Patents Assigned to BAE Systems plc
-
Publication number: 20240384899Abstract: In some examples, an apparatus comprises a first working fluid circuit comprising a first working fluid, a heat exchanger fluidly coupled to and in thermal communication with the first working fluid circuit, the heat exchanger to transfer thermal energy from a heat source stream to the first working fluid within the first working fluid circuit, a recuperator fluidly coupled to and in thermal communication with the first working fluid circuit and disposed downstream of the heat exchanger, a first condenser fluidly coupled to and in thermal communication with the first working fluid circuit and disposed downstream of the recuperator, a second working fluid circuit comprising a second working fluid, the second working fluid circuit coupled to and in thermal communication with the first condenser, a second condenser fluidly coupled to and in thermal communication with the second working fluid circuit and disposed downstream of the first condenser, and a third working fluid circuit comprising a third working fluidType: ApplicationFiled: September 2, 2022Publication date: November 21, 2024Applicant: BAE SYSTEMS plcInventors: Madan Pal, Darren James Goodman, Taimoor Rana, Callum Oliver Shaikh
-
Patent number: 12145717Abstract: A vehicle control system (110) for use with at least one fluidic control effector (102) for a vehicle, the vehicle control system (110) comprising a controller (110), wherein the controller is configured to: receive a vehicle control input indicating a demanded vehicle manoeuvre, wherein the input is further configured to receive condition data; determine a fluid mass-flow for the at least one fluid control effector based on the received vehicle control input and the condition data, wherein the relationship between the fluid mass-flow and the vehicle control input is substantially non-linear; and output data relating to the determined fluid mass-flow to effect the demanded vehicle manoeuvre, wherein the fluid mass-flow is determined to provide a substantially linear relationship between the vehicle control input and the effected demanded vehicle manoeuvre.Type: GrantFiled: September 3, 2020Date of Patent: November 19, 2024Assignee: BAE Systems plcInventors: Clyde Warsop, William James Crowther, Ian Lunnon
-
Publication number: 20240376959Abstract: According to the present invention there is provided a vibration control system comprising: a resonator comprising: a base attachable to an external body; a control element; and one or more connection elements each having a resilient portion, wherein the control element is resiliently connected to the base by the one or more connection elements such that relative movement between the control element and the base is facilitated by the one or more connection elements; and a driving mechanism, wherein the resonator comprises at least a part of the driving mechanism.Type: ApplicationFiled: September 12, 2022Publication date: November 14, 2024Applicant: BAE SYSTEMS plcInventors: Jordan Cheer, Stephen Daley, Lawrence Singleton
-
Publication number: 20240379086Abstract: In some examples, an acoustic absorbing structure comprises a surface comprising an array of apertures, each aperture defining an opening for a corresponding channel, each channel forming a non-resonant acoustic attenuation structure with an axially decreasing cross-section over at least a portion of the length of the channel.Type: ApplicationFiled: March 23, 2022Publication date: November 14, 2024Applicant: BAE SYSTEMS PLCInventors: Ewan David FINLAYSON, Alastair Paul HIBBINS, Sir John Roy SAMBLES, Gwyn RICHARDS, David PATIENCE
-
Publication number: 20240377144Abstract: A cooling system (100) for removing heat from a heat source (1000) fluid cooling circuit (1100). The cooling system (100) comprises a first fluid manifold (200) for flow of a heat transfer fluid, the first fluid manifold (200) comprising a flow inlet (210) and a flow outlet (212); a heat exchanger (310) and a heat sink unit (410) each in heat transfer communication with the first fluid manifold (200). In a first mode of operation, heat transfer fluid enters the flow inlet (210) and part of the heat transfer fluid flow is controlled to be in heat transfer communication with the heat exchanger (310), and the remainder of the heat transfer fluid flow is controlled to be in heat transfer communication with the heat sink unit (410). In a second mode of operation, heat transfer fluid enters the flow inlet (210) and all of the heat transfer fluid flow is controlled to first be in heat transfer communication with the heat sink unit (410) and then in heat transfer communication with the heat exchanger (310).Type: ApplicationFiled: July 7, 2022Publication date: November 14, 2024Applicant: BAE Systems plcInventor: Evaldas Greiciunas
-
Publication number: 20240376949Abstract: According to the present invention there is provided a resonator comprising: a base attachable to an external body; a control element; and one or more connection elements each having a resilient spiral portion, wherein the control element is resiliently connected to the base by the one or more connection elements such that relative movement between the control element and the base is facilitated by the one or more connection elements.Type: ApplicationFiled: September 12, 2022Publication date: November 14, 2024Applicant: BAE SYSTEMS plcInventors: Jordan Cheer, Stephen Daley, Lawrence Singleton
