- 专利标题: Combustion chamber for a turbomachine
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申请号: US17431254申请日: 2020-02-19
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公开(公告)号: US11808456B2公开(公告)日: 2023-11-07
- 发明人: Jacques Marcel Arthur Bunel , William Louis Rodolphe Dousse , Benjamin Frantz Karl Villenave
- 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: CHRISTENSEN O'CONNOR JOHNSON KINDNESS PLLC
- 优先权: FR 01635 2019.02.19
- 国际申请: PCT/FR2020/000037 2020.02.19
- 国际公布: WO2020/169894A 2020.08.27
- 进入国家日期: 2021-08-16
- 主分类号: F23R3/28
- IPC分类号: F23R3/28 ; F02C3/00 ; F23R3/50 ; F23R3/60
摘要:
A combustion chamber includes a bottom wall having at least one opening, at least one sleeve mounted upstream of the bottom wall and fixed to the bottom wall, a closing ring defining an annular groove with the sleeve and fixed to the sleeve, and at least one air and fuel injection system having an axis, mounted in the opening of the bottom wall. The injection system has an annular flange extending radially with respect to the axis and is mounted in the groove with radial clearance. A baffle is situated downstream of the bottom wall and is fixed to the sleeve and/or to the bottom wall.
公开/授权文献
- US20220018543A1 COMBUSTION CHAMBER FOR A TURBOMACHINE 公开/授权日:2022-01-20
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