Variable regulator for pneumatic airplane starters
    1.
    发明公开
    Variable regulator for pneumatic airplane starters 失效
    变量调节器fneumzechen Flugzeuganlasser。

    公开(公告)号:EP0473530A1

    公开(公告)日:1992-03-04

    申请号:EP91500101.0

    申请日:1991-08-23

    IPC分类号: F02N7/14 B64F1/34

    CPC分类号: F02N7/14

    摘要: The regulator makes it possible to start different types of airplanes with a single starter, providing it the pressure and air flow required.
    Upon the operator selecting the start step corresponding to the plane to start, the convenient rating of the turbine is set by operating a simple control that controls the flow of fuel to the combustion chamber, using the indications of a sensor that indicates to it the rotation speed achieved by the turbine. When the operation so requires, in order to obtain the pressure and air flow that the airplane needs to start, the system also activates different mechanisms.
    As an alternative, by means of a microprocessor the start step corresponding to the plane to start can be chosen automatically, using the indications of pressure and flow at the inlet of the airplane.

    摘要翻译: 调节器可以使用单个启动器启动不同类型的飞机,为其提供所需的压力和空气流量。 在操作者选择与该平面相对应的开始步骤开始时,通过使用控制向燃烧室的燃料流动的简单控制来设定涡轮机的便利等级,该指示使用向其指示旋转的传感器 涡轮机达到的速度。 当操作需要时,为了获得飞机需要启动的压力和空气流量,系统还激活不同的机制。 作为替代,通过微处理器,可以使用飞机入口处的压力和流量的指示来自动选择与启动平面相对应的起始步骤。