-
Patent number: 12143374Abstract: A method of providing secure communication between first and second devices comprises the first device and the second device connecting to a server via a secure communication channel. Encryption keys for the devices are generated and data relating to the encryption keys are exchanged via the server in the secure communication channel. A peer-to-peer connection for exchanging data is generated using encrypted connection information for the devices.Type: GrantFiled: October 22, 2020Date of Patent: November 12, 2024Assignee: BAE Systems plcInventors: Ashley Kurtis, Kristian Daniel
-
Patent number: 12140528Abstract: A corrosion sensor is described. The corrosion sensor comprises a substrate 10 and a patterned conductive layer provided on the substrate 10, wherein the conductive layer defines: a common terminal; a set of terminals, including a first terminal and a second terminal; and a set of sensing elements, including a first sensing element and a second sensing element; wherein respective sensing elements of the set thereof are electrically coupled to the common terminal and to respective terminals of the set thereof, such that the respective terminals of the set thereof are specific to the respective sensing elements of the set thereof.Type: GrantFiled: June 28, 2021Date of Patent: November 12, 2024Assignee: BAE Systems plcInventors: Mark David Balmond, Ian Michael Sturland, David William Gough, Christopher Colin Figgures
-
Publication number: 20240367318Abstract: A robot cell, having a cell floor defining an array of nodes corresponding with a predetermined two-dimensional coordinate system and defining a volume for receiving a workpiece W therein and accessible by a human operator, is described. The robot cell comprises: a set of robots, including a first robot, having respective bases, end effectors and working envelopes and defining respective three-dimensional coordinate systems, located according to the array of nodes; a set of detectors, including a first detector, configured to detect respective locations and/or bearings of the set of robots using a set of targets disposed on and/or in the cell floor; a safety system, configured to alert the human operator; and a controller, communicatively coupled to the set of robots and to the set of detectors, configured to control movement of the set of robots using the detected respective locations and/or bearings of the set of robots.Type: ApplicationFiled: April 13, 2022Publication date: November 7, 2024Applicant: BAE Systems plcInventors: Jane Alexandra Byford, Martin Knott, Daniel James Middleton, Jake Butterworth, Craig Philip Turnbull
-
Publication number: 20240362463Abstract: The invention relates to a system and method for detecting anomalous system behaviour. The system comprises a plurality of sensors and a trained autoencoder. The method of training comprises: obtaining training data and test data comprising multiple data records for at least one engineering asset which corresponds to the engineering asset whose behaviour is to be classified, wherein the data records comprise a plurality of sensor readings for the engineering asset; fitting the autoencoder to the obtained training data; running the test data through the encoder of the fitted autoencoder to obtain encodings of the test data; generating a plurality of data sets from the obtained encodings, wherein the generated plurality of data sets include under-represented data sets; cloning the fitted autoencoder to create a cloned autoencoder for each of the generated plurality of data sets; and aggregating the cloned autoencoders to form an over-arching autoencoder.Type: ApplicationFiled: September 15, 2022Publication date: October 31, 2024Applicant: BAE SYSTEMS plcInventors: Samuel Horry, Richard Edward John Nicklin, Hans-Heinrich Mai
-
Patent number: 12123687Abstract: There is provided a projectile, a system and a related method of operation of a projectile comprising: a front ogive section; an aft section; and a control module; wherein the front ogive section is rotatably connected to the aft section by a coupling device, the front ogive section further comprising an asymmetric surface such that the asymmetric surface exerts an imbalance upon the projectile, where in use, the angular rotation of the front ogive section can be selectively adjusted relative to the aft section by commands from the control module to the coupling device influencing a helical trajectory of the projectile in flight thereby causing a change in direction thereby steering the projectile towards a target.Type: GrantFiled: July 21, 2021Date of Patent: October 22, 2024Assignee: BAE SYSTEMS PLCInventor: James Joshua Norris
-
