Force-controlled throttle for adjusting the engine thrust of a combat aircraft
    21.
    发明授权
    Force-controlled throttle for adjusting the engine thrust of a combat aircraft 有权
    用于调整作战飞机发动机推力的控制节气门

    公开(公告)号:US07313468B2

    公开(公告)日:2007-12-25

    申请号:US10920452

    申请日:2004-08-18

    IPC分类号: B64D31/04

    CPC分类号: B64D31/04

    摘要: A force-controlled throttle for adjusting the engine thrust of a combat aircraft with a handle for operation by a pilot and with a signal generating device that is connected to the handle for generating a control signal used for adjusting the engine thrust. The signal generating device is provided for generating the control signal as a function of the force exerted by the pilot on the handle in operation. The throttle may include force-controlled elements for control of an afterburner.

    摘要翻译: 一种用于通过驾驶员操作的手柄调节作战飞机的发动机推力的力控制节气门,以及连接到手柄的信号发生装置,用于产生用于调节发动机推力的控制信号。 信号发生装置被提供用于根据由操作员在手柄上施加的力的函数产生控制信号。 节气门可以包括用于控制加力燃烧器的力控制元件。

    Bi-directional, dual acting, electric safety lock
    22.
    发明授权
    Bi-directional, dual acting, electric safety lock 失效
    双向,双作用,电动安全锁

    公开(公告)号:US5984241A

    公开(公告)日:1999-11-16

    申请号:US924963

    申请日:1997-09-08

    申请人: Gary A. Sparks

    发明人: Gary A. Sparks

    IPC分类号: B64C13/04 B64C13/14

    CPC分类号: B64D31/04

    摘要: An electrical lock for a moving part prevents the part from moving unless a device controlled by the part is in a safe mode. The invention may find a use in many different environments. The specific example here described is a set of reverse thruster doors on a jet engine. The lock prevents a throttle from applying or removing power unless the reverse thruster doors are properly set for such application or removal of power. The lock is removed when the doors reach full deployment or retraction, respectively, which is appropriate for the direction in which said throttle is moved. These functions are provided under the control of a single solenoid.

    摘要翻译: 用于移动部件的电锁防止部件移动,除非由部件控制的装置处于安全模式。 本发明可以在许多不同的环境中使用。 这里描述的具体示例是喷气发动机上的一组反向推进器门。 除非反向推进器门适当地设置用于这种应用或移除电源,否则锁可防止油门施加或移除动力。 当门分别达到完全展开或缩回时,锁被去除,这适合于所述节气门移动的方向。 这些功能在单个电磁阀的控制下提供。

    Control apparatus
    23.
    发明授权
    Control apparatus 失效
    控制装置

    公开(公告)号:US5143330A

    公开(公告)日:1992-09-01

    申请号:US672312

    申请日:1991-03-20

    申请人: Arthur Kaye

    发明人: Arthur Kaye

    IPC分类号: B64D31/04 G05G9/04

    CPC分类号: B64D31/04 G05G9/04

    摘要: Control apparatus comprises a throttle stick suitable for STOVL aircraft which incorporates vectorable nozzle control means with thrust demand, thus obviating the need for a separate control lever for controlling vectorable nozzles. A handle (10) rotates to pre-determined angular positions in response to operator-exerted pressure, said pressure being sensed by force transducers (7a, 7b) hence providing the operator with tactile feedback proportional to thrust demand. A control lever (2) attached to the handle (10) is pivotable about a hinge pin (8). Rotation of the lever (2) about the pin (8) is sensed by a potentiometer (9) whose output is used to control vectorable nozzles.