary
Teope, Kaz I.
Abstract
A system, method and apparatus for unfolding and folding a multi-arm device that includes a support member and an actuator. A first arm is coupled to the actuator and extends from a folded position to an unfolded position upon actuation of the actuator. A second arm is coupled to the actuator and moves from a folded position to an unfolded position upon actuation of a linkage that causes the second arm to rotate. A third arm moves from a folded position to an unfolded position, via an elbow joint, upon release of a tether attached to the third arm.
F16M 13/02 - Other supports for positioning apparatus or articlesMeans for steadying hand-held apparatus or articles for supporting on, or attaching to, an object, e.g. tree, gate, window-frame, cycle
B64C 1/30 - Parts of fuselage relatively movable to reduce overall dimensions of aircraft
F16H 25/22 - Screw mechanisms with balls, rollers, or similar members between the co-operating partsElements essential to the use of such members
F15B 15/14 - Fluid-actuated devices for displacing a member from one position to anotherGearing associated therewith characterised by the construction of the motor unit of the straight-cylinder type
United States of America as represented by the Secretary of the Air Force (USA)
Inventor
Mahoney, Clare M.
Vaia, Richard A.
Park, Kyoungweon
Abstract
The present invention relates to processes for selective reshaping of nanoparticles in three dimensional articles, three dimensional articles produced by such processes, and methods of using such three dimensional articles. As a result of the aforementioned process, such three dimensional articles can have selective tuning that arises, at least in part, from the reshaped nanoparticles found in such articles. Such tuning provides the aforementioned articles with superior performance that can be advantageous in the areas including such as optical filters, multi-functional composites and sensing elements.
C09D 11/037 - Printing inks characterised by features other than the chemical nature of the binder characterised by the pigment
C09D 11/107 - Printing inks based on artificial resins containing macromolecular compounds obtained by reactions only involving carbon-to-carbon unsaturated bonds from unsaturated acids or derivatives thereof
B33Y 70/00 - Materials specially adapted for additive manufacturing
B29C 35/08 - Heating or curing, e.g. crosslinking or vulcanising by wave energy or particle radiation
C09D 11/101 - Inks specially adapted for printing processes involving curing by wave energy or particle radiation, e.g. with UV-curing following the printing
C09D 11/106 - Printing inks based on artificial resins containing macromolecular compounds obtained by reactions only involving carbon-to-carbon unsaturated bonds
B33Y 80/00 - Products made by additive manufacturing
United States of America as represented by the Secretary of the Air Force (USA)
Inventor
Fowler, Eric
Hayes, Michael
Eversley, Kevin
Abstract
An ergonomic method for working in confined work spaces is disclosed. The method, in some cases, includes the steps of: a) providing a support structure that is generally in the configuration of a rectangular prism having six faces, a length, width, and a height in which the length, width, and height differ from one another so that the structure provides three different height positions when the support structure is placed on the floor of the workspace; b) placing the support structure with one of its faces in contact with a contoured floor surface in a confined work space; and c) sitting or standing on the support structure.
A47C 5/12 - Chairs of special materials of plastics, with or without reinforcement
A47C 3/16 - Chairs characterised by structural featuresChairs or stools with rotatable or vertically-adjustable seats of legless type, e.g. with seat directly resting on the floorHassocksPouffes
United States of America as represented by the Secretary of the Air Force (USA)
Inventor
Rondeau, Christopher M.
Temple, Michael A.
Lopez, Jr., Juan
Betances, J. Addison
Abstract
A method for cyber security monitor includes monitoring a network interface that is input-only configured to surreptitiously and covertly receive bit-level, physical layer communication between networked control and sensor field devices. During a training mode, a baseline distinct native attribute (DNA) fingerprint is generated for each networked field device. During a protection mode, a current DNA fingerprint is generated for each networked field device. The current DNA fingerprint is compared to the baseline DNA fingerprint for each networked field device. In response to detect at least one of RAA and PAA based on a change in the current DNA fingerprint to the baseline DNA fingerprint of one or more networked field devices, an alert is transmitted, via an external security engine interface to an external security engine.