Patent number: 12123785Abstract: A system to determine a temperature corrected pressure of a medium in a pressure transducer is disclosed. The system comprises a first circuitry to obtain a first value related to a vibration frequency of the vibration of a pressure sensitive vibration member; a second circuity to obtain a second value related to a vibration amplitude of the vibration of the vibration member; and a third circuity to use the first value and the second value to determine the temperature corrected pressure of the medium based on a predetermined relationship between the vibration frequency and the vibration amplitude.Type: GrantFiled: March 10, 2020Date of Patent: October 22, 2024Assignee: BAE SYSTEMS plcInventor: David Christopher D'Oyly-Watkins
-
Patent number: 12115717Abstract: Apparatus (100) for use in space, the apparatus (100) comprising: a feedstock storage module (108) for storing a feedstock; a heating module (110) coupled to the feedstock storage module (108) and configured to heat the feedstock; an extrusion nozzle (112) coupled to the heating module (110) and configured to extrude heated feedstock from the apparatus (110); and one or more thrusters (118) configured to provide a propulsive force to the apparatus (100).Type: GrantFiled: August 28, 2019Date of Patent: October 15, 2024Assignee: BAE Systems plcInventor: Nicholas Giacomo Robert Colosimo
-
Patent number: 12116104Abstract: There is disclosed a rotorcraft comprising: an array of lift devices; a pilot housing; connecting lines attaching the pilot housing to the array of lift devices; and an actuator interface at the pilot housing such that the pilot can 5 steer the rotorcraft.Type: GrantFiled: April 29, 2021Date of Patent: October 15, 2024Assignee: BAE Systems plcInventor: David Charles Atkinson
-
Publication number: 20240337382Abstract: A jet engine exhaust assembly 20 is disclosed. The exhaust assembly comprises a double-walled exhaust duct 22 comprising an inner wall defining the inner profile of the duct and an outer wall spaced apart from the outer surface of said inner wall to define a cooling space 21 therebetween. The double-walled exhaust duct 20 is a structural load bearing component.Type: ApplicationFiled: August 26, 2016Publication date: October 10, 2024Applicant: BAE SYSTEMS PLCInventors: JONATHAN PETER IRVING, STEPHEN CHARLES NUNN, COLIN WHAITES
-
Patent number: 12113280Abstract: An airborne redirection unit (ARU), for deflecting an RF energy beam, the ARU comprising: A canopy comprising a surface for slowing the rate of descent, A beam director supported at the canopy, the ARU being configured to focus the RF energy beam.Type: GrantFiled: May 7, 2020Date of Patent: October 8, 2024Assignee: BAE Systems plcInventors: Nicholas Giacomo Robert Colosimo, Keith Antony Rigby, Christopher Charles Rawlinson Jones
-
Patent number: 12111141Abstract: According to the present invention, there is provided an ammunition belt link comprising, a sprung wire, said sprung wire arranged to form a first receiving portion suitable for retaining a first ammunition cartridge, a second receiving portion suitable for retaining a second ammunition cartridge, a spacer between said first receiving and second receiving portions, an ammunition cartridge locator aide, said locator aid locates in an ejector groove of a received cartridge and, the wire ammunition belt link further comprising a support surface suitable for retaining the first and/or second ammunition cartridge.Type: GrantFiled: July 9, 2021Date of Patent: October 8, 2024Assignee: BAE SYSTEMS PLCInventors: Joshua Matthew Stubbs, Nathan William Rowe
-
Patent number: 12111139Abstract: There is provided a vehicle for protecting an entity against directed-energy weapons, comprising: a housing; and a shield for absorbing or reflecting a laser beam, the shield, in use, extending in a plane from the housing. There is also provided a system of vehicles and a method of coordinating a plurality of vehicles to protect an entity against directed-energy weapons.Type: GrantFiled: August 18, 2022Date of Patent: October 8, 2024Assignee: BAE Systems plcInventor: Nicholas Giacomo Robert Colosimo
-
Publication number: 20240333692Abstract: A method of creating one or more secure tunnels within a network, a router node implementing the method and a network comprising a plurality of router nodes. The method comprises: connecting a first router node to the network, wherein the first router node comprises a plurality of bearer interfaces, each having a virtual routing and forwarding VRF module; receiving, from neighbouring nodes in the network, at least one loopback address for at least one bearer interface in the neighbouring nodes; and detecting, using the first router node, one or more routing prefixes associated with a traffic or management tunnel within the at least one received loopback address.Type: ApplicationFiled: July 13, 2022Publication date: October 3, 2024Applicant: BAE SYSTEMS plcInventors: David James SULLIVAN, Neville James MICKLEWRIGHT
-
Patent number: 12104529Abstract: A thermodynamic apparatus (10) comprising a compressor module (100), a turbine module (200), and a regenerative heat exchanger (300) centred on a central axis (12). The compressor module (100), turbine module (200) and regenerative heat exchanger (300) are arranged in series along the central axis (12) such that the regenerative heat exchanger (300) is provided between the compressor module (100) and the turbine module (200).Type: GrantFiled: December 8, 2023Date of Patent: October 1, 2024Assignee: BAE SYSTEMS PLCInventor: James William Spain