发明名称 |
GAS TURBINE ENGINE COMBUSTION CHAMBER COMPRISING CMC DEFLECTORS |
摘要 |
A gas turbine engine combustion chamber including at least one deflector mounted on the chamber end wall and including an opening for a carburetted air supply device. The deflector includes an opening, corresponding to the chamber end wall opening, with an annular cylindrical part for attachment to the wall, the cylindrical part including a mechanical attachment mechanism collaborating with a complementary attachment mechanism on a metal sleeve secured to the wall and a cylindrical centering cup fixed by one end to the sleeve and housed inside the cylindrical part of the deflector. |
申请公布号 |
EP2307805(B1) |
申请公布日期 |
2017.03.15 |
申请号 |
EP20090772283 |
申请日期 |
2009.06.10 |
申请人 |
Safran Aircraft Engines |
发明人 |
DUVAL, Sylvain;HERNANDEZ, Didier, Hyppolyte;LUNEL, Romain, Nicolas |
分类号 |
F23R3/28;F23R3/50 |
主分类号 |
F23R3/28 |
代理机构 |
|
代理人 |
|
主权项 |
|
地址 |
|