Abrégé

A ram-air parachute system is presented. The system may include upper and lower airfoil surface members and one or more proximal wall members, distal wall members, interior wall members, and proximal-facing air inlets. The proximal-facing air inlets may be defined between the interior wall members and the upper and lower airfoil surface members. One or more edge airfoils may be defined between the proximal wall members and at least a portion of the upper airfoil surface member, the lower airfoil surface member and the distal wall member(s). The edge airfoils may be in fluidic communication with the proximal-facing air inlet such that air may flow into the edge airfoils via the proximal-facing air inlet and inflate the edge airfoils. Inflation of the edge airfoils may vertically expand the parachute system, increasing a vertical distance between the upper and lower airfoil surface members.

Classes IPC  ?

• B64D 17/02 - Disposition ou structure de la coupole

Produits et services

Business project management services; Business consultation in the field of business process improvement

Produits et services

Apparatus for energy storage, namely, energy storage systems comprised of electrical storage batteries, electrical inductors and magnets

Abrégé

A system and method for transient satellite doppler signal position determination to receive measured signals associated with respective satellites, determine transmission characteristics from the measured signals, determine orbital characteristics of the satellites from the measured signals responsive to indications of the current time via Doppler calculations, identify the satellites responsive to the transmission characteristics and/or and the orbital characteristics, determine a current position of the satellites relative to the system from the Doppler calculations and identifying the satellites, and determine a geolocation of the system responsive to the current position of the satellites relative to the system.

Classes IPC  ?

• G01S 5/02 - Localisation par coordination de plusieurs déterminations de direction ou de ligne de positionLocalisation par coordination de plusieurs déterminations de distance utilisant les ondes radioélectriques
• G01S 5/10 - Position du récepteur obtenue par coordination de plusieurs lignes de position définies par des mesures de différence de parcours

Abrégé

A system and method for transient satellite doppler signal position determination by receiving multiple measured signals, determining transmission characteristics for those signals, determining orbital characteristics of satellites associated with those signals via a Doppler calculation, identifying the satellites from the transmission and orbital characteristics, determining a closest approach point responsive to identifying the satellites and the Doppler calculations, determining current positions of the satellites relative to the receiver from the closest approach point determinations via comparison to an orbital location-defining modeling equation associated with the first satellite, and determining a geolocation of the receiver responsive to each of the current position of the satellites relative to the receiver.

Classes IPC  ?

• G01S 5/02 - Localisation par coordination de plusieurs déterminations de direction ou de ligne de positionLocalisation par coordination de plusieurs déterminations de distance utilisant les ondes radioélectriques
• G01S 5/10 - Position du récepteur obtenue par coordination de plusieurs lignes de position définies par des mesures de différence de parcours

Abrégé

An energy storage apparatus including a spherical rotating member having permanent magnets and uniquely-identifiable location-defining elements, a plurality of coils, a controller operably coupled to the plurality of coils, a power source, and a location sensing apparatus operable to detect the plurality of location-defining elements. The controller may compare time-sequential information from the location sensing apparatus to determine a rotational axis and a rotational speed of the rotating member, operate the coils to change the rotational axis speed of the rotating member, increase energy stored by the rotating member by increasing the rotational speed by operating the coils to generate magnetic fields that interact with the permanent magnets, and withdraw energy by operating the coils to generate magnetic fields that interact with the magnetic fields of the permanent magnets to produce induced current in the coils and directing the induced current to a power delivery location.

Classes IPC  ?

• H02K 7/02 - Masses additionnelles pour augmenter l'inertie, p. ex. volants
• B60K 6/10 - Les moteurs primaires comportant des moteurs à combustion et des moyens d'accumulation d'énergie mécanique ou fluide au moyen d'un accumulateur mécanique rechargeable, p. ex. d'un volant
• B62D 37/06 - Stabilisation des caisses de véhicules sans agir sur les dispositifs de suspension au moyen de masses mobiles en utilisant des gyroscopes
• B64G 1/40 - Aménagements ou adaptations des systèmes de propulsion
• B63H 21/12 - Aménagements de l'appareil moteur de propulsion ou de certains de ses éléments pour utilisation à bord des navires le navire étant actionné par moteurs
• B64D 27/24 - Aéronefs caractérisés par le type ou la position des groupes moteurs utilisant la vapeur ou l'énergie de ressorts

Produits et services

Business project management services; business consultation in the field of business process improvement

Abrégé

A propeller system including a propeller including a central attachment member and a plurality of blade apparatuses, each including a blade body attached to the central attachment member and a magnetic coupling member attached to a radially outward end of the blade body. The propeller system further comprises a propeller frame configured to at least partially circumscribe the magnetic coupling member of each blade apparatus and a plurality of electromagnets positioned on the propeller frame and operable to generate magnetic fields to suspend the magnetic coupling members, laterally translate the magnetic coupling members, rotate the magnetic coupling members along the radial axis of the propeller system, thereby rotating the blade bodies.

Classes IPC  ?

• B64C 11/44 - Mécanismes de changement de pas des pales électriques
• B64C 11/06 - Montage des pales dans le cas de pales à pas variable

Abrégé

A propeller system with directional thrust control comprising a hub, a plurality of blade attachment apparatuses attached to the hub, and a plurality of blades, each blade of the plurality of blades being attached to a blade attachment apparatus of the plurality of blade attachment apparatuses. The hub is operable to rotate about a rotation axis thereof. The plurality of blades is attached to the hub via the plurality of blade attachment apparatuses such that the plurality of blades rotates about the rotation axis of the hub when the hub rotates about the rotation axis thereof. Each blade attachment apparatus of the plurality of blade attachment apparatuses is operable to rotate the blade attached thereto about a blade rotation axis.

Classes IPC  ?

• B64C 11/44 - Mécanismes de changement de pas des pales électriques
• B64C 11/48 - Ensembles de plusieurs hélices coaxiales
• B64C 11/06 - Montage des pales dans le cas de pales à pas variable
• B64C 15/02 - Commande de l'assiette, de la direction du vol ou de l'altitude par jets réactifs les jets étant des jets propulsifs
• B64C 11/32 - Mécanismes de changement de pas des pales mécaniques
• B64C 39/02 - Aéronefs non prévus ailleurs caractérisés par un emploi spécial

Produits et services

Project management services for others for business purposes in the fields of architecture, interior design, urban planning design; management of customer appreciation programs of others; business management consultancy featuring the analysis and the implementation of strategy plans for management projects