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    • 4. 发明申请
    • ASPIRATING SEAL ASSEMBLY AND METHOD OF ASSEMBLING
    • 吸附密封组件和组装方法
    • US20170022837A1
    • 2017-01-26
    • US14807376
    • 2015-07-23
    • General Electric Company
    • Quang Tue Nguyen TranRodrigo Rodriguez ErdmengerChristopher Jon Potokar
    • F01D11/00F01D9/02F01D11/02F01D5/02
    • F01D5/046F01D5/048F01D11/025Y02E20/14Y02T50/673
    • An aspirating seal assembly for use in a turbine engine is provided. The aspirating seal assembly includes a face seal and a rotary component. The face seal includes a first annular seal surface, and the rotary component includes a second annular seal surface positioned adjacent the first annular seal surface and defining a seal interface therebetween. The face seal is configured to discharge a flow of air towards the seal interface. The seal assembly also includes a first seal member extending between the first and second annular seal surfaces such that the flow of air induces a back pressure across the seal interface, and a second seal member positioned radially inward from the first seal member and extending between the first and second annular seal surfaces. A length of the second seal member is selected to increase the back pressure induced across the seal interface.
    • 提供了一种用于涡轮发动机的吸气密封组件。 抽吸密封组件包括面密封件和旋转部件。 所述面密封件包括第一环形密封表面,并且所述旋转部件包括邻近所述第一环形密封表面定位并且在其之间限定密封接合的第二环形密封表面。 面密封件构造成朝向密封界面排出空气流。 密封组件还包括在第一和第二环形密封表面之间延伸的第一密封构件,使得空气流引导穿过密封界面的背压,以及从第一密封构件径向向内定位并在第一密封构件之间延伸的第二密封构件 第一和第二环形密封表面。 选择第二密封构件的长度以增加在密封界面上引起的背压。