All.space Networks Limited

United Kingdom

Back to Profile

1-49 of 49 for All.space Networks Limited Sort by
Query
Aggregations
IP Type
        Patent 36
        Trademark 13
Jurisdiction
        United States 37
        World 8
        Canada 2
        Europe 2
Date
2025 June 1
2025 (YTD) 8
2024 5
2023 17
2022 6
See more
IPC Class
H01Q 25/00 - Antennas or antenna systems providing at least two radiating patterns 14
H01Q 1/24 - SupportsMounting means by structural association with other equipment or articles with receiving set 12
H01Q 19/06 - Combinations of primary active antenna elements and units with secondary devices, e.g. with quasi-optical devices, for giving the antenna a desired directional characteristic using refracting or diffracting devices, e.g. lens 12
H04B 7/185 - Space-based or airborne stations 8
H01Q 21/00 - Antenna arrays or systems 7
See more
NICE Class
09 - Scientific and electric apparatus and instruments 13
38 - Telecommunications services 9
Status
Pending 15
Registered / In Force 34

1.

ISOTROPIC 3D-PRINTED GRADIENT-INDEX RF LENS

      
Application Number 18974078
Status Pending
Filing Date 2024-12-09
First Publication Date 2025-07-31
Owner All.Space Networks Limited (United Kingdom)
Inventor
  • Turpin, Jeremiah P.
  • Bouhanna, Zakaria
  • Finney, John
  • Dinc, Ergin

Abstract

Inhomogeneous dielectric lenses for electromagnetic waves can be produced by a process such as 3D printing to have controllable dielectric values. Dielectric values can be produced by a varying density of air voids within, for example, a dielectric matrix to obtain an effective overall density. Approaches in accordance with various embodiments can obtain uniform, isotropic dielectric properties without resonant behavior by the use of aperiodic distributions of nonuniformly-sized air voids. Target air fraction and distribution of air voids can be specified by a target dielectric constant through dielectric mixing rules, such as Maxwell-Garnet mixing rules, and a requirement for locally uniform distributions of air voids, while varying the density of the air voids across the overall structure to produce a desired gradient of dielectric properties.

IPC Classes  ?

  • H01Q 15/08 - Refracting or diffracting devices, e.g. lens, prism formed of solid dielectric material
  • B29D 11/00 - Producing optical elements, e.g. lenses or prisms
  • B33Y 10/00 - Processes of additive manufacturing
  • B33Y 80/00 - Products made by additive manufacturing
  • H01Q 15/02 - Refracting or diffracting devices, e.g. lens, prism

2.

LENS ANTENNA SYSTEM

      
Application Number 18909922
Status Pending
Filing Date 2024-10-08
First Publication Date 2025-06-05
Owner All.Space Networks Limited (United Kingdom)
Inventor
  • Scarborough, Clinton P.
  • Turpin, Jeremiah P.
  • Difonzo, Daniel F.
  • Finney, John

Abstract

An antenna system that includes a plurality of lens sets. Each lens set includes a lens and at least one feed element. At least one feed element is aligned with the lens and configured to direct a signal through the lens at a desired direction.

IPC Classes  ?

  • H01Q 3/46 - Active lenses or reflecting arrays
  • H01Q 1/24 - SupportsMounting means by structural association with other equipment or articles with receiving set
  • H01Q 1/28 - Adaptation for use in or on aircraft, missiles, satellites, or balloons
  • H01Q 3/14 - Arrangements for changing or varying the orientation or the shape of the directional pattern of the waves radiated from an antenna or antenna system using mechanical relative movement between primary active elements and secondary devices of antennas or antenna systems for varying the relative position of primary active element and a refracting or diffracting device
  • H01Q 3/24 - Arrangements for changing or varying the orientation or the shape of the directional pattern of the waves radiated from an antenna or antenna system varying the orientation by switching energy from one active radiating element to another, e.g. for beam switching
  • H01Q 3/30 - Arrangements for changing or varying the orientation or the shape of the directional pattern of the waves radiated from an antenna or antenna system varying the relative phase or relative amplitude of energisation between two or more active radiating elementsArrangements for changing or varying the orientation or the shape of the directional pattern of the waves radiated from an antenna or antenna system varying the distribution of energy across a radiating aperture varying the phase
  • H01Q 19/06 - Combinations of primary active antenna elements and units with secondary devices, e.g. with quasi-optical devices, for giving the antenna a desired directional characteristic using refracting or diffracting devices, e.g. lens
  • H01Q 21/00 - Antenna arrays or systems
  • H01Q 21/06 - Arrays of individually energised antenna units similarly polarised and spaced apart
  • H01Q 21/22 - Antenna units of the array energised non-uniformly in amplitude or phase, e.g. tapered array or binomial array
  • H01Q 25/00 - Antennas or antenna systems providing at least two radiating patterns

3.

HYDRA

      
Application Number 1851370
Status Registered
Filing Date 2025-02-20
Registration Date 2025-02-20
Owner ALL.SPACE NETWORKS LIMITED (United Kingdom)
NICE Classes  ?
  • 09 - Scientific and electric apparatus and instruments
  • 38 - Telecommunications services

Goods & Services

Communication platform terminals; communication platform terminals providing concurrent access to satellite and terrestrial networks; communications terminal for simultaneous multi-satellite multi-orbit connectivity; communication equipment namely multi-network service enabled platform terminals; communication equipment namely multi-orbit antenna; communication terminal equipment, namely electronically steered antenna for switching between different orbits and terrestrial networks; communication terminal equipment namely optical lenses, optical lens arrays, radio frequency lenses, microwave lenses; data transmitters for use in satellite and terrestrial communication platform terminals; data communication equipment and apparatus; downloadable computer software for use in data collection and transmission for satellite and terrestrial communication terminals. Telecommunication services; operation of satellite to earth receiver and transmitter aerials; communications consultation services.

4.

FIELD-ASSEMBLED MODULAR PHASED ARRAY SATCOM TERMINAL

      
Application Number 18671016
Status Pending
Filing Date 2024-05-22
First Publication Date 2025-04-24
Owner All.Space Networks Limited (United Kingdom)
Inventor
  • Turpin, Jeremiah P.
  • Billman, Brian Murphy
  • Finney, John

Abstract

A field-assembled satellite communications terminal has a plurality of discrete, modular aperture blocks. Each aperture block contains an electrically steered antenna aperture, and a plurality of interconnection ports for power and data communications between the plurality of aperture blocks. The plurality of interconnection ports are removably connectable by the end user in the field. The terminal further has a signal processing system for receiving, processing, and generating signals to and from the apertures. The aperture blocks are connected to each other in the field and self-configure to form an electrically-steered antenna.

IPC Classes  ?

  • H01Q 3/26 - Arrangements for changing or varying the orientation or the shape of the directional pattern of the waves radiated from an antenna or antenna system varying the relative phase or relative amplitude of energisation between two or more active radiating elementsArrangements for changing or varying the orientation or the shape of the directional pattern of the waves radiated from an antenna or antenna system varying the distribution of energy across a radiating aperture
  • H01Q 3/38 - Arrangements for changing or varying the orientation or the shape of the directional pattern of the waves radiated from an antenna or antenna system varying the relative phase or relative amplitude of energisation between two or more active radiating elementsArrangements for changing or varying the orientation or the shape of the directional pattern of the waves radiated from an antenna or antenna system varying the distribution of energy across a radiating aperture varying the phase by electrical means with variable phase-shifters the phase-shifters being digital
  • H04B 10/118 - Arrangements specific to free-space transmission, i.e. transmission through air or vacuum specially adapted for satellite communication
  • H04B 17/12 - MonitoringTesting of transmitters for calibration of transmit antennas, e.g. of amplitude or phase
  • H04B 17/21 - MonitoringTesting of receivers for calibrationMonitoringTesting of receivers for correcting measurements
  • H04B 17/27 - MonitoringTesting of receivers for locating or positioning the transmitter

5.

HIGH-GAIN MULTIBEAM GNSS ANTENNA

      
Application Number 18731138
Status Pending
Filing Date 2024-05-31
First Publication Date 2025-04-24
Owner All.Space Networks Limited (United Kingdom)
Inventor
  • Zavrel, Robert J.
  • Turpin, Jeremiah P.
  • Finney, John

Abstract

A multibeam Radio Frequency (RF) lens antenna is designed as a receiver for Global Navigation Satellite System (GNSS) applications, such as GPS (Global Positioning System), Galileo, GLONASS, COMPASS, and others. The RF lens and plurality of associated feed elements and receiver circuits combine to form a plurality of resulting high-gain relatively narrow beams that, taken together, allow reception of signals from GNSS satellites over the entire upper hemisphere. Any kind of RF lens can be used, where the lens can be of homogeneous or inhomogeneous, dielectric or metamaterial/metasurface construction. The benefit of this approach to build a GNSS receiver over existing alternatives is increased gain and decreased noise at each receiver, which improves the signal to noise ratio (SNR) and improves the accuracy and reliability of the position and time measurements, while also reducing the impact of, and sensitivity to, interference, jamming, and spoofing signals. The approaches described in this patent can be combined with existing signal processing and accuracy improvement methods (such as Real-Time Kinematic (RTK), Precise-Point Positioning (PPP), and Differential GPS (DGPS)) for further benefits. This system has applications within the surveying, maritime, land mobility, aerospace, and government positioning market areas.

IPC Classes  ?

  • G01S 19/21 - Interference related issues
  • G01S 19/14 - Receivers specially adapted for specific applications
  • G01S 19/23 - Testing, monitoring, correcting or calibrating of a receiver element
  • G01S 19/37 - Hardware or software details of the signal processing chain
  • H01Q 1/24 - SupportsMounting means by structural association with other equipment or articles with receiving set

6.

