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    • 1. 发明申请
    • BRAKE MECHANISM FOR AIR TURBINE STARTER
    • 用于空气涡轮起动器的制动机构
    • US20110188997A1
    • 2011-08-04
    • US12700337
    • 2010-02-04
    • Weishun W. NiJeffrey A. StadlerJody A. Peterson
    • Weishun W. NiJeffrey A. StadlerJody A. Peterson
    • F01D15/12F16D65/24
    • F02C7/277F05D2260/902F16D2121/12
    • A brake assembly (44) for an air turbine starter (10) includes a brake cylinder (46) located in the air turbine starter (10). A brake piston (48) is located at least partially within the brake cylinder (46) and slidable therein. A biasing member (50) biases the brake piston (48) toward a turbine wheel (12) of the air turbine starter (10) applying a braking force to the turbine wheel (12) and defining a piston chamber (58) between the turbine wheel (12) and the brake piston (48). A through opening (56) in the brake piston (48) into the piston chamber (58) is configured such that a flow of fluid through the through opening (56) into the piston chamber (58) applies a force to the brake piston (48) sufficient to overcome the bias thereby allowing rotation of the turbine wheel (12).
    • 用于空气涡轮起动器(10)的制动组件(44)包括位于空气涡轮起动器(10)中的制动缸(46)。 制动活塞(48)至少部分地位于制动缸(46)内并在其中可滑动。 偏压构件(50)将制动活塞(48)朝向空气涡轮起动器(10)的涡轮机叶片(12)偏压,向涡轮机叶轮(12)施加制动力并且在涡轮机之间限定活塞室(58) 车轮(12)和制动活塞(48)。 制动活塞(48)中的进入活塞室(58)的通孔(56)构造成使得通过通孔(56)进入活塞室(58)的流体流向制动活塞( 足以克服偏压从而允许涡轮机叶轮(12)的旋转。