- 专利标题: PLATFORM COVER PLATES FOR GAS TURBINE ENGINE COMPONENTS
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申请号: US15961930申请日: 2018-04-25
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公开(公告)号: US20190330986A1公开(公告)日: 2019-10-31
- 发明人: Corey D. Anderson , Brandon W. Spangler
- 申请人: United Technologies Corporation
- 主分类号: F01D5/18
- IPC分类号: F01D5/18
摘要:
Components for gas turbine engines are provided. The components include a platform, a first airfoil extending from the platform, a first cavity located within the first airfoil, the first cavity includes a forward portion and an aft portion separated by a divider, a cover plate attached to the platform on a side opposite the airfoil, wherein a platform cavity is defined between the cover plate and the platform and wherein the first cavity is fluidly connected to the platform cavity through a first cavity inlet, and a first cavity separating rail dividing the platform cavity into a first platform forward cavity and a first platform aft cavity, wherein the first platform forward cavity is fluidly connected to the aft portion of the first cavity and the first platform aft cavity is fluidly connected to the forward portion of the first cavity.
公开/授权文献
- US10697309B2 Platform cover plates for gas turbine engine components 公开/授权日:2020-06-30