HYDRA

      
Serial Number 79422323
Status Pending
Filing Date 2025-02-20
Owner ALL.SPACE NETWORKS LIMITED (United Kingdom)
NICE Classes  ?
  • 38 - Telecommunications services
  • 09 - Scientific and electric apparatus and instruments

Goods & Services

Telecommunication services; operation of satellite to earth receiver and transmitter aerials; communications consultation services. Communication platform terminals; communication platform terminals providing concurrent access to satellite and terrestrial networks; communications terminal for simultaneous multi-satellite multi-orbit connectivity; communication equipment namely multi-network service enabled platform terminals; communication equipment namely multi-orbit antenna; communication terminal equipment, namely electronically steered antenna for switching between different orbits and terrestrial networks; communication terminal equipment namely optical lenses, optical lens arrays, radio frequency lenses, microwave lenses; data transmitters for use in satellite and terrestrial communication platform terminals; data communication equipment and apparatus; downloadable computer software for use in data collection and transmission for satellite and terrestrial communication terminals.

7.

Satellite communication terminal

      
Application Number 29883402
Grant Number D1061489
Status In Force
Filing Date 2023-01-27
First Publication Date 2025-02-11
Grant Date 2025-02-11
Owner All.Space Networks Limited (United Kingdom)
Inventor
  • Sutcliffe, Harry
  • Hutchison, Hutch
  • Oakey, Ryan

8.

MULTI-BEAM ANTENNA ARRAY

      
Application Number 18696763
Status Pending
Filing Date 2022-09-20
First Publication Date 2025-01-30
Owner All.Space Networks Limited (United Kingdom)
Inventor
  • Szczepanik, John-Paul
  • Keeton, Richard
  • Sharma, Vikas
  • Papaioannou, Maria
  • De Jager, Derek
  • Al-Taei, Sarmad
  • Savage, Kevin
  • Candotti, Massimo
  • Willmott, Lan
  • Long, Nicholas Leonard
  • Turpin, Jeremiah P.
  • Finney, John

Abstract

There is disclosed a multi-beam antenna array, comprising a main array of antenna modules, each antenna module comprising a plurality M of individually-steerable antenna elements. The antenna modules are arranged in the main array with N-fold rotational symmetry, the antenna elements are arranged within each module with M-fold rotational symmetry, and each antenna element comprises a sub-array of radiating elements.

IPC Classes  ?

  • H01Q 21/00 - Antenna arrays or systems
  • H01Q 19/06 - Combinations of primary active antenna elements and units with secondary devices, e.g. with quasi-optical devices, for giving the antenna a desired directional characteristic using refracting or diffracting devices, e.g. lens
  • H01Q 21/20 - Arrays of individually energised antenna units similarly polarised and spaced apart the units being spaced along, or adjacent to, a curvilinear path
  • H01Q 25/00 - Antennas or antenna systems providing at least two radiating patterns

9.

PRISM FOR REPOINTING REFLECTOR ANTENNA MAIN BEAM

      
Application Number 18536580
Status Pending
Filing Date 2023-12-12
First Publication Date 2024-04-18
Owner All.Space Networks Limited (United Kingdom)
Inventor
  • Turpin, Jeremiah P.
  • Finney, John

Abstract

A microwave prism is used to repoint an operational Direct-to-Home (DTH) or Very Small Aperture Terminal (VSAT) reflector antenna as part of a ground terminal to receive (or transmit) signals from a different satellite or orbital position without physically moving the reflector or the feed horn antenna. The microwave prism operates by shifting the radiated fields from the horn antenna generally perpendicular to the focal axis of the parabolic reflector in order to cause the main beam of the reflector to scan in response. For an existing reflector antenna receiving signals from an incumbent satellite, a prism has been designed to be snapped into place over the feed horn and shift the fields laterally by a calibrated distance. The structure of the prism is designed to be positioned and oriented correctly without the use of skilled labor. This system allows a satellite service provider to repoint their subscribers to a new satellite by shipping a self-install kit of the prism that is pre-configured to have the correct orientation and position on the feed antenna to correctly re-point the beam at a different satellite once the prism is applied. One benefit of the system is that unskilled labor, i.e., the subscribers themselves, can be used to repoint a large number of subscriber antennas in a satellite network rather than requiring the cost of a truck roll and a technician to visit every site. The microwave prisms to implement this functionality can be constructed in different ways, with homogeneous slabs or blocks, Gradient-Index (GRIN), multi-layered dielectric, geometric or graded-index Fresnel-zone, metasurface, or metamaterial prisms. The geometric and electrical constraints of the design are determined by the incumbent and target satellites, and the ground terminal location.

IPC Classes  ?

  • H01Q 19/13 - Combinations of primary active antenna elements and units with secondary devices, e.g. with quasi-optical devices, for giving the antenna a desired directional characteristic using reflecting surfaces wherein the surfaces are concave the primary radiating source being a single radiating element, e.g. a dipole, a slot, a waveguide termination
  • H01Q 1/24 - SupportsMounting means by structural association with other equipment or articles with receiving set
  • H01Q 3/08 - Arrangements for changing or varying the orientation or the shape of the directional pattern of the waves radiated from an antenna or antenna system using mechanical movement of antenna or antenna system as a whole for varying two co-ordinates of the orientation
  • H01Q 3/20 - Arrangements for changing or varying the orientation or the shape of the directional pattern of the waves radiated from an antenna or antenna system using mechanical relative movement between primary active elements and secondary devices of antennas or antenna systems for varying relative position of primary active element and a reflecting device wherein the primary active element is fixed and the reflecting device is movable
  • H01Q 5/55 - Feeding or matching arrangements for broad-band or multi-band operation for horn or waveguide antennas
  • H01Q 15/04 - Refracting or diffracting devices, e.g. lens, prism comprising wave-guiding channel or channels bounded by effective conductive surfaces substantially perpendicular to the electric vector of the wave, e.g. parallel-plate waveguide lens
  • H01Q 15/16 - Reflecting surfacesEquivalent structures curved in two dimensions, e.g. paraboloidal
  • H01Q 19/19 - Combinations of primary active antenna elements and units with secondary devices, e.g. with quasi-optical devices, for giving the antenna a desired directional characteristic using reflecting surfaces having two or more spaced reflecting surfaces comprising one main concave reflecting surface associated with an auxiliary reflecting surface
  • H04B 7/185 - Space-based or airborne stations

10.

CIRCUIT AND SYSTEM APPARATUS FOR SYNTHESIZING ONE OR MULTIPLE BEAMS ON A SWITCHED-FEED ANTENNA

      
Application Number 18516684
Status Pending
Filing Date 2023-11-21
First Publication Date 2024-03-14
Owner All.Space Networks Limited (United Kingdom)
Inventor
  • Diebold, Sebastian
  • Sharma, Vikas
  • Billman, Brian Murphy
  • Turpin, Jeremiah P.

Abstract

A circuit has at least one amplifier and a signal routing device such as one or more switches, and an array of antenna elements from which some subset must be enabled and processed at a time. The antenna elements can be grouped in accordance with an organization scheme (e.g., rows, columns) to enable more flexibility in selecting and routing the signals. The system is used to create one or more beams, which can be pointed (steered) to a wide range of directions by means of selecting one or more feed antennas in a switched-feed antenna without including full receive and transmit circuitry (DSP, frequency conversion) for each feed in the array. In this case, minimizing the number of DSP chains is desirable to reduce the cost, power, and complexity of the antenna. The resulting beam(s) can be combined and manipulated to support multiple users, track several targets, increase operational range, increase radar resolution, or data-rate in communications.

IPC Classes  ?

  • H01Q 3/26 - Arrangements for changing or varying the orientation or the shape of the directional pattern of the waves radiated from an antenna or antenna system varying the relative phase or relative amplitude of energisation between two or more active radiating elementsArrangements for changing or varying the orientation or the shape of the directional pattern of the waves radiated from an antenna or antenna system varying the distribution of energy across a radiating aperture
  • H01Q 3/36 - Arrangements for changing or varying the orientation or the shape of the directional pattern of the waves radiated from an antenna or antenna system varying the relative phase or relative amplitude of energisation between two or more active radiating elementsArrangements for changing or varying the orientation or the shape of the directional pattern of the waves radiated from an antenna or antenna system varying the distribution of energy across a radiating aperture varying the phase by electrical means with variable phase-shifters
  • H04B 1/16 - Circuits
  • H04B 7/0426 - Power distribution

11.

LENS ANTENNA SYSTEM

      
Application Number 18498013
Status Pending
Filing Date 2023-10-30
First Publication Date 2024-03-07
Owner All.Space Networks Limited (United Kingdom)
Inventor
  • Scarborough, Clinton P.
  • Turpin, Jeremiah P.
  • Difonzo, Daniel F.
  • Finney, John

Abstract

An antenna system that includes a plurality of lens sets. Each lens set includes a lens and at least one feed element. At least one feed element is aligned with the lens and configured to direct a signal through the lens at a desired direction.

IPC Classes  ?

  • H01Q 3/46 - Active lenses or reflecting arrays
  • H01Q 1/28 - Adaptation for use in or on aircraft, missiles, satellites, or balloons
  • H01Q 3/14 - Arrangements for changing or varying the orientation or the shape of the directional pattern of the waves radiated from an antenna or antenna system using mechanical relative movement between primary active elements and secondary devices of antennas or antenna systems for varying the relative position of primary active element and a refracting or diffracting device
  • H01Q 3/24 - Arrangements for changing or varying the orientation or the shape of the directional pattern of the waves radiated from an antenna or antenna system varying the orientation by switching energy from one active radiating element to another, e.g. for beam switching
  • H01Q 3/30 - Arrangements for changing or varying the orientation or the shape of the directional pattern of the waves radiated from an antenna or antenna system varying the relative phase or relative amplitude of energisation between two or more active radiating elementsArrangements for changing or varying the orientation or the shape of the directional pattern of the waves radiated from an antenna or antenna system varying the distribution of energy across a radiating aperture varying the phase
  • H01Q 19/06 - Combinations of primary active antenna elements and units with secondary devices, e.g. with quasi-optical devices, for giving the antenna a desired directional characteristic using refracting or diffracting devices, e.g. lens
  • H01Q 21/00 - Antenna arrays or systems
  • H01Q 21/06 - Arrays of individually energised antenna units similarly polarised and spaced apart
  • H01Q 21/22 - Antenna units of the array energised non-uniformly in amplitude or phase, e.g. tapered array or binomial array
  • H01Q 25/00 - Antennas or antenna systems providing at least two radiating patterns

12.

