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    SYSTEMS AND METHODS FOR PROPULSOR SYNCHRONIZATION
    2.
    发明公开
    SYSTEMS AND METHODS FOR PROPULSOR SYNCHRONIZATION 审中-公开

    公开(公告)号：US20230382546A1

    公开(公告)日：2023-11-30

    申请号：US17752020

    申请日：2022-05-24

    申请人： BETA AIR, LLC

    发明人： Collin Freiheit ,  Nicholas Moy

    IPC分类号： B64D31/12 ,  B64D27/24 ,  B64C29/00 ,  B64C11/50

    CPC分类号： B64D31/12 ,  B64D27/24 ,  B64C29/0025 ,  B64C11/50

    摘要： A system for propulsor synchronization using electronic brakes is disclosed. The system includes a controller located in an electric aircraft configured to receive a first signal from a first propulsor sensor of a plurality of propulsor sensors, the first propulsor sensor configured to measure a first motion parameter of a first propulsor of a plurality of propulsors. The controller may receive a second signal from a second propulsor sensor of the plurality of propulsor sensors, the second propulsor sensor configured to measure a second motion parameter of a second propulsor of the plurality of propulsors. The controller may synchronously decelerate the first propulsor and the second propulsor based on the first motion parameter and the second motion parameter.

    Aircraft including an engine controlled by synchrophasing
    4.
    发明授权
    Aircraft including an engine controlled by synchrophasing 有权
    飞机包括由同步控制的发动机

    公开(公告)号：US08740133B2

    公开(公告)日：2014-06-03

    申请号：US13055340

    申请日：2009-07-21

    申请人： Jean-Michel Saucray ,  Philippe Chareyre

    发明人： Jean-Michel Saucray ,  Philippe Chareyre

    IPC分类号： B64C1/40

    CPC分类号： B64D31/12 ,  B64C11/008 ,  B64C11/48 ,  B64C11/50 ,  B64D27/08 ,  B64D2027/026 ,  Y02T50/66

    摘要： An aircraft including at least one engine having counter-rotating rotors, the engine or at least one of the engines having imbalances associated with at least one ellipse. The aircraft includes at least one vibration damper attached in an arrangement such that, at a given engine speed and for at least one given common direction of a large axis of the ellipse or at least one of the ellipses, a speed related to the two ends of the damper is higher than for any other arrangement of the damper.

    摘要翻译： 一种包括至少一个具有反转转子的发动机的发动机，所述发动机或至少一个所述发动机具有与至少一个椭圆相关联的不平衡。 飞行器包括至少一个振动阻尼器，该振动阻尼器以一种布置方式附接，使得在给定的发动机转速下，对于椭圆的大轴或至少一个椭圆的至少一个给定的共同方向，与两端相关的速度 的阻尼器比阻尼器的任何其它布置高。

    Propeller control system
    5.
    发明授权
    Propeller control system 失效
    螺旋桨控制系统

    公开(公告)号：US5335175A

    公开(公告)日：1994-08-02

    申请号：US847007

    申请日：1992-05-27

    申请人： Gilbert A. Turner

    发明人： Gilbert A. Turner

    IPC分类号： B64C11/50

    CPC分类号： B64C11/50

    摘要： A propeller control system comprises a phase controller (11) having a phase control gain to control a propeller phase relationship, free air turbulence detection means (7, 9) and a gain controller (8) for varying the phase control gain in response to detected free air turbulence such that in the presence of turbulence a low gain is selected and in the absence of turbulence a high gain is selected. By varying the gain in this way the sensitivity of the phase controller (11) is reduced during turbulent conditions preventing excessive phase changes by the controller (11) striving to follow a turbulent master propeller. Similarly a speed controller (14) has its gain set by a gain controller (17) according to the degree of turbulence detected.

    摘要翻译： PCT No.PCT / GB91 / 01361 Sec。 371日期：1992年5月27日 102（e）日期1992年5月27日PCT 1991年8月9日PCT PCT。 出版物WO92 / 02411 日期1992年2月20日。一种螺旋桨控制系统，包括具有相位控制增益以控制螺旋桨相位关系的相位控制器（11），自由空气湍流检测装置（7,9）和增益控制器（8） 响应于检测到的自由空气湍流的相位控制增益，使得在存在湍流的情况下选择低增益，并且在没有湍流的情况下选择高增益。 通过以这种方式改变增益，相位控制器（11）的灵敏度在湍流条件下被减小，从而防止控制器（11）过度相位变化，从而追求湍流主螺旋桨。 类似地，根据检测到的湍流程度，速度控制器（14）具有由增益控制器（17）设定的增益。