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公开(公告)号:US12116144B2
公开(公告)日:2024-10-15
申请号:US17889689
申请日:2022-08-17
申请人: AIRBUS HELICOPTERS
CPC分类号: B64F1/125 , B64C25/52 , B64C2025/325
摘要: An anchor for an aircraft. The anchor comprises a jack comprising a housing and a head that is able to move in translation in relation to the housing along an elevation axis, the head having three degrees of rotational freedom respectively about a longitudinal axis as well as a transverse axis and the elevation axis, the anchor comprising a member for taking up forces surrounding the jack and provided with a fastening suitable for being secured to the aircraft.
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公开(公告)号:US12116128B2
公开(公告)日:2024-10-15
申请号:US18504553
申请日:2023-11-08
申请人: KNIGHTWERX INC.
发明人: Daniel Baumgartner
IPC分类号: B64C39/00 , B64C11/46 , B64C25/32 , B64C29/02 , B64C39/02 , B64D9/00 , B64D17/80 , F41G3/06 , F41G3/08 , F41G3/16 , G02B23/10 , G05D1/00 , G09G3/00 , B64U10/25 , B64U50/13
CPC分类号: B64C39/024 , B64C11/46 , B64C25/32 , B64C29/02 , B64D9/00 , B64D17/80 , F41G3/06 , F41G3/08 , F41G3/165 , G02B23/10 , G05D1/106 , G09G3/001 , B64U10/25 , B64U50/13 , B64U2201/00 , G09G2320/0686
摘要: A tactical system includes a first HUD system mountable to a first weapon and a second HUD system mountable to a second weapon. The first HUD system includes sensors providing position and orientation data of the first weapon, a processor to calculate a target position based on the position and orientation data, and a communications module to communicate the target position over a network. The second HUD system includes sensors providing position and orientation data of the second weapon, a communications module configured to import the target position from the network, and a processor to: calculate a position and an orientation of the second weapon based on the position and orientation data of the second weapon; calculate a target vector based on the target position and the position of the second weapon; and generate a target finder visualization based on the target vector and the orientation of the second weapon.
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公开(公告)号:US12103707B2
公开(公告)日:2024-10-01
申请号:US18236169
申请日:2023-08-21
申请人: AEROVIRONMENT, INC.
发明人: Tom Millspaugh
IPC分类号: B64F1/22 , B64C25/32 , B64C39/02 , B64F1/223 , B64U10/25 , B64U50/19 , B64U50/31 , B64U80/50 , B64U80/86
CPC分类号: B64F1/224 , B64C25/32 , B64C39/024 , B64U10/25 , B64U50/19 , B64U50/31 , B64U80/50 , B64U80/86
摘要: Systems, devices, and methods for a ground support system for an unmanned aerial vehicle (UAV) including: at least one handling fixture, where each handling fixture is configured to support at least one wing panel of the UAV; and at least one dolly, where each dolly is configured to receive at least one landing pod of the UAV, and where each landing pod supports at least one wing panel of the UAV; where the at least one handling fixture and the at least one dolly are configured to move and rotate two or more wing panels to align the two or more wing panels with each other for assembly of the UAV; and where the at least one dolly further allows for transportation of the UAV over uneven terrain.
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公开(公告)号:US20240294251A1
公开(公告)日:2024-09-05
申请号:US18509696
申请日:2023-11-15
发明人: Axel FINK , Reynaldo OIOLI-NETO
CPC分类号: B64C25/36 , B64C25/06 , B64C25/58 , B64C2025/325
摘要: A rotorcraft comprising a fuselage forming at least one lower lateral fuselage compartment with at least a first fitting, a second fitting, and a third fitting; and at least one non-retractable wheel-type landing gear that comprises: at least one wheel; a shock absorber with a shock absorber tube having an open end and an axially opposed closed end, and a shock absorber rod telescopically mounted to the shock absorber tube via the open end; a first fixation provided close to the open end on the shock absorber tube and connected to the first fitting; a second fixation provided close to the closed end on the shock absorber tube and connected to the second fitting; and a third fixation provided close to the closed end on the shock absorber tube and connected to the third fitting.
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公开(公告)号:US20240228061A1
公开(公告)日:2024-07-11
申请号:US18236169
申请日:2023-08-21
申请人: AEROVIRONMENT, INC.
发明人: Tom Millspaugh
CPC分类号: B64F1/224 , B64C25/32 , B64C39/024 , B64U80/86
摘要: Systems, devices, and methods for a ground support system for an unmanned aerial vehicle (UAV) including: at least one handling fixture, where each handling fixture is configured to support at least one wing panel of the UAV; and at least one dolly, where each dolly is configured to receive at least one landing pod of the UAV, and where each landing pod supports at least one wing panel of the UAV; where the at least one handling fixture and the at least one dolly are configured to move and rotate two or more wing panels to align the two or more wing panels with each other for assembly of the UAV; and where the at least one dolly further allows for transportation of the UAV over uneven terrain.
