发明名称 |
Annular combustion chamber of a turbomachine |
摘要 |
An annular combustion chamber for a turbomachine presenting an axial direction, a radial direction, and an azimuth direction, the combustion chamber including a first annular wall and a second annular wall, each annular wall defining at least a portion of an enclosure of the combustion chamber. The first annular wall and the second annular wall present complementary assembly mechanisms that co-operate by engagement in azimuth. |
申请公布号 |
US8925331(B2) |
申请公布日期 |
2015.01.06 |
申请号 |
US201214124511 |
申请日期 |
2012.06.04 |
申请人 |
Turbomeca |
发明人 |
Carrere Bernard;Savary Nicolas |
分类号 |
F23R3/60;F23R3/00 |
主分类号 |
F23R3/60 |
代理机构 |
Oblon, Spivak, McClelland, Maier & Neustadt, L.L.P. |
代理人 |
Oblon, Spivak, McClelland, Maier & Neustadt, L.L.P. |
主权项 |
1. An annular combustion chamber for a turbomachine presenting an axial direction, a radial direction, and an azimuth direction, the combustion chamber comprising:
a first annular wall and a second annular wall, each annular wall defining at least a portion of an enclosure of the combustion chamber, wherein the first annular wall and the second annular wall present complementary assembly means that co-operate by engagement in azimuth, and wherein the complementary assembly means comprises a plurality of first tongues extending from the first annular wall in azimuth in a first direction, and a plurality of second tongues extending from the second annular wall in azimuth in a second direction, opposite to the first direction, the first and second tongues co-operating by engagement in azimuth. |
地址 |
Bordes FR |