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Auxiliary starter for transferring to the main shaft - directly connected with the HPC shaft of the aeroderivate jet engine

机译:辅助起动器,用于转移到主轴上-直接与航改喷气发动机的HPC轴连接

摘要

in one aspect, the disclosure relates to system starting the gas turbine, which includes a shaft (34) connecting the compressor and the turbine. the ring casing extends peripherally around the shaft so that the ring casing defines the compartment. orifice extends radially outwards from the ring enclosure for mounting ring to the fixed housing wall.the pacemaker is placed in this compartment. a rotary ring connects to the housing and selectively connected with the starter. the collar has a radially inner surface containing the cervical vertebra to do with shaft. the pacemaker after activation is collar, which rotates the shaft for starting the gas turbine.
机译:一方面,本发明涉及启动燃气轮机的系统,该系统包括连接压缩机和涡轮机的轴(34)。环形壳体围绕轴沿周向延伸,从而环形壳体限定了隔室。孔从环罩径向向外延伸,用于将环安装到固定的壳体壁上。起搏器放置在该隔室中。旋转环连接到壳体并选择性地与起动器连接。颈圈具有径向内表面,该径向内表面包含与轴相连的颈椎。激活后的起搏器为轴环,该轴环旋转轴以启动燃气轮机。

著录项

  • 公开/公告号PL231367B1

    专利类型

  • 公开/公告日2019-02-28

    原文格式PDF

  • 申请/专利权人 GENERAL ELECTRIC COMPANY;

    申请/专利号PL20150414612

  • 发明设计人 SZCZEPANOWSKI PAWEŁ;GOLDYN MATEUSZ;

    申请日2015-10-30

  • 分类号F02C7/268;

  • 国家 PL

  • 入库时间 2022-08-21 12:01:21

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