Lens antenna system

      
Application Number 18496626
Grant Number 11967776
Status In Force
Filing Date 2023-10-27
First Publication Date 2024-02-22
Grant Date 2024-04-23
Owner All.Space Networks Limited (United Kingdom)
Inventor
  • Scarborough, Clinton P.
  • Turpin, Jeremiah P.
  • Difonzo, Daniel F.
  • Finney, John

Abstract

An antenna system that includes a plurality of lens sets. Each lens set includes a lens and at least one feed element. At least one feed element is aligned with the lens and configured to direct a signal through the lens at a desired direction.

IPC Classes  ?

  • H01Q 3/46 - Active lenses or reflecting arrays
  • H01Q 1/28 - Adaptation for use in or on aircraft, missiles, satellites, or balloons
  • H01Q 3/14 - Arrangements for changing or varying the orientation or the shape of the directional pattern of the waves radiated from an antenna or antenna system using mechanical relative movement between primary active elements and secondary devices of antennas or antenna systems for varying the relative position of primary active element and a refracting or diffracting device
  • H01Q 3/24 - Arrangements for changing or varying the orientation or the shape of the directional pattern of the waves radiated from an antenna or antenna system varying the orientation by switching energy from one active radiating element to another, e.g. for beam switching
  • H01Q 3/30 - Arrangements for changing or varying the orientation or the shape of the directional pattern of the waves radiated from an antenna or antenna system varying the relative phase or relative amplitude of energisation between two or more active radiating elementsArrangements for changing or varying the orientation or the shape of the directional pattern of the waves radiated from an antenna or antenna system varying the distribution of energy across a radiating aperture varying the phase
  • H01Q 19/06 - Combinations of primary active antenna elements and units with secondary devices, e.g. with quasi-optical devices, for giving the antenna a desired directional characteristic using refracting or diffracting devices, e.g. lens
  • H01Q 21/00 - Antenna arrays or systems
  • H01Q 21/06 - Arrays of individually energised antenna units similarly polarised and spaced apart
  • H01Q 21/22 - Antenna units of the array energised non-uniformly in amplitude or phase, e.g. tapered array or binomial array
  • H01Q 25/00 - Antennas or antenna systems providing at least two radiating patterns
  • H01Q 1/24 - SupportsMounting means by structural association with other equipment or articles with receiving set

13.

Lens antenna system

      
Application Number 18496301
Grant Number 11967775
Status In Force
Filing Date 2023-10-27
First Publication Date 2024-02-15
Grant Date 2024-04-23
Owner All.Space Networks Limited (United Kingdom)
Inventor
  • Scarborough, Clinton P.
  • Turpin, Jeremiah P.
  • Difonzo, Daniel F.
  • Finney, John

Abstract

An antenna system that includes a plurality of lens sets. Each lens set includes a lens and at least one feed element. At least one feed element is aligned with the lens and configured to direct a signal through the lens at a desired direction.

IPC Classes  ?

  • H01Q 3/46 - Active lenses or reflecting arrays
  • H01Q 1/28 - Adaptation for use in or on aircraft, missiles, satellites, or balloons
  • H01Q 3/14 - Arrangements for changing or varying the orientation or the shape of the directional pattern of the waves radiated from an antenna or antenna system using mechanical relative movement between primary active elements and secondary devices of antennas or antenna systems for varying the relative position of primary active element and a refracting or diffracting device
  • H01Q 3/24 - Arrangements for changing or varying the orientation or the shape of the directional pattern of the waves radiated from an antenna or antenna system varying the orientation by switching energy from one active radiating element to another, e.g. for beam switching
  • H01Q 3/30 - Arrangements for changing or varying the orientation or the shape of the directional pattern of the waves radiated from an antenna or antenna system varying the relative phase or relative amplitude of energisation between two or more active radiating elementsArrangements for changing or varying the orientation or the shape of the directional pattern of the waves radiated from an antenna or antenna system varying the distribution of energy across a radiating aperture varying the phase
  • H01Q 19/06 - Combinations of primary active antenna elements and units with secondary devices, e.g. with quasi-optical devices, for giving the antenna a desired directional characteristic using refracting or diffracting devices, e.g. lens
  • H01Q 21/00 - Antenna arrays or systems
  • H01Q 21/06 - Arrays of individually energised antenna units similarly polarised and spaced apart
  • H01Q 21/22 - Antenna units of the array energised non-uniformly in amplitude or phase, e.g. tapered array or binomial array
  • H01Q 25/00 - Antennas or antenna systems providing at least two radiating patterns
  • H01Q 1/24 - SupportsMounting means by structural association with other equipment or articles with receiving set

14.

METHOD OF OPERATING A SATELLITE COMMUNICATIONS TERMINAL

      
Application Number GB2023050948
Publication Number 2023/194752
Status In Force
Filing Date 2023-04-11
Publication Date 2023-10-12
Owner ALL.SPACE NETWORKS LIMITED (United Kingdom)
Inventor
  • Billman, Brian
  • Turpin, Jeremiah P.
  • Finney, John

Abstract

A method of operating a satellite communications terminal. The method comprises analysing data to be communicated through the satellite communications terminal to identify separate data streams and to determine a data stream parameter characterising each data stream, identifying a plurality of communications links available through the satellite communications terminal comprising a satellite communications link and one or more further communications links, determining a link parameter characterising each available communications link, selecting at least two communications links from the available communications links and establishing or maintaining simultaneous connections to each selected communications link; and transmitting a first data stream through a first selected communications link and transmitting a second data stream through a second selected communications link, wherein the selection of at least two communications links is based on the data stream parameters characterising the first and second data streams and the link parameters characterising the available communications links.

IPC Classes  ?

15.

METHOD OF OPERATING A SATELLITE COMMUNICATIONS TERMINAL

      
Application Number 18132005
Status Pending
Filing Date 2023-04-07
First Publication Date 2023-10-12
Owner All.Space Networks Limited (United Kingdom)
Inventor
  • Billman, Brian Murphy
  • Turpin, Jeremiah P.
  • Finney, John

Abstract

A method of operating a satellite communications terminal. The method comprises analysing data to be communicated through the satellite communications terminal to identify separate data streams and to determine a data stream parameter characterising each data stream, identifying a plurality of communications links available through the satellite communications terminal comprising a satellite communications link and one or more further communications links, determining a link parameter characterising each available communications link, selecting at least two communications links from the available communications links and establishing or maintaining simultaneous connections to each selected communications link; and transmitting a first data stream through a first selected communications link and transmitting a second data stream through a second selected communications link, wherein the selection of at least two communications links is based on the data stream parameters characterising the first and second data streams and the link parameters characterising the available communications links.

IPC Classes  ?

  • H04B 7/185 - Space-based or airborne stations
  • H04W 76/16 - Setup of multiple wireless link connections involving different core network technologies, e.g. a packet-switched [PS] bearer in combination with a circuit-switched [CS] bearer

16.

SATELLITE COMMUNICATIONS NETWORK, SATELLITE TERMINAL AND OPERATION METHOD

      
Application Number 18120372
Status Pending
Filing Date 2023-03-11
First Publication Date 2023-09-14
Owner All.Space Networks Limited (United Kingdom)
Inventor
  • Billman, Brian Murphy
  • Turpin, Jeremiah P.
  • Finney, John

Abstract

A method of operating a satellite communications network, the method comprising: receiving from a satellite terminal a message; and storing the message contents in a satellite network database, the message indicating one or both of: (i) a list of communication satellites which are blocked to a satellite antenna or a portion of the field of view of the satellite antenna which is blocked, at a particular geographic location of the satellite antenna; and (ii) a list of communication satellites that are visible to the satellite antenna or a visible portion of the field of view of the satellite antenna, at a particular geographic location of the satellite antenna. A method of operating a satellite terminal having a satellite antenna. The method comprises controlling a beam of the satellite antenna to scan at least a portion of the field of view of the satellite antenna and locate at least one communication satellite or controlling a beam of the satellite antenna to perform a search to locate a communication satellite in the vicinity of a predicted location of the communication satellite, the predicted location being obtained from satellite ephemeris data. The method further comprises updating a satellite terminal database of communication satellites and their locations by recording the location of the located communication satellite in the satellite terminal database. The database and satellite ephemeris data may be used to determine a list of communication satellites which are blocked or a portion of the field of view of the satellite antenna which is blocked at the current location of the satellite antenna, or to determine a list of communication satellites that are visible to the satellite antenna or a visible portion of the field of view of the satellite antenna. The blocking information or visibility information may be transmitted to a satellite communication network and may be used to build a model of satellite communications network availability across a geographical area.

IPC Classes  ?

17.

ENVIRONMENTALLY ROBUST FABRIC RADOME FOR PLANAR MMWAVE BEAM-STEERING ANTENNAS

      
Application Number 18181498
Status Pending
Filing Date 2023-03-09
First Publication Date 2023-09-14
Owner ALL.SPACE NETWORKS LIMITED (United Kingdom)
Inventor
  • Oakley, Ryan
  • Willmott, Ian

Abstract

A radome assembly for an antenna, comprises: a mounting ring comprising an annular bonding surface; a layer of radome fabric or film bonded to the annular bonding surface and extending radially inwardly and radially outwardly of the bonding surface; and an annular enclosing element located radially outwardly of the bonding surface which encloses or covers at least a portion of the fabric of film radially outward of the annular bonding surface.

IPC Classes  ?

  • H01Q 1/42 - Housings not intimately mechanically associated with radiating elements, e.g. radome

18.

