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A combustion chamber heat shield and seal assembly and a method of manufacturing a combustion chamber heat shield and seal assembly

机译:燃烧室热屏蔽和密封组件以及制造燃烧室热屏蔽和密封组件的方法

摘要

A gas turbine engine combustion chamber heat shield and seal assembly comprises a heat shield and a seal. The heat shield has an aperture and the seal is located in the aperture in the heat shield. The seal comprises an annular member having an upstream end, a middle and a downstream end. The upstream end of the seal has a diameter greater than the diameter of the aperture in the heat shield, the middle has a diameter less than the diameter of the aperture in the heat shield and the downstream end of the seal has a diameter greater than the diameter of the aperture in the heat shield.
机译:燃气涡轮发动机燃烧室热屏蔽和密封组件包括热屏蔽和密封。隔热罩具有孔,并且密封件位于隔热罩的孔中。该密封件包括具有上游端,中间端和下游端的环形构件。密封件的上游端的直径大于隔热罩中的孔的直径,中间的直径小于隔热罩中的孔的直径,并且密封件的下游端的直径大于隔热罩的孔的直径。隔热罩上孔的直径。

著录项

  • 公开/公告号GB2511563B

    专利类型

  • 公开/公告日2015-06-24

    原文格式PDF

  • 申请/专利权人 ROLLS-ROYCE PLC;

    申请/专利号GB20130004184

  • 发明设计人 IAN MURRAY GARRY;

    申请日2013-03-08

  • 分类号F23R3;

  • 国家 GB

  • 入库时间 2022-08-21 14:53:35

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