Invention Grant
- Patent Title: Turbine shroud assembly
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Application No.: US16960726Application Date: 2018-12-24
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Publication No.: US11078804B2Publication Date: 2021-08-03
- Inventor: Nicolas Paul Tableau , Sébastien Serge Francis Congratel , Antoine Claude Michel Etienne Danis , Clément Jean Pierre Duffau , Clément Jarrossay
- Applicant: SAFRAN AIRCRAFT ENGINES
- Applicant Address: FR Paris
- Assignee: SAFRAN AIRCRAFT ENGINES
- Current Assignee: SAFRAN AIRCRAFT ENGINES
- Current Assignee Address: FR Paris
- Agency: Pillsbury Winthrop Shaw Pittman LLP
- Priority: FR1850151 20180109
- International Application: PCT/FR2018/053546 WO 20181224
- International Announcement: WO2019/138168 WO 20190718
- Main IPC: F01D11/08
- IPC: F01D11/08

Abstract:
A turbine ring assembly includes ring sectors forming a turbine ring and a ring support structure, each sector having, along a cutting plane defined by an axial direction and a radial direction of the ring, a portion forming an annular base with, in the radial direction, an inner face and an outer face from which a first and a second lug protrude, the structure including a shroud from which protrude a first and a second radial clamp from which the first and second lugs are held. The turbine ring includes an annular flange having a first portion bearing against the first lug, and a second portion removably fixed to the first radial clamp, the first portion including radial slits open on a free end of the annular flange and delimiting first-portion sectors.
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