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    A SYSTEM COMPRISING AN AUTONMOUS VEHICLE AND AN AUTONOMOUS DELIVERY DRONE
    2.
    发明公开
    A SYSTEM COMPRISING AN AUTONMOUS VEHICLE AND AN AUTONOMOUS DELIVERY DRONE 审中-公开

    公开(公告)号：EP4513130A1

    公开(公告)日：2025-02-26

    申请号：EP23275125.5

    申请日：2023-08-23

    Applicant: BAE SYSTEMS plc

    Inventor： The designation of the inventor has not yet been filed

    IPC: F41H7/00 ,  B64C39/02 ,  B64U80/00

    Abstract: A system (100) comprising a first autonomous vehicle (300) configured to carry an ammunition subcomponent (400). The first autonomous vehicle (300) comprises an ammunition subcomponent receiving system (302). The system further comprises an autonomous heavy lift drone air-vehicle (2000) comprising an ammunition subcomponent loading system (2202) configured for loading the first autonomous vehicle (300) with the ammunition subcomponent (400) by delivering the ammunition subcomponent (400) to the ammunition subcomponent receiving system (302) of the first autonomous vehicle (300).

    EXTENDABLE SEAT PAN
    3.
    发明公开
    EXTENDABLE SEAT PAN 审中-公开

    公开(公告)号：EP4512719A1

    公开(公告)日：2025-02-26

    申请号：EP24195433.8

    申请日：2024-08-20

    Applicant: Dehns

    Inventor： DOWTY, Mark B. ,  RAO, Sreekanth ,  ACHARYA, Pradeep

    IPC: B64D11/06 ,  B60N2/02 ,  B60N2/62

    Abstract: A seat pan (106) includes a break over function. The break over enables downward motion of a portion of the seat pan. The downward motion of the portion of the seat pan allows a distance between passenger seats to be reduced while maintaining a minimum required egress distance between the passenger seats. The breakover seat pan assists in egress. The portion of the seat pan may be actuated upwards to increase the length of the seat pan while a passenger is seated. The seat pan thus creates a supported seat surface when an occupant sits on the seat while presenting with a reduced surface when not occupied.

    PANELS
    4.
    发明公开
    PANELS 审中-公开

    公开(公告)号：EP4512716A1

    公开(公告)日：2025-02-26

    申请号：EP23192497.8

    申请日：2023-08-21

    Applicant: B/E Aerospace (UK) Limited

    Inventor： GROCOTT, Edward John Reynard ,  WIEBE, Zac Lewis ,  OHL, Craig T ,  BLUMBERG, Rafael

    IPC: B64D11/04

    Abstract: A panel (28P, 30, 32, 28S) for use in the construction of a galley (10) of an aircraft (2) is disclosed. The panel comprises a frame (50), at least one insulation panel (40, 42,44, 46, 48), and a cover panel (54). The frame comprises first and second opposing faces (88, 90) and one or more edge faces (92), and each edge face extends between the first and second faces. The cover panel has first and second opposing faces (104, 106) and each insulation panel has first and second opposing faces (100, 102). One or more of the edge faces of the frame define a housing aperture (94) and the frame is fixed to the cover panel with the first face of the frame adjacent to the second face of the cover panel. The housing aperture is configured to receive the at least one insulation panel, and at least one insulation panel is fixed to the cover panel with the first face of the at least one insulation panel adjacent to the second face of the cover panel.

    SPRAY GUN ASSEMBLIES, METHODS AND SYSTEMS FOR APPLYING COATING WITH PLURAL COMPONENTS
    5.
    发明公开
    SPRAY GUN ASSEMBLIES, METHODS AND SYSTEMS FOR APPLYING COATING WITH PLURAL COMPONENTS 审中-公开

    公开(公告)号：EP4512535A1

    公开(公告)日：2025-02-26

    申请号：EP24189392.4

    申请日：2024-07-18

    Applicant: The Boeing Company

    Inventor： Schuette, Waynie M. ,  Adams, Scott A. ,  Dillard, Anthony E.

    IPC: B05B7/24 ,  B05B15/25 ,  B05B15/58 ,  B05B7/08 ,  B64F5/10

    Abstract: A spray gun assembly (100) for applying a coating with plural components includes a nozzle (102), a main pneumatic inlet (104), an atomizing air flow path (110), a fan air flow path (112), a colloidal feed inlet (114), an internal atomizing outlet (120), a pressurized feed inlet (122), and a catalyst outlet (128). The nozzle includes a main atomizing outlet and a fan air outlet. The main pneumatic inlet receives compressed air from a compressed air source (108). The colloidal feed inlet receives a colloidal suspension component of the coating via gravity feed from a gravity feed container (116). The pressurized feed inlet receives a catalyst component of the coating from a pressurized feed container (124). The catalyst outlet expels the catalyst component in the fan air flow path proximate the nozzle. A method for applying a coating with plural components is also provided. A system includes the gravity feed container, the pressurized feed container and the spray gun assembly.

    INTEGRATED BUSBAR HEATER FOR ICE PROTECTION SYSTEMS
    7.
    发明公开
    INTEGRATED BUSBAR HEATER FOR ICE PROTECTION SYSTEMS 审中-公开

    公开(公告)号：EP4484295A3

    公开(公告)日：2025-02-26

    申请号：EP24213941.8

    申请日：2021-03-31

    Applicant: Goodrich Corporation

    Inventor： CARPINO II, Richard J.

    IPC: B64D15/12 ,  B64D15/20

    Abstract: A control system (200) for a de-icing system (400) may comprise an electrical heating mat (402,404), a controller (127), and a tangible, non-transitory memory configured to communicate with the controller, the tangible, non-transitory memory having instructions stored thereon that, in response to execution by the controller, cause the controller to perform operations comprising: receiving (802), by the controller, an enable command from a control interface (175); polling (804), by the controller, a sensor (202) for a sensor data; receiving (806), by the controller, the sensor data from the sensor; passing (808), by the controller, the sensor data to an ice protection logic (204); determining (810), by the controller via the ice protection logic, an icing condition; and applying (812), by the controller, an electrical current to a first busbar portion (604A-1) of the electrical heating mat.

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