Load-Bearing Composite Platform
    1.
    发明申请

    公开(公告)号:US20230036562A1

    公开(公告)日:2023-02-02

    申请号:US17390421

    申请日:2021-07-30

    Abstract: The present disclosure provides a load-bearing composite platform. The platform includes a core layer, first and second reinforcement layers, and a frame. The core layer includes a structural sublayer, a force distribution sublayer, and an abrasion prevention sublayer. The first reinforcement layer is adhered to the force distribution sublayer, and the second reinforcement layer is adhered to the structural sublayer. The second reinforcement layer is an inverse of the first reinforcement layer. The frame surrounds the first reinforcement layer, the second reinforcement layer, and the core layer.

    Filter Cartridge with Turbulence Generating Features

    公开(公告)号:US20210331110A1

    公开(公告)日:2021-10-28

    申请号:US17237247

    申请日:2021-04-22

    Abstract: The present disclosure provides a filter cartridge for a facepiece respirator mask body. The filter cartridge includes a cover, a base, and a filter medium. The cover has a top surface, a cover sidewall, cover support elements, and an inhalation vent. The cover support elements extend downwardly from the top surface. The inhalation vent is located at least primarily in the cover sidewall. The base has a bottom surface, a base sidewall, base support elements, and an inhalation port. The base support elements extend upwardly from the bottom surface. The inhalation port is located in the bottom surface. The base and the cover collectively define an interior compartment. The filter medium is sandwiched between the base support elements and the cover support elements in a manner that divides the interior compartment into an upper chamber and a lower chamber.

    Autonomous guidance and flight control system implementation on a partial-authority aircraft

    公开(公告)号:US12077282B2

    公开(公告)日:2024-09-03

    申请号:US17719967

    申请日:2022-04-13

    CPC classification number: B64C13/503 B64D43/00 G08G5/003

    Abstract: This disclosure provides a means to implement an autonomous guidance and flight control system on a partial authority aircraft. One embodiment of the disclosure includes receiving a control command result, filtering the control command result into a low frequency component and a high frequency component, directing the low frequency component to at least one trim servomechanism and directing the high frequency component to at least one stability augmentation stabilizer servomechanism, linking outputs from the trim servomechanism and the stability augmentation stabilizer servomechanism for actuating a pilot control configured to control rotors, and actuating at least one rotor. The low frequency component includes frequencies below a break frequency and the high frequency component includes frequencies above the break frequency. The break frequency is established by rate and position of the at least one servomechanism.

    Autonomous Guidance and Flight Control System Implementation on a Partial-Authority Aircraft

    公开(公告)号:US20220380023A1

    公开(公告)日:2022-12-01

    申请号:US17719967

    申请日:2022-04-13

    Abstract: This disclosure provides a means to implement an autonomous guidance and flight control system on a partial authority aircraft. One embodiment of the disclosure includes receiving a control command result, filtering the control command result into a low frequency component and a high frequency component, directing the low frequency component to at least one trim servomechanism and directing the high frequency component to at least one stability augmentation stabilizer servomechanism, linking outputs from the trim servomechanism and the stability augmentation stabilizer servomechanism for actuating a pilot control configured to control rotors, and actuating at least one rotor. The low frequency component includes frequencies below a break frequency and the high frequency component includes frequencies above the break frequency. The break frequency is established by rate and position of the at least one servomechanism.

    Actively stabilized random number generator

    公开(公告)号:US12086570B2

    公开(公告)日:2024-09-10

    申请号:US17209680

    申请日:2021-03-23

    CPC classification number: G06F7/588

    Abstract: An actively stabilized random number generator includes a random number generator and a feedback controller. The random number generator includes a chaotic physical circuit realizing an iterated function. The iterated function is configured to produce a trajectory of iterates and has an operating parameter β and a desired Markov operating point. A binary bit converter has a symbol function configured to produce binary symbols from the trajectory of iterates and a maximal kneading sequence. The feedback controller is configured to observe the maximal kneading sequence within the trajectory of iterates and adjust the operating parameter to the desired Markov operating point.

    Load-bearing composite platform
    8.
    发明授权

    公开(公告)号:US11623428B2

    公开(公告)日:2023-04-11

    申请号:US17390421

    申请日:2021-07-30

    Abstract: The present disclosure provides a load-bearing composite platform. The platform includes a core layer, first and second reinforcement layers, and a frame. The core layer includes a structural sublayer, a force distribution sublayer, and an abrasion prevention sublayer. The first reinforcement layer is adhered to the force distribution sublayer, and the second reinforcement layer is adhered to the structural sublayer. The second reinforcement layer is an inverse of the first reinforcement layer. The frame surrounds the first reinforcement layer, the second reinforcement layer, and the core layer.

    ACTIVELY STABILIZED RANDOM NUMBER GENERATOR

    公开(公告)号:US20220308836A1

    公开(公告)日:2022-09-29

    申请号:US17209680

    申请日:2021-03-23

    Abstract: An actively stabilized random number generator includes a random number generator and a feedback controller. The random number generator includes a chaotic physical circuit realizing an iterated function. The iterated function is configured to produce a trajectory of iterates and has an operating parameter β and a desired Markov operating point. A binary bit converter has a symbol function configured to produce binary symbols from the trajectory of iterates and a maximal kneading sequence. The feedback controller is configured to observe the maximal kneading sequence within the trajectory of iterates and adjust the operating parameter to the desired Markov operating point.

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