ENVIRONMENTALLY ROBUST FABRIC RADOME FOR PLANAR mmWAVE BEAM-STEERING ANTENNAS

      
Application Number GB2023050533
Publication Number 2023/170400
Status In Force
Filing Date 2023-03-07
Publication Date 2023-09-14
Owner ALL.SPACE NETWORKS LIMITED (United Kingdom)
Inventor
  • Oakey, Ryan
  • Willmott, Ian

Abstract

A radome assembly for an antenna, comprises: a mounting ring (407; 607) comprising an annular bonding surface (405; 605); a layer (403; 603) of radome fabric or film bonded to the annular bonding surface (405; 605) and extending radially inwardly and radially outwardly of the bonding surface; and an annular enclosing element (411; 611) located radially outwardly of the bonding surface (405; 605) which encloses or covers at least a portion of the fabric of film (403; 603) radially outward of the annular bonding surface (405; 605).

IPC Classes  ?

  • H01Q 1/42 - Housings not intimately mechanically associated with radiating elements, e.g. radome

19.

GAIN ROLL-OFF FOR HYBRID MECHANICAL-LENS ANTENNA PHASED ARRAYS

      
Application Number 18313200
Status Pending
Filing Date 2023-05-05
First Publication Date 2023-08-31
Owner All.Space Networks Limited (United Kingdom)
Inventor
  • Scarborough, Clinton P.
  • Turpin, Jeremiah P.
  • Billman, Brian M.
  • Finney, John

Abstract

A hybrid mechanical-lens array antenna is described that can be configured with different orientations and arrangements of the plurality of lenses within the array to control and enhance the performance at different regions of scan. This can include the addition of a secondary array (a skirt) at a large tilt angle, tilting the primary array, tilting the individual lenses within the primary array, or any combination. These design choices, when holding the number of lens modules (and, therefore, cost and power consumption) constant, have the effect of changing the system height, reducing the boresight gain and increasing the gain at scan, with each option showing different trades of height and scan and boresight performance.

IPC Classes  ?

  • H01Q 3/04 - Arrangements for changing or varying the orientation or the shape of the directional pattern of the waves radiated from an antenna or antenna system using mechanical movement of antenna or antenna system as a whole for varying one co-ordinate of the orientation
  • H01Q 19/06 - Combinations of primary active antenna elements and units with secondary devices, e.g. with quasi-optical devices, for giving the antenna a desired directional characteristic using refracting or diffracting devices, e.g. lens

20.

Non-cooperative position, navigation, and timing extraction from VSAT communications signals using multi-beam phased array antenna

      
Application Number 18135520
Grant Number 12306314
Status In Force
Filing Date 2023-04-17
First Publication Date 2023-08-17
Grant Date 2025-05-20
Owner All.Space Networks Limited (United Kingdom)
Inventor
  • Turpin, Jeremiah P.
  • Billman, Brian
  • Finney, John

Abstract

A ground antenna determines the current time and its own position from received signals that were transmitted by artificial earth satellites for communication. A high-gain multi-beam electrically-steered antenna is combined with a processing system to measure the angles between two or more satellites and determine the present distance to each satellite by the information broadcast on the TT&C channel. The knowledge of the angles and distances, as well as the trajectory of the satellites, can be combined with their locations as predicted by the satellite ephemeris data to triangulate the location of the receiver. This system is different from conventional GPS antennas because it does not require the cooperation of active communication with the satellites to derive a location estimate. The location is computed by the ground terminal, not by the satellite. This system can be used in cases where other locating services are offline, jammed, or otherwise unavailable to maintain location and time synchronization.

IPC Classes  ?

  • G01S 19/31 - Acquisition or tracking of other signals for positioning
  • G01S 19/25 - Acquisition or tracking of signals transmitted by the system involving aiding data received from a cooperating element, e.g. assisted GPS
  • G01S 19/49 - Determining position by combining or switching between position solutions derived from the satellite radio beacon positioning system and position solutions derived from a further system whereby the further system is an inertial position system, e.g. loosely-coupled
  • H01Q 3/34 - Arrangements for changing or varying the orientation or the shape of the directional pattern of the waves radiated from an antenna or antenna system varying the relative phase or relative amplitude of energisation between two or more active radiating elementsArrangements for changing or varying the orientation or the shape of the directional pattern of the waves radiated from an antenna or antenna system varying the distribution of energy across a radiating aperture varying the phase by electrical means

21.

PLANAR MULTIBEAM HYBRID-ELECTROMECHANICAL SATCOM TERMINAL

      
Application Number GB2023050199
Publication Number 2023/148474
Status In Force
Filing Date 2023-01-30
Publication Date 2023-08-10
Owner ALL.SPACE NETWORKS LIMITED (United Kingdom)
Inventor Turpin, Jeremiah P.

Abstract

A lens array antenna system that includes a plurality of lens modules, each consisting of an RF lens and a plurality of feeds forming a linear feed region or feed array. Multiple linear feed regions supporting different frequency bands may be used. The lenses and array of feeds jointly rotate and are slidably connected to allow the location of the linear feed region relative to the focal locus of the lens to be changed by an actuator and controller to allow any two focal points corresponding to desired beam scanning directions to be covered by the linear feed region. In this way, a planar hybrid electromechanical beamforming antenna can form two independent beams in the upper hemisphere with only two mechanical actuators and a single axis of electronic beamforming, reducing production cost compared to existing multibeam antenna solutions.

IPC Classes  ?

  • H01Q 3/04 - Arrangements for changing or varying the orientation or the shape of the directional pattern of the waves radiated from an antenna or antenna system using mechanical movement of antenna or antenna system as a whole for varying one co-ordinate of the orientation
  • H01Q 3/14 - Arrangements for changing or varying the orientation or the shape of the directional pattern of the waves radiated from an antenna or antenna system using mechanical relative movement between primary active elements and secondary devices of antennas or antenna systems for varying the relative position of primary active element and a refracting or diffracting device
  • H01Q 21/06 - Arrays of individually energised antenna units similarly polarised and spaced apart
  • H01Q 25/00 - Antennas or antenna systems providing at least two radiating patterns

22.

Planar multibeam hybrid-electromechanical SATCOM terminal

      
Application Number 18103365
Grant Number 12206180
Status In Force
Filing Date 2023-01-30
First Publication Date 2023-08-03
Grant Date 2025-01-21
Owner All.Space Networks Limited (United Kingdom)
Inventor Turpin, Jeremiah P.

Abstract

A lens array antenna system that includes a plurality of lens modules, each consisting of an RF lens and a plurality of feeds forming a linear feed region or feed array. Multiple linear feed regions supporting different frequency bands may be used. The lenses and array of feeds jointly rotate and are slidably connected to allow the location of the linear feed region relative to the focal locus of the lens to be changed by an actuator and controller to allow any two focal points corresponding to desired beam scanning directions to be covered by the linear feed region. In this way, a planar hybrid electromechanical beamforming antenna can form two independent beams in the upper hemisphere with only two mechanical actuators and a single axis of electronic beamforming, reducing production cost compared to existing multibeam antenna solutions.

IPC Classes  ?

  • H01Q 3/14 - Arrangements for changing or varying the orientation or the shape of the directional pattern of the waves radiated from an antenna or antenna system using mechanical relative movement between primary active elements and secondary devices of antennas or antenna systems for varying the relative position of primary active element and a refracting or diffracting device
  • H01Q 25/00 - Antennas or antenna systems providing at least two radiating patterns

23.

Multi-band lens antenna system

      
Application Number 18084409
Grant Number 12316016
Status In Force
Filing Date 2022-12-19
First Publication Date 2023-07-20
Grant Date 2025-05-27
Owner All.Space Networks Limited (United Kingdom)
Inventor
  • Turpin, Jeremiah P.
  • Scarborough, Clinton P.
  • Difonzo, Daniel F.
  • Billman, Brian Murphy

Abstract

A multi-band antenna system that includes a first antenna array and a second antenna array. The first antenna array includes a plurality of lens sets, each including a lens and feed element(s) configured to transmit and/or receive electromagnetic signals that pass through the lens. The second antenna array includes a plurality of antenna elements, each disposed between two of the lenses of the first array.

IPC Classes  ?

  • H01Q 25/00 - Antennas or antenna systems providing at least two radiating patterns
  • H01Q 5/42 - Imbricated or interleaved structuresCombined or electromagnetically coupled arrangements, e.g. comprising two or more non-connected fed radiating elements using two or more imbricated arrays
  • H01Q 19/06 - Combinations of primary active antenna elements and units with secondary devices, e.g. with quasi-optical devices, for giving the antenna a desired directional characteristic using refracting or diffracting devices, e.g. lens

24.

High-gain multibeam GNSS antenna

      
Application Number 18083419
Grant Number 12007485
Status In Force
Filing Date 2022-12-16
First Publication Date 2023-07-13
Grant Date 2024-06-11
Owner All.Space Networks Limited (United Kingdom)
Inventor
  • Zavrel, Robert J.
  • Turpin, Jeremiah P.
  • Finney, John

Abstract

A multibeam Radio Frequency (RF) lens antenna is designed as a receiver for Global Navigation Satellite System (GNSS) applications, such as GPS (Global Positioning System), Galileo, GLONASS, COMPASS, and others. The RF lens and plurality of associated feed elements and receiver circuits combine to form a plurality of resulting high-gain relatively narrow beams that, taken together, allow reception of signals from GNSS satellites over the entire upper hemisphere. Any kind of RF lens can be used, where the lens can be of homogeneous or inhomogeneous, dielectric or metamaterial/metasurface construction. The benefit of this approach to build a GNSS receiver over existing alternatives is increased gain and decreased noise at each receiver, which improves the signal to noise ratio (SNR) and improves the accuracy and reliability of the position and time measurements, while also reducing the impact of, and sensitivity to, interference, jamming, and spoofing signals. The approaches described in this patent can be combined with existing signal processing and accuracy improvement methods (such as Real-Time Kinematic (RTK), Precise-Point Positioning (PPP), and Differential GPS (DEPS)) for further benefits. This system has applications within the surveying, maritime, land mobility, aerospace, and government positioning market areas.

IPC Classes  ?

  • G01S 19/21 - Interference related issues
  • G01S 19/14 - Receivers specially adapted for specific applications
  • G01S 19/23 - Testing, monitoring, correcting or calibrating of a receiver element
  • G01S 19/37 - Hardware or software details of the signal processing chain
  • H01Q 1/24 - SupportsMounting means by structural association with other equipment or articles with receiving set

25.