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公开(公告)号:US20240203267A1
公开(公告)日:2024-06-20
申请号:US18204529
申请日:2023-06-01
IPC分类号: G08G5/00 , B64C25/10 , B64C25/32 , B64C39/02 , B64U10/10 , B64U30/20 , B64U50/13 , B64U50/19 , B64U101/00
CPC分类号: G08G5/0034 , B64C25/10 , B64C25/32 , B64C39/024 , G08G5/0069 , B64C2025/325 , B64U10/10 , B64U30/20 , B64U50/13 , B64U50/19 , B64U2101/00 , B64U2201/10
摘要: An unmanned helicopter platform includes a fuselage, a tail coupled with the fuselage, a payload rail coupled with and extending along the fuselage and a main rotor assembly coupled with the fuselage. The tail includes a tail rotor and a tail rotor motor. The tail is removably coupled to the fuselage. The main rotor assembly includes a main rotor having an axis of rotation and a main rotor motor.
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公开(公告)号:US11970268B2
公开(公告)日:2024-04-30
申请号:US17784930
申请日:2020-12-14
发明人: Kevin Garanger , Jeremy Epps , Eric Feron , Michael Miller
CPC分类号: B64C39/024 , B64C25/32 , B64C37/02 , B64D27/24 , B64U30/20 , B64U50/19 , B64U2201/20
摘要: A fractal unmanned aircraft system (200) includes a first module (100), a second module (100) and a third module, (100) each having a top member (120) and a first thruster (130) affixed thereto. Each module (100) is laterally coupled to each other. A fourth module (100) has a bottom that is affixed to the top members (120) of the first module (100), the second module (100) and the third module (100) so as to form a tetrahedral structure. A power source (220) supplies power to the first thrusters (130). A control circuit (222) controls the unmanned aircraft system so as to cause the fractal unmanned aircraft system (200) to fly in a controlled manner.
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公开(公告)号:US20240076038A1
公开(公告)日:2024-03-07
申请号:US18504553
申请日:2023-11-08
申请人: KNIGHTWERX INC.
发明人: Daniel Baumgartner
IPC分类号: B64C39/02 , B64C11/46 , B64C25/32 , B64C29/02 , B64D9/00 , B64D17/80 , F41G3/06 , F41G3/08 , F41G3/16 , G02B23/10 , G05D1/10 , G09G3/00
CPC分类号: B64C39/024 , B64C11/46 , B64C25/32 , B64C29/02 , B64D9/00 , B64D17/80 , F41G3/06 , F41G3/08 , F41G3/165 , G02B23/10 , G05D1/106 , G09G3/001 , B64U10/25
摘要: Systems and methods for a weapon mountable tactical heads-up display (HUD) are provided. The HUD may include a 9 degrees of freedom (9DOF) sensor, a target library, and a target finder visualization. The target library may store respective ballistic information for each target of a plurality of targets. The respective ballistic information may include a target vector for each target of the plurality of targets. The target vector may be calculated based on data received from the 9DOF sensor. The target finder visualization may allow a shooter to locate a selected target of the plurality of targets. The target finder visualization may be based on the target vector.
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公开(公告)号:US20240043113A1
公开(公告)日:2024-02-08
申请号:US18365310
申请日:2023-08-04
CPC分类号: B64C25/405 , F16D27/14
摘要: A powered clutch actuator assembly for integration with a clutch assembly is provided. The actuator and clutch assemblies, sized to fit within constraints of an aircraft landing gear wheel-mounted taxi drive system, are engineered to occupy a default neutral disengaged position that prevents torque transfer when torque to move the aircraft should not be transferred to the taxi drive system. Multiple solenoids and diodes power rotational motion of the actuator assembly to move a bi-directional clutch component in a desired rotational direction during torque transfer. A locking solenoid automatically locks and maintains the actuator assembly in a neutral disengaged condition when none of the solenoids are powered and disengages the actuator assembly when one solenoid is powered to cause rotation of the actuator assembly. Solenoid supports structured to operate as integral heat sinks may direct heat to an on-aircraft heat sink, prolonging the working life of the actuator assembly.
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10.
公开(公告)号:US11852621B2
公开(公告)日:2023-12-26
申请号:US17211997
申请日:2021-03-25
IPC分类号: G01N33/24 , B64C25/32 , B64C39/02 , G01N19/00 , B64U101/00
CPC分类号: G01N33/24 , B64C25/32 , B64C39/024 , G01N19/00 , B64U2101/00 , G01N2033/245
摘要: A system for monitoring tilled floor conditions within a field includes a sensor frame and a tilled floor sensing assembly supported on the sensor frame. The assembly, in turn, includes a plurality of pins configured to be extended relative to the sensor frame such that each pin penetrates a top surface of the field. Furthermore, the assembly includes a plurality of position sensors, with each position sensor configured to capture data indicative of a position of a given pin of the plurality of pins relative to the sensor frame. Moreover, the assembly includes a plurality of force sensors, with each force sensor configured to capture data indicative of a force being applied to a given pin of the plurality of pins. Additionally, the data captured by the plurality of position sensors and the data captured by the plurality of force sensors is indicative of a tilled floor profile of the field.
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