Invention Grant
- Patent Title: Interstage seal assembly for gas turbine engine
- Patent Title (中): 燃气轮机发动机级间密封总成
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Application No.: US14254153Application Date: 2014-04-16
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Publication No.: US09540941B2Publication Date: 2017-01-10
- Inventor: Mahesh Janarthanan , Jeffrey A. Kain , Mushtaq Kazi
- Applicant: Siemens Energy, Inc.
- Applicant Address: US FL Orlando
- Assignee: Siemens Energy, Inc.
- Current Assignee: Siemens Energy, Inc.
- Current Assignee Address: US FL Orlando
- Main IPC: F01D11/02
- IPC: F01D11/02 ; F01D11/00 ; F02C7/28

Abstract:
A seal assembly is provided for a turbine engine and includes an annular labyrinth seal holder supported on a radially inner end of vanes A plurality of radially extending labyrinth seal elements are supported on the labyrinth seal holder, and a brush seal assembly is supported to the labyrinth seal holder downstream from the labyrinth seal elements. The brush seal assembly includes a brush seal holder and a brush seal located adjacent to an axially rearward one of the rotor arms. The brush seal holder is attached to an axially facing surface of the labyrinth seal holder. A seal plate defining a detachable labyrinth seal element extends radially inward from the axially facing surface of the labyrinth seal holder to the rearward rotor arm at a location upstream of the brush seal.
Public/Granted literature
- US20150300189A1 INTERSTAGE SEAL ASSEMBLY FOR GAS TURBINE ENGINE Public/Granted day:2015-10-22
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