Field-assembled modular phased array SATCOM terminal

      
Application Number 18089779
Grant Number 11996626
Status In Force
Filing Date 2022-12-28
First Publication Date 2023-07-13
Grant Date 2024-05-28
Owner All.Space Networks Limited (United Kingdom)
Inventor
  • Turpin, Jeremiah P.
  • Billman, Brian Murphy
  • Finney, John

Abstract

A field-assembled satellite communications terminal has a plurality of discrete, modular aperture blocks. Each aperture block contains an electrically steered antenna aperture, and a plurality of interconnection ports for power and data communications between the plurality of aperture blocks. The plurality of interconnection ports are removably connectable by the end user in the field. The terminal further has a signal processing system for receiving, processing, and generating signals to and from the apertures. The aperture blocks are connected to each other in the field and self-configure to form an electrically-steered antenna.

IPC Classes  ?

  • H01Q 3/26 - Arrangements for changing or varying the orientation or the shape of the directional pattern of the waves radiated from an antenna or antenna system varying the relative phase or relative amplitude of energisation between two or more active radiating elementsArrangements for changing or varying the orientation or the shape of the directional pattern of the waves radiated from an antenna or antenna system varying the distribution of energy across a radiating aperture
  • H01Q 3/38 - Arrangements for changing or varying the orientation or the shape of the directional pattern of the waves radiated from an antenna or antenna system varying the relative phase or relative amplitude of energisation between two or more active radiating elementsArrangements for changing or varying the orientation or the shape of the directional pattern of the waves radiated from an antenna or antenna system varying the distribution of energy across a radiating aperture varying the phase by electrical means with variable phase-shifters the phase-shifters being digital
  • H04B 10/118 - Arrangements specific to free-space transmission, i.e. transmission through air or vacuum specially adapted for satellite communication
  • H04B 17/12 - MonitoringTesting of transmitters for calibration of transmit antennas, e.g. of amplitude or phase
  • H04B 17/21 - MonitoringTesting of receivers for calibrationMonitoringTesting of receivers for correcting measurements
  • H04B 17/27 - MonitoringTesting of receivers for locating or positioning the transmitter

26.

MULTI-BEAM ANTENNA ARRAY

      
Application Number GB2022052371
Publication Number 2023/052743
Status In Force
Filing Date 2022-09-20
Publication Date 2023-04-06
Owner ALL.SPACE NETWORKS LIMITED (United Kingdom)
Inventor
  • Szczepanik, Jean-Paul
  • Keeton, Richard
  • Sharma, Vikas
  • Papaionannou, Maria
  • De Jager, Derek
  • Al-Taei, Sarmad
  • Savage, Kevin
  • Candotti, Massimo
  • Wilmott, Ian
  • Long, Nicholas Leonard
  • Turpin, Jeremiah P.
  • Finney, John

Abstract

There is disclosed a multi-beam antenna array, comprising a main array of antenna modules, each antenna module comprising a plurality M of individually-steerable antenna elements. The antenna modules are arranged in the main array with N-fold rotational symmetry, the antenna elements are arranged within each module with M-fold rotational symmetry, and each antenna element comprises a sub-array of radiating elements.

IPC Classes  ?

  • H01Q 25/00 - Antennas or antenna systems providing at least two radiating patterns
  • H01Q 21/00 - Antenna arrays or systems
  • H01Q 21/20 - Arrays of individually energised antenna units similarly polarised and spaced apart the units being spaced along, or adjacent to, a curvilinear path
  • H01Q 19/06 - Combinations of primary active antenna elements and units with secondary devices, e.g. with quasi-optical devices, for giving the antenna a desired directional characteristic using refracting or diffracting devices, e.g. lens
  • H01Q 3/24 - Arrangements for changing or varying the orientation or the shape of the directional pattern of the waves radiated from an antenna or antenna system varying the orientation by switching energy from one active radiating element to another, e.g. for beam switching

27.

ALL.SPACE

      
Application Number 1720621
Status Registered
Filing Date 2023-01-26
Registration Date 2023-01-26
Owner ALL.SPACE NETWORKS LIMITED (United Kingdom)
NICE Classes  ?
  • 09 - Scientific and electric apparatus and instruments
  • 38 - Telecommunications services

Goods & Services

Telecommunications equipment and hardware, namely, antennas, antenna terminals, optical lenses, optical lens arrays, radio frequency lenses, microwave lenses; antennas, antenna terminals, optical lenses, optical lens arrays, radio frequency lenses, microwave lenses for wireless communication systems, broadband point to point and point to multipoint communications systems; fifth generation wireless indoor antennas, fifth generation wireless outdoor antennas, microwave antennas, mobile antennas, and ground station antennas; electro-magnetic and radio spectrum counter-measure systems, active radar systems, and systems for radio frequency detection, monitoring, and processing. Telecommunications services; telecommunications consultation services; providing access to telecommunication networks.

28.

ALL.SPACE

      
Application Number 224737800
Status Pending
Filing Date 2023-01-26
Owner ALL.SPACE NETWORKS LIMITED (United Kingdom)
NICE Classes  ?
  • 09 - Scientific and electric apparatus and instruments
  • 38 - Telecommunications services

Goods & Services

(1) Telecommunications equipment and hardware, namely, antennas, antenna terminals, optical lenses, optical lens arrays, radio frequency lenses, microwave lenses; antennas, antenna terminals, optical lenses, optical lens arrays, radio frequency lenses, microwave lenses for wireless communication systems, broadband point to point and point to multipoint communications systems; fifth generation wireless indoor antennas, fifth generation wireless outdoor antennas, microwave antennas, mobile antennas, and ground station antennas; electro-magnetic and radio spectrum counter-measure systems, active radar systems, and systems for radio frequency detection, monitoring, and processing. (1) Telecommunications services; telecommunications consultation services; providing access to telecommunication networks.

29.

ALL.SPACE

      
Serial Number 79365958
Status Registered
Filing Date 2023-01-26
Registration Date 2024-10-08
Owner ALL.SPACE NETWORKS LIMITED (United Kingdom)
NICE Classes  ?
  • 38 - Telecommunications services
  • 09 - Scientific and electric apparatus and instruments

Goods & Services

Telecommunications services, namely, transmission of voice, data, graphics, images, audio and video by means of telecommunications networks, wireless communication networks, and the Internet; telecommunications consultation services; providing access to telecommunication networks Telecommunications equipment and hardware, namely, antennas, antenna terminals, optical lenses, optical lens arrays, radio frequency lenses being devices for use in wireless communications, microwave lenses; antennas, antenna terminals, optical lenses, optical lens arrays, radio frequency lenses being devices for use in wireless communications, microwave lenses for wireless communication systems, broadband point to point and point to multipoint communications systems comprised of telecommunications base station equipment for cellular and fixed networking and communications applications; fifth generation wireless indoor antennas, fifth generation wireless outdoor antennas, microwave antennas, mobile antennas, and ground station antennas; electro-magnetic and radio spectrum counter-measure systems comprised primarily of antennas and radio frequency lenses being devices for use in wireless communications; active radar systems comprised of antennas and radio frequency lenses being devices for use in wireless communications; systems for radio frequency detection, monitoring, and processing comprised of antennas and radio frequency lenses being devices for use in wireless communications

30.

Prism for repointing reflector antenna main beam

      
Application Number 17943895
Grant Number 11888228
Status In Force
Filing Date 2022-09-13
First Publication Date 2023-01-05
Grant Date 2024-01-30
Owner All.Space Networks Limited (United Kingdom)
Inventor
  • Turpin, Jeremiah P.
  • Finney, John

Abstract

A microwave prism is used to repoint an operational Direct-to-Home (DTH) or Very Small Aperture Terminal (VSAT) reflector antenna as part of a ground terminal to receive (or transmit) signals from a different satellite or orbital position without physically moving the reflector or the feed horn antenna. The microwave prism operates by shifting the radiated fields from the horn antenna generally perpendicular to the focal axis of the parabolic reflector in order to cause the main beam of the reflector to scan in response. For an existing reflector antenna receiving signals from an incumbent satellite, a prism has been designed to be snapped into place over the feed horn and shift the fields laterally by a calibrated distance. The structure of the prism is designed to be positioned and oriented correctly without the use of skilled labor. This system allows a satellite service provider to repoint their subscribers to a new satellite by shipping a self-install kit of the prism that is pre-configured to have the correct orientation and position on the feed antenna to correctly re-point the beam at a different satellite once the prism is applied. One benefit of the system is that unskilled labor, i.e., the subscribers themselves, can be used to repoint a large number of subscriber antennas in a satellite network rather than requiring the cost of a truck roll and a technician to visit every site. The microwave prisms to implement this functionality can be constructed in different ways, with homogeneous slabs or blocks, Gradient-Index (GRIN), multi-layered dielectric, geometric or graded-index Fresnel-zone, metasurface, or metamaterial prisms. The geometric and electrical constraints of the design are determined by the incumbent and target satellites, and the ground terminal location.

IPC Classes  ?

  • H01Q 19/13 - Combinations of primary active antenna elements and units with secondary devices, e.g. with quasi-optical devices, for giving the antenna a desired directional characteristic using reflecting surfaces wherein the surfaces are concave the primary radiating source being a single radiating element, e.g. a dipole, a slot, a waveguide termination
  • H01Q 5/55 - Feeding or matching arrangements for broad-band or multi-band operation for horn or waveguide antennas
  • H01Q 1/24 - SupportsMounting means by structural association with other equipment or articles with receiving set
  • H01Q 3/08 - Arrangements for changing or varying the orientation or the shape of the directional pattern of the waves radiated from an antenna or antenna system using mechanical movement of antenna or antenna system as a whole for varying two co-ordinates of the orientation
  • H01Q 3/20 - Arrangements for changing or varying the orientation or the shape of the directional pattern of the waves radiated from an antenna or antenna system using mechanical relative movement between primary active elements and secondary devices of antennas or antenna systems for varying relative position of primary active element and a reflecting device wherein the primary active element is fixed and the reflecting device is movable
  • H01Q 15/16 - Reflecting surfacesEquivalent structures curved in two dimensions, e.g. paraboloidal
  • H01Q 19/19 - Combinations of primary active antenna elements and units with secondary devices, e.g. with quasi-optical devices, for giving the antenna a desired directional characteristic using reflecting surfaces having two or more spaced reflecting surfaces comprising one main concave reflecting surface associated with an auxiliary reflecting surface
  • H04B 7/185 - Space-based or airborne stations
  • H01Q 15/04 - Refracting or diffracting devices, e.g. lens, prism comprising wave-guiding channel or channels bounded by effective conductive surfaces substantially perpendicular to the electric vector of the wave, e.g. parallel-plate waveguide lens

31.

