- 专利标题: Turbine ring assembly
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申请号: US15680924申请日: 2017-08-18
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公开(公告)号: US10598045B2公开(公告)日: 2020-03-24
- 发明人: Nicolas Paul Tableau , Sébastien Serge Francis Congratel , Clément Jean Pierre Duffau , Lucien Henri Jacques Quennehen
- 申请人: Safran Aircraft Engines
- 申请人地址: FR Paris
- 专利权人: Safran Aircraft Engines
- 当前专利权人: Safran Aircraft Engines
- 当前专利权人地址: FR Paris
- 代理机构: Bookoff McAndrews, PLLC
- 优先权: FR1657827 20160819
- 主分类号: F01D25/28
- IPC分类号: F01D25/28 ; F01D25/24 ; F01D11/00 ; F01D11/08
摘要:
A turbine ring assembly includes ring sectors forming a turbine ring and a ring support structure, each ring sector having, in a section plane defined by an axial direction and a radial direction of the turbine ring, a portion forming an annular base with, in the radial direction, an inside face defining the inside face of the turbine ring and an outside face from which a first and a second attachment tab protrude, the ring support structure having a central annulus from which a first and a second radial tab protrude, between which the first and second attachment tabs of each ring sector are held. The first radial tab comprises a one-piece annular flange that is fastened in a removable manner to the central annulus of the ring support structure.
公开/授权文献
- US20180051590A1 TURBINE RING ASSEMBLY 公开/授权日:2018-02-22
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