United States of America as represented by the Secretary of the Air Force (USA)
Inventor
Mann, James M.
Bowen, Thomas A.
Hunt, Eric M.
Abstract
3 has a sufficient crystal size to be characterized and used in the fields of neutron detection, radiation-hardened electronics, nuclear forensics, nuclear engineering photovoltaics, lasers, light-emitting diodes, photoelectrolysis and magnetic applications.
C30B 7/10 - Single-crystal growth from solutions using solvents which are liquid at normal temperature, e.g. aqueous solutions by application of pressure, e.g. hydrothermal processes
C01F 17/32 - Compounds containing rare earth metals and at least one element other than a rare earth metal, oxygen or hydrogen, e.g. La4S3Br6 oxide or hydroxide being the only anion, e.g. NaCeO2 or MgxCayEuO
United States of America as represented by the Secretary of the Air Force (USA)
Inventor
Gillaugh, Daniel
Kaszynski, Alexander
Brown, Jeffrey
Abstract
The present disclosure is directed to a method and system to develop finite element (FE) models of as-manufactured turbomachinery blades using a combination of optical topography measurements, mesh morphing and strain gauge measurements. The method and system improves strain gauge to blade tip timing correlation using as-manufactured blade dimensions with finite element modeling.
G01M 15/14 - Testing gas-turbine engines or jet-propulsion engines
G01B 11/26 - Measuring arrangements characterised by the use of optical techniques for measuring angles or tapersMeasuring arrangements characterised by the use of optical techniques for testing the alignment of axes
G01L 1/22 - Measuring force or stress, in general by measuring variations in ohmic resistance of solid materials or of electrically-conductive fluidsMeasuring force or stress, in general by making use of electrokinetic cells, i.e. liquid-containing cells wherein an electrical potential is produced or varied upon the application of stress using resistance strain gauges
G01B 11/06 - Measuring arrangements characterised by the use of optical techniques for measuring length, width, or thickness for measuring thickness
97.
Optimized heteroepitaxial growth of semiconductors
United States of America as represented by the Secretary of the Air Force (USA)
Inventor
Tassev, Vladimir
Abstract
3 (ammonia), and HF (hydrogen fluoride); flowing the carrier gas over the Group II/III element; exposing the substrate to the ternary-forming gasses in a predetermined ratio of first ternary-forming gas to second ternary-forming gas (1tf:2tf ratio); and changing the 1tf:2tf ratio over time.
United States of America as represented by the Secretary of the Air Force (USA)
Inventor
Kiser, Brett
Abstract
An aircraft loading system is configured to tether equipment within an aircraft. The loading system has a wedge shaped bracket that has a front plate joined to two side plates and a bottom plate. A middle plate is parallel to the front plate and joins the two side plates. A front opening is arranged through the bottom plate between the front plate and the middle plate. The front opening is configured to accommodate an attachment ring. The attachment ring is used to tether the equipment within the aircraft.
United States of America as represented by the Secretary of the Air Force (USA)
Inventor
Prentice, David C
Abstract
Various embodiments comprise systems, mechanisms, methods and apparatus configured to regenerate or recreate a stream of substantially continuous serial bus data traffic using stored data packet sequences representing captured energy associated with inverting and non-inverting communication lines of a differential transmission line type of serial bus (e.g., RS-422, MIL STD 1553, and the like).
United States of America as represented by the Secretary of the Air Force (USA)
Inventor
Tassev, Vladimir
Vangala, Shivashankar
Tomich, David H
Abstract
3 (sapphire), silicon (Si), germanium (Ge), GaAs, GaP, GaSb, InAs, InP, CdTe, CdS, CdSe, or GaSe. The first material deposited on the common substrate may be one or more electronic or optical binary materials from the group consisting of AlN, GaN, GaP, InP, GaAs, InAs, AlAs, ZnSe, GaSe, ZnTe, CdTe, HgTe, GaSb, SiC, CdS, CdSe, or their ternaries or quaternaries. The far-from-equilibrium process is one of MOCVD and MBE, and the close-to-equilibrium process is HVPE.