ALL.SPACE

      
Application Number 1669455
Status Registered
Filing Date 2022-01-26
Registration Date 2022-01-26
Owner ALL.SPACE NETWORKS LIMITED (United Kingdom)
NICE Classes  ?
  • 09 - Scientific and electric apparatus and instruments
  • 38 - Telecommunications services

Goods & Services

Telecommunications equipment and hardware, namely, antennas, antenna terminals, optical lenses, optical lens arrays, radio frequency lenses, microwave lenses; antennas, antenna terminals, optical lenses, optical lens arrays, radio frequency lenses, microwave lenses for wireless communication systems, broadband point to point and point to multipoint communications systems; fifth generation wireless indoor antennas, fifth generation wireless outdoor antennas, microwave antennas, mobile antennas, and ground station antennas; electro-magnetic and radio spectrum counter-measure systems, active radar systems, and systems for radio frequency detection, monitoring, and processing. Telecommunications services; telecommunications consultation services; providing access to telecommunication networks.

32.

ALL.SPACE

      
Application Number 1663310
Status Registered
Filing Date 2022-01-10
Registration Date 2022-01-10
Owner ALL.SPACE NETWORKS LIMITED (United Kingdom)
NICE Classes  ?
  • 09 - Scientific and electric apparatus and instruments
  • 38 - Telecommunications services

Goods & Services

Telecommunications equipment and hardware, namely, antennas, antenna terminals, optical lenses, optical lens arrays, radio frequency lenses, microwave lenses; antennas, antenna terminals, optical lenses, optical lens arrays, radio frequency lenses, microwave lenses for wireless communication systems, broadband point to point and point to multipoint communications systems; fifth generation wireless indoor antennas, fifth generation wireless outdoor antennas, microwave antennas, mobile antennas, and ground station antennas; electro-magnetic and radio spectrum counter-measure systems, active radar systems, and systems for radio frequency detection, monitoring, and processing. Telecommunications services; telecommunications consultation services; providing access to telecommunication networks.

33.

Isotropic 3D-printed gradient-index RF lens

      
Application Number 17517823
Grant Number 12170403
Status In Force
Filing Date 2021-11-03
First Publication Date 2022-05-05
Grant Date 2024-12-17
Owner All.Space Networks Limited (United Kingdom)
Inventor
  • Turpin, Jeremiah P.
  • Bouhanna, Zakaria
  • Finney, John
  • Dinc, Ergin

Abstract

Inhomogeneous dielectric lenses for electromagnetic waves can be produced by a process such as 3D printing to have controllable dielectric values. Dielectric values can be produced by a varying density of air voids within, for example, a dielectric matrix to obtain an effective overall density. Approaches in accordance with various embodiments can obtain uniform, isotropic dielectric properties without resonant behavior by the use of aperiodic distributions of nonuniformly-sized air voids. Target air fraction and distribution of air voids can be specified by a target dielectric constant through dielectric mixing rules, such as Maxwell-Garnet mixing rules, and a requirement for locally uniform distributions of air voids, while varying the density of the air voids across the overall structure to produce a desired gradient of dielectric properties.

IPC Classes  ?

  • H01Q 15/08 - Refracting or diffracting devices, e.g. lens, prism formed of solid dielectric material
  • B29D 11/00 - Producing optical elements, e.g. lenses or prisms
  • B33Y 10/00 - Processes of additive manufacturing
  • B33Y 80/00 - Products made by additive manufacturing
  • H01Q 15/02 - Refracting or diffracting devices, e.g. lens, prism

34.

REACH BEYOND

      
Serial Number 97299569
Status Registered
Filing Date 2022-03-07
Registration Date 2023-09-05
Owner ALL.SPACE NETWORKS LIMITED ()
NICE Classes  ? 09 - Scientific and electric apparatus and instruments

Goods & Services

Telecommunications equipment and hardware, namely, antennas, antenna terminals, optical lens arrays, radio frequency lenses, microwave lenses; antennas, antenna terminals, optical lens arrays, radio frequency lenses, microwave lenses for wireless communication systems, broadband point to point and point to multipoint communications systems; fifth generation wireless indoor antennas, fifth generation wireless outdoor antennas, microwave antennas, mobile antennas, and ground station antennas; electro-magnetic and radio spectrum counter-measure systems comprised primarily of electromagnetic apparatus used to generate and measure electromagnetic fields and signal processing and analysis equipment, antennas and radio frequency lenses, active radar systems comprised primarily of radar apparatus, radar detectors, radar antennas and radar displays, antennas and radio frequency lenses, and systems for radio frequency detection, monitoring, and processing comprised primarily of radio frequency transmitters, radio frequency receivers, radio frequency antennas, computer hardware, frequency meters, and frequency synthesizers, antennas and radio frequency lenses

35.

ALL.SPACE

      
Application Number 218796200
Status Pending
Filing Date 2022-01-10
Owner ALL.SPACE NETWORKS LIMITED (United Kingdom)
NICE Classes  ?
  • 09 - Scientific and electric apparatus and instruments
  • 38 - Telecommunications services

Goods & Services

(1) Telecommunications equipment and hardware, namely, antennas, antenna terminals, optical lenses, optical lens arrays, radio frequency lenses, microwave lenses; antennas, antenna terminals, optical lenses, optical lens arrays, radio frequency lenses, microwave lenses for wireless communication systems, broadband point to point and point to multipoint communications systems; fifth generation wireless indoor antennas, fifth generation wireless outdoor antennas, microwave antennas, mobile antennas, and ground station antennas; electro-magnetic and radio spectrum counter-measure systems, active radar systems, and systems for radio frequency detection, monitoring, and processing. (1) Telecommunications services; telecommunications consultation services; providing access to telecommunication networks.

36.

ALL.SPACE

      
Serial Number 79341335
Status Registered
Filing Date 2022-01-10
Registration Date 2023-11-14
Owner ALL.SPACE NETWORKS LIMITED (United Kingdom)
NICE Classes  ?
  • 09 - Scientific and electric apparatus and instruments
  • 38 - Telecommunications services

Goods & Services

Telecommunications equipment and hardware, namely, antennas, antenna terminals, optical lenses, optical lens arrays, radio frequency lenses being devices for use in wireless communications, microwave lenses; antennas, antenna terminals, optical lenses, optical lens arrays, radio frequency lenses, microwave lenses for wireless communication systems, broadband point to point and point to multipoint communications systems comprised of telecommunications base station equipment for cellular and fixed networking and communications applications; fifth generation wireless indoor antennas, fifth generation wireless outdoor antennas, microwave antennas, mobile antennas, and ground station antennas; electro-magnetic and radio spectrum counter-measure systems comprised primarily of antennas and radio frequency lenses; active radar systems comprised of antennas and radio frequency lenses; systems for radio frequency detection, monitoring, and processing comprised of antennas and radio frequency lenses Telecommunications services, namely, transmission of voice, data, graphics, images, audio and video by means of telecommunications networks, wireless communication networks, and the Internet; Telecommunications consultation services; Providing access to telecommunication networks

37.

Field-assembled modular phased array SATCOM terminal

      
Application Number 17221143
Grant Number 11581639
Status In Force
Filing Date 2021-04-02
First Publication Date 2021-10-07
Grant Date 2023-02-14
Owner ALL.SPACE NETWORKS LTD. (United Kingdom)
Inventor
  • Turpin, Jeremiah P.
  • Billman, Brian
  • Finney, John

Abstract

A field-assembled satellite communications terminal has a plurality of discrete, modular aperture blocks. Each aperture block contains an electrically steered antenna aperture, and a plurality of interconnection ports for power and data communications between the plurality of aperture blocks. The plurality of interconnection ports are removably connectable by the end user in the field. The terminal further has a signal processing system for receiving, processing, and generating signals to and from the apertures. The aperture blocks are connected to each other in the field and self-configure to form an electrically-steered antenna.

IPC Classes  ?

  • H04B 17/12 - MonitoringTesting of transmitters for calibration of transmit antennas, e.g. of amplitude or phase
  • H01Q 3/26 - Arrangements for changing or varying the orientation or the shape of the directional pattern of the waves radiated from an antenna or antenna system varying the relative phase or relative amplitude of energisation between two or more active radiating elementsArrangements for changing or varying the orientation or the shape of the directional pattern of the waves radiated from an antenna or antenna system varying the distribution of energy across a radiating aperture
  • H04B 17/21 - MonitoringTesting of receivers for calibrationMonitoringTesting of receivers for correcting measurements
  • H04B 17/27 - MonitoringTesting of receivers for locating or positioning the transmitter
  • H01Q 3/38 - Arrangements for changing or varying the orientation or the shape of the directional pattern of the waves radiated from an antenna or antenna system varying the relative phase or relative amplitude of energisation between two or more active radiating elementsArrangements for changing or varying the orientation or the shape of the directional pattern of the waves radiated from an antenna or antenna system varying the distribution of energy across a radiating aperture varying the phase by electrical means with variable phase-shifters the phase-shifters being digital
  • H04B 10/118 - Arrangements specific to free-space transmission, i.e. transmission through air or vacuum specially adapted for satellite communication

38.

