发明名称 BRAKE MECHANISM FOR AIR TURBINE STARTER
摘要 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).
申请公布号 US2011188997(A1) 申请公布日期 2011.08.04
申请号 US20100700337 申请日期 2010.02.04
申请人 HAMILTON SUNDSTRAND CORPORATION 发明人 NI WEISHUN W.;STADLER JEFFREY A.;PETERSON JODY A.
分类号 F01D15/12;F16D65/22 主分类号 F01D15/12
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