HIGH COMFORT ENDURANCE HAPTIC CUSHION

    公开(公告)号:US20250051016A1

    公开(公告)日:2025-02-13

    申请号:US18924845

    申请日:2024-10-23

    Abstract: A system is disclosed herein, including a cushion including a plurality of tactors and a plurality of air bladders disposed adjacent the plurality of tactors, a pump assembly operably connected to the plurality of bladders, a processor, and a memory operatively coupled to the processor. The memory includes instructions stored thereon that, when executed by the processor, cause the processor to determine an inflation sequence for the plurality of air bladders, determine a deflation sequence for the plurality of air bladders, output commands to the pump assembly corresponding to the inflation sequence and the deflation sequence, and output vibrate commands to the plurality of tactors.

    DUAL STRIKER TIMING BASED MASS SCALAR DETERMINATION

    公开(公告)号:US20240317409A1

    公开(公告)日:2024-09-26

    申请号:US18463103

    申请日:2023-09-07

    CPC classification number: B64D25/10

    Abstract: A method is disclosed herein. The method includes determining, by a processor, a first time value in response to a switch being actuated a first time by a first striker, determining, by the processor, a second time value in response to the switch being actuated a second time by a second striker, the second striker disposed a first distance from the first striker and the second time value being after the first time value, calculating, by the processor, a change in time between the first time value and the second time value, and adjusting, by the processor, a timing sequence based on the change in time.

    EJECTION SEAT ACTIVE ROLL CORRECTION
    4.
    发明公开

    公开(公告)号:US20240076048A1

    公开(公告)日:2024-03-07

    申请号:US17902726

    申请日:2022-09-02

    CPC classification number: B64D25/10 G05D1/0808

    Abstract: A roll stabilization system for an aircraft ejection seat may be provided. An integral seat sequencer may activate an ejection sequence causing an aircraft ejection seat to be ejected from an aircraft. In various instances, particularly with lighter occupants of the aircraft ejection seat, the aircraft ejection seat may begin a rotational movement. To ameliorate this rotational movement, a roll correction rocket motor is installed on the aircraft ejection seat and selectively activated by the integral seat sequencer in the event that an undesired rotational movement is detected.

    Retention systems and methods for ejection seats

    公开(公告)号:US11851194B2

    公开(公告)日:2023-12-26

    申请号:US17462420

    申请日:2021-08-31

    CPC classification number: B64D25/10 B64D25/06

    Abstract: A method may include receiving, via a processor, an ejection initiation signal indicating an ejection event for an ejection seat of an aircraft has been initiated; commanding, via the processor, a retraction mechanism to retract a cuff assembly towards a seat back of the ejection seat in response to the ejection initiation signal; and commanding, via the processor, a guillotine to sever a cord coupled to the cuff assembly.

    Drogue bridle connection assembly for ejection seats

    公开(公告)号:US11618577B2

    公开(公告)日:2023-04-04

    申请号:US17032464

    申请日:2020-09-25

    Abstract: A drogue bridle attachment assembly may comprise a housing, a lock pin, jackscrew gear pin, and a drive gear pin. The housing may define a bridle opening. The lock pin may be configured to translate into the bridle opening. The jackscrew gear pin may include a threaded portion and a gear portion. The threaded portion may engage a threaded opening in the lock pin. The drive gear pin may include a drive gear portion intermeshed with the gear portion of the jackscrew gear pin.

    Aircraft escape system and ejection seat sequencer for ejection systems

    公开(公告)号:US11548649B2

    公开(公告)日:2023-01-10

    申请号:US17125494

    申请日:2020-12-17

    Inventor: John Hampton

    Abstract: An article of manufacture may include a tangible, non-transitory computer-readable storage medium having instructions stored thereon for controlling deployment of aircraft escape and ejection seat subsystems. The instructions, in response to execution by a sequencer, cause the sequencer to perform operations, which may comprise receiving, by the sequencer, a power input; sending, by the sequencer, a first deploy signal to a first aircraft escape subsystem; and sending, by the sequencer, a second deploy signal to a first ejection seat subsystem.

    Automatic mode selection system
    10.
    发明授权

    公开(公告)号:US11505326B2

    公开(公告)日:2022-11-22

    申请号:US17104623

    申请日:2020-11-25

    Abstract: A system for automatic ejection mode selection may comprise: a first ejection seat configured to receive a first pilot; a second ejection seat configured to receive a second pilot or a non-pilot; a user detection system configured to determine whether the second ejection seat has the second pilot, the non-pilot, or is empty; and a controller configured to adjust an ejection system in response to determining whether the second ejection seat has the second pilot, the non-pilot, or is empty.

Patent Agency Ranking