Prism for repointing reflector antenna main beam

      
Application Number 17182992
Grant Number 11469515
Status In Force
Filing Date 2021-02-23
First Publication Date 2021-08-26
Grant Date 2022-10-11
Owner ALL.SPACE NETWORKS LTD. (United Kingdom)
Inventor
  • Turpin, Jeremiah P.
  • Finney, John

Abstract

A microwave prism is used to repoint an operational Direct-to-Home (DTH) or Very Small Aperture Terminal (VSAT) reflector antenna as part of a ground terminal to receive (or transmit) signals from a different satellite or orbital position without physically moving the reflector or the feed horn antenna. The microwave prism operates by shifting the radiated fields from the horn antenna generally perpendicular to the focal axis of the parabolic reflector in order to cause the main beam of the reflector to scan in response. For an existing reflector antenna receiving signals from an incumbent satellite, a prism has been designed to be snapped into place over the feed horn and shift the fields laterally by a calibrated distance. The structure of the prism is designed to be positioned and oriented correctly without the use of skilled labor. This system allows a satellite service provider to repoint their subscribers to a new satellite by shipping a self-install kit of the prism that is pre-configured to have the correct orientation and position on the feed antenna to correctly re-point the beam at a different satellite once the prism is applied. One benefit of the system is that unskilled labor, i.e., the subscribers themselves, can be used to repoint a large number of subscriber antennas in a satellite network rather than requiring the cost of a truck roll and a technician to visit every site. The microwave prisms to implement this functionality can be constructed in different ways, with homogeneous slabs or blocks, Gradient-Index (GRIN), multi-layered dielectric, geometric or graded-index Fresnel-zone, metasurface, or metamaterial prisms. The geometric and electrical constraints of the design are determined by the incumbent and target satellites and the ground terminal location.

IPC Classes  ?

  • H01Q 19/13 - Combinations of primary active antenna elements and units with secondary devices, e.g. with quasi-optical devices, for giving the antenna a desired directional characteristic using reflecting surfaces wherein the surfaces are concave the primary radiating source being a single radiating element, e.g. a dipole, a slot, a waveguide termination
  • H01Q 5/55 - Feeding or matching arrangements for broad-band or multi-band operation for horn or waveguide antennas
  • H01Q 1/24 - SupportsMounting means by structural association with other equipment or articles with receiving set
  • H01Q 3/08 - Arrangements for changing or varying the orientation or the shape of the directional pattern of the waves radiated from an antenna or antenna system using mechanical movement of antenna or antenna system as a whole for varying two co-ordinates of the orientation
  • H01Q 3/20 - Arrangements for changing or varying the orientation or the shape of the directional pattern of the waves radiated from an antenna or antenna system using mechanical relative movement between primary active elements and secondary devices of antennas or antenna systems for varying relative position of primary active element and a reflecting device wherein the primary active element is fixed and the reflecting device is movable
  • H01Q 15/16 - Reflecting surfacesEquivalent structures curved in two dimensions, e.g. paraboloidal
  • H01Q 19/19 - Combinations of primary active antenna elements and units with secondary devices, e.g. with quasi-optical devices, for giving the antenna a desired directional characteristic using reflecting surfaces having two or more spaced reflecting surfaces comprising one main concave reflecting surface associated with an auxiliary reflecting surface
  • H04B 7/185 - Space-based or airborne stations

39.

High-gain multibeam GNSS antenna

      
Application Number 17125681
Grant Number 11550062
Status In Force
Filing Date 2020-12-17
First Publication Date 2021-07-08
Grant Date 2023-01-10
Owner ALL.SPACE NETWORKS LTD. (United Kingdom)
Inventor
  • Zavrel, Robert J.
  • Turpin, Jeremiah P.
  • Finney, John

Abstract

A multibeam Radio Frequency (RF) lens antenna is designed as a receiver for Global Navigation Satellite System (GNSS) applications, such as GPS (Global Positioning System), Galileo, GLONASS, COMPASS, and others. The RF lens and plurality of associated feed elements and receiver circuits combine to form a plurality of resulting high-gain relatively narrow beams that, taken together, allow reception of signals from GNSS satellites over the entire upper hemisphere. Any kind of RF lens can be used, where the lens can be of homogeneous or inhomogeneous, dielectric or metamaterial metasurface construction. The benefit of this approach to build a GNSS receiver over existing alternatives is increased gain and decreased noise at each receiver, which improves the signal to noise ratio (SNR) and improves the accuracy and reliability of the position and time measurements, while also reducing the impact of, and sensitivity to, interference, jamming, and spoofing signals. The approaches described in this patent can be combined with existing signal processing and accuracy improvement methods (such as Real-Time Kinematic (RTK), Precise-Point Positioning (PPP), and Differential GPS (DEPS)) for further benefits. This system has applications within the surveying, maritime, land mobility, aerospace, and government positioning market areas.

IPC Classes  ?

  • G01S 19/37 - Hardware or software details of the signal processing chain
  • G01S 19/21 - Interference related issues
  • G01S 19/14 - Receivers specially adapted for specific applications
  • G01S 19/23 - Testing, monitoring, correcting or calibrating of a receiver element
  • H01Q 1/24 - SupportsMounting means by structural association with other equipment or articles with receiving set

40.

Circuit and system apparatus for synthesizing one or multiple beams on a switched-feed antenna

      
Application Number 17084396
Grant Number 11870154
Status In Force
Filing Date 2020-10-29
First Publication Date 2021-05-06
Grant Date 2024-01-09
Owner All.Space Networks Limited (United Kingdom)
Inventor
  • Diebold, Sebastian
  • Sharma, Vikas
  • Billman, Brian Murphy
  • Turpin, Jeremiah P.

Abstract

A circuit has at least one amplifier and a signal routing device such as one or more switches, and an array of antenna elements from which some subset must be enabled and processed at a time. The antenna elements can be grouped in accordance with an organization scheme (e.g., rows, columns) to enable more flexibility in selecting and routing the signals. The system is used to create one or more beams, which can be pointed (steered) to a wide range of directions by means of selecting one or more feed antennas in a switched-feed antenna without including full receive and transmit circuitry (DSP, frequency conversion) for each feed in the array. In this case, minimizing the number of DSP chains is desirable to reduce the cost, power, and complexity of the antenna. The resulting beam(s) can be combined and manipulated to support multiple users, track several targets, increase operational range, increase radar resolution, or data-rate in communications.

IPC Classes  ?

  • H01Q 3/26 - Arrangements for changing or varying the orientation or the shape of the directional pattern of the waves radiated from an antenna or antenna system varying the relative phase or relative amplitude of energisation between two or more active radiating elementsArrangements for changing or varying the orientation or the shape of the directional pattern of the waves radiated from an antenna or antenna system varying the distribution of energy across a radiating aperture
  • H01Q 3/36 - Arrangements for changing or varying the orientation or the shape of the directional pattern of the waves radiated from an antenna or antenna system varying the relative phase or relative amplitude of energisation between two or more active radiating elementsArrangements for changing or varying the orientation or the shape of the directional pattern of the waves radiated from an antenna or antenna system varying the distribution of energy across a radiating aperture varying the phase by electrical means with variable phase-shifters
  • H04B 1/16 - Circuits
  • H04B 7/0426 - Power distribution

41.

Dynamic interference reduction for antenna beam tracking systems

      
Application Number 17024763
Grant Number 11043736
Status In Force
Filing Date 2020-09-18
First Publication Date 2021-01-07
Grant Date 2021-06-22
Owner ALL.SPACE NETWORKS LTD. (United Kingdom)
Inventor
  • Difonzo, Daniel F.
  • Turpin, Jeremiah P.

Abstract

An antenna beam tracking system has dynamic interference reduction. The system includes antennas that can form multiple beams, each beam of which can continually track or point its beams independently in various angular directions. A first beam continually tracks and receives (downlink) signals from a desired source or node such as a satellite or terrestrial node which generally has an apparent motion relative to the antenna. A second beam continually tracks and receives potentially harmful interference signals that may arise from different directions. The signals of the second beam are dynamically coupled to the signals in the first beam in such a manner as to effect cancellation or substantial reduction of the interference.

IPC Classes  ?

  • H01Q 1/24 - SupportsMounting means by structural association with other equipment or articles with receiving set
  • H01Q 25/00 - Antennas or antenna systems providing at least two radiating patterns
  • H04W 16/28 - Cell structures using beam steering
  • H04B 7/185 - Space-based or airborne stations

42.

Gain roll-off for hybrid mechanical-lens antenna phased arrays

      
Application Number 16865123
Grant Number 11735816
Status In Force
Filing Date 2020-05-01
First Publication Date 2020-11-05
Grant Date 2023-08-22
Owner All.Space Networks Limited (United Kingdom)
Inventor
  • Scarborough, Clinton P.
  • Turpin, Jeremiah P.
  • Billman, Brian M.
  • Finney, John

Abstract

A hybrid mechanical-lens array antenna is described that can be configured with different orientations and arrangements of the plurality of lenses within the array to control and enhance the performance at different regions of scan. This can include the addition of a secondary array (a skirt) at a large tilt angle, tilting the primary array, tilting the individual lenses within the primary array, or any combination. These design choices, when holding the number of lens modules (and, therefore, cost and power consumption) constant, have the effect of changing the system height, reducing the boresight gain and increasing the gain at scan, with each option showing different trades of height and scan and boresight performance.

IPC Classes  ?

  • H01Q 3/04 - Arrangements for changing or varying the orientation or the shape of the directional pattern of the waves radiated from an antenna or antenna system using mechanical movement of antenna or antenna system as a whole for varying one co-ordinate of the orientation
  • H01Q 19/06 - Combinations of primary active antenna elements and units with secondary devices, e.g. with quasi-optical devices, for giving the antenna a desired directional characteristic using refracting or diffracting devices, e.g. lens

43.

Multi-band lens antenna system

      
Application Number 16576408
Grant Number 11605905
Status In Force
Filing Date 2019-09-19
First Publication Date 2020-03-19
Grant Date 2023-03-14
Owner ALL.SPACE NETWORKS LTD. (United Kingdom)
Inventor
  • Turpin, Jeremiah P.
  • Scarborough, Clinton P.
  • Difonzo, Daniel F.
  • Billman, Brian Murphy

Abstract

A multi-band antenna system that includes a first antenna array and a second antenna array. The first antenna array includes a plurality of lens sets, each including a lens and feed element(s) configured to transmit and/or receive electromagnetic signals that pass through the lens. The second antenna array includes a plurality of antenna elements, each disposed between two of the lenses of the first array.

IPC Classes  ?

  • H01Q 19/06 - Combinations of primary active antenna elements and units with secondary devices, e.g. with quasi-optical devices, for giving the antenna a desired directional characteristic using refracting or diffracting devices, e.g. lens
  • H01Q 25/00 - Antennas or antenna systems providing at least two radiating patterns
  • H01Q 5/42 - Imbricated or interleaved structuresCombined or electromagnetically coupled arrangements, e.g. comprising two or more non-connected fed radiating elements using two or more imbricated arrays

44.

Miscellaneous Design

      
Application Number 018123155
Status Registered
Filing Date 2019-10-25
Registration Date 2020-03-10
Owner ALL.SPACE NETWORKS LIMITED (United Kingdom)
NICE Classes  ? 09 - Scientific and electric apparatus and instruments

Goods & Services

Telecommunications equipment and hardware, namely, antennas, antenna terminals, optical lenses, optical lens arrays, radio frequency lenses, microwave lenses; antennas, antenna terminals, optical lenses, optical lens arrays, radio frequency lenses, microwave lenses for wireless communication systems, broadband point to point and point to multipoint communications systems; fifth generation wireless indoor antennas, fifth generation wireless outdoor antennas, microwave antennas, mobile antennas, and ground station antennas; electro-magnetic and radio spectrum counter-measure systems comprised primarily of electromagnetic apparatus used to generate and measure electromagnetic fields and signal processing and analysis equipment, active radar systems comprised primarily of radar apparatus, radar detectors, radar antennas and radar displays, and systems for radio frequency detection, monitoring, and processing comprised primarily of radio frequency transmitters, radio frequency receivers, radio frequency antennas, computer hardware, frequency meters, frequency and synthesizers, all the aforesaid goods in the field of satellite services and integrated satellite terminals for consumer broadband and aeronautical applications, satellite space-to-ground communications, high-altitude platforms and integrated high-altitude platform terminals, radar, electronic warfare, and 5g terrestrial services.

45.

Dynamic interference reduction for antenna beam tracking systems

      
Application Number 16298491
Grant Number 10797381
Status In Force
Filing Date 2019-03-11
First Publication Date 2019-09-19
Grant Date 2020-10-06
Owner ALL.SPACE NETWORKS LTD. (United Kingdom)
Inventor
  • Difonzo, Daniel F.
  • Turpin, Jeremiah P.

Abstract

An antenna beam tracking system has dynamic interference reduction. The system includes antennas that can form multiple beams, each beam of which can continually track or point its beams independently in various angular directions. A first beam continually tracks and receives (downlink) signals from a desired source or node such as a satellite or terrestrial node which generally has an apparent motion relative to the antenna. A second beam continually tracks and receives potentially harmful interference signals that may arise from different directions. The signals of the second beam are dynamically coupled to the signals in the first beam in such a manner as to effect cancellation or substantial reduction of the interference.

IPC Classes  ?

  • H01Q 1/24 - SupportsMounting means by structural association with other equipment or articles with receiving set
  • H01Q 25/00 - Antennas or antenna systems providing at least two radiating patterns
  • H04W 16/28 - Cell structures using beam steering
  • H04B 7/185 - Space-based or airborne stations

46.

Miscellaneous Design

      
Serial Number 88361197
Status Registered
Filing Date 2019-03-28
Registration Date 2022-05-24
Owner ALL.SPACE NETWORKS LIMITED ()
NICE Classes  ? 09 - Scientific and electric apparatus and instruments

Goods & Services

Telecommunications equipment and hardware, namely, antennas, antenna terminals, optical lenses, optical lens arrays, radio frequency lenses, microwave lenses; antennas, antenna terminals, optical lenses, optical lens arrays, radio frequency lenses, microwave lenses for wireless communication systems, broadband point to point and point to multipoint communications systems; fifth generation wireless indoor antennas, fifth generation wireless outdoor antennas, microwave antennas, mobile antennas, and ground station antennas; electro-magnetic and radio spectrum counter-measure systems comprised primarily of electromagnetic apparatus used to generate and measure electromagnetic fields and signal processing and analysis equipment, active radar systems comprised primarily of radar apparatus, radar detectors, radar antennas and radar displays, and systems for radio frequency detection, monitoring, and processing comprised primarily of radio frequency transmitters, radio frequency receivers, radio frequency antennas, computer hardware, frequency meters, frequency and synthesizers, all the aforesaid goods in the field of satellite services and integrated satellite terminals for consumer broadband and aeronautical applications, satellite space-to-ground communications, high-altitude platforms and integrated high-altitude platform terminals, radar, electronic warfare, and 5G terrestrial services

47.

Lens antenna system

      
Application Number 16173985
Grant Number 10553947
Status In Force
Filing Date 2018-10-29
First Publication Date 2019-03-07
Grant Date 2020-02-04
Owner ALL.SPACE NETWORKS LTD. (United Kingdom)
Inventor
  • Scarborough, Clinton P.
  • Turpin, Jeremiah P.
  • Difonzo, Daniel F.
  • Finney, John

Abstract

An antenna system that includes a plurality of lens sets. Each lens set includes a lens and at least one feed element. At least one feed element is aligned with the lens and configured to direct a signal through the lens at a desired direction.

IPC Classes  ?

  • H01Q 3/46 - Active lenses or reflecting arrays
  • H01Q 3/24 - Arrangements for changing or varying the orientation or the shape of the directional pattern of the waves radiated from an antenna or antenna system varying the orientation by switching energy from one active radiating element to another, e.g. for beam switching
  • H01Q 3/30 - Arrangements for changing or varying the orientation or the shape of the directional pattern of the waves radiated from an antenna or antenna system varying the relative phase or relative amplitude of energisation between two or more active radiating elementsArrangements for changing or varying the orientation or the shape of the directional pattern of the waves radiated from an antenna or antenna system varying the distribution of energy across a radiating aperture varying the phase
  • H01Q 19/06 - Combinations of primary active antenna elements and units with secondary devices, e.g. with quasi-optical devices, for giving the antenna a desired directional characteristic using refracting or diffracting devices, e.g. lens
  • H01Q 21/06 - Arrays of individually energised antenna units similarly polarised and spaced apart
  • H01Q 25/00 - Antennas or antenna systems providing at least two radiating patterns
  • H01Q 1/28 - Adaptation for use in or on aircraft, missiles, satellites, or balloons
  • H01Q 3/14 - Arrangements for changing or varying the orientation or the shape of the directional pattern of the waves radiated from an antenna or antenna system using mechanical relative movement between primary active elements and secondary devices of antennas or antenna systems for varying the relative position of primary active element and a refracting or diffracting device
  • H01Q 21/00 - Antenna arrays or systems
  • H01Q 21/22 - Antenna units of the array energised non-uniformly in amplitude or phase, e.g. tapered array or binomial array
  • H01Q 1/24 - SupportsMounting means by structural association with other equipment or articles with receiving set

48.

REACH BEYOND

      
Application Number 017965500
Status Registered
Filing Date 2018-10-05
Registration Date 2019-09-14
Owner ALL.SPACE NETWORKS LIMITED (United Kingdom)
NICE Classes  ? 09 - Scientific and electric apparatus and instruments

Goods & Services

Telecommunications equipment and hardware, namely, antennas, antenna terminals, optical lenses, optical lens arrays, radio frequency lenses, microwave lenses; antennas, antenna terminals, optical lenses, optical lens arrays, radio frequency lenses, microwave lenses for wireless communication systems, broadband point to point and point to multipoint communications systems; fifth generation wireless indoor antennas, fifth generation wireless outdoor antennas, microwave antennas, mobile antennas, and ground station antennas; electro-magnetic and radio spectrum counter-measure systems, active radar systems, and systems for radio frequency detection, monitoring, and processing.

49.

System and method for providing a compact, flat, microwave lens with wide angular field of regard and wideband operation

      
Application Number 15849049
Grant Number 11894610
Status In Force
Filing Date 2017-12-20
First Publication Date 2018-06-28
Grant Date 2024-02-06
Owner All.Space Networks Limited (United Kingdom)
Inventor
  • Turpin, Jeremiah P.
  • Scarborough, Clinton P.
  • Difonzo, Daniel F.
  • Finney, John

Abstract

A system designs a thin and relatively flat microwave focusing lens that can produce multiple simultaneous beams, using readily-available isotropic dielectric materials, and having a gradient-index (GRIN) profile. The design optimizes the lens to achieve beam scanning and/or multiple beams over a wide field of regard (FOR) with broad bandwidth and a very short focal length compared with conventional lenses. The lens can be used individually or as an element in a more complex antenna having multiple lenses in various orientations that are independently switched, selected and/or excited simultaneously as elements in a phased array. The antenna terminal incorporates such lens into an array of lenses along with one or more feeds to produce single or multiple beams covering a broad field of regard for such applications as satellite communications on-the-move, cellular, broadband point-point or point-multipoint and other terrestrial or satellite communications systems. The lens and array design support multiple simultaneous independently steerable beams as well as null placement for interference cancellation.

IPC Classes  ?

  • H01Q 15/02 - Refracting or diffracting devices, e.g. lens, prism
  • G06F 30/20 - Design optimisation, verification or simulation
  • H01Q 25/00 - Antennas or antenna systems providing at least two radiating patterns
  • H01Q 15/08 - Refracting or diffracting devices, e.g. lens, prism formed of solid dielectric material
  • H01Q 1/28 - Adaptation for use in or on aircraft, missiles, satellites, or balloons
  • H01Q 1/48 - Earthing meansEarth screensCounterpoises
  • H01Q 19/06 - Combinations of primary active antenna elements and units with secondary devices, e.g. with quasi-optical devices, for giving the antenna a desired directional characteristic using refracting or diffracting devices, e.g. lens