发明名称 |
Safety device for restarting windmilling turbojet |
摘要 |
<p>A turbojet (1) has a fan (2) and compressor driven respectively by low pressure turbine and high pressure turbine through the coaxial shafts (3,4). The shafts are interconnected, to compensate rotation speed in normal operation of turbojet. A braking system (6) slowdown or blocks a differential (5) having an annular gear (7) rotating about the shafts, when turbojet shuts down.</p> |
申请公布号 |
EP1270903(A1) |
申请公布日期 |
2003.01.02 |
申请号 |
EP20020291410 |
申请日期 |
2002.06.07 |
申请人 |
SNECMA MOTEURS |
发明人 |
FRANCHET, MICHEL;HEBRAUD, GUY |
分类号 |
F02C3/113;F02C7/262;F02C7/264;F02C7/275;F02K3/06;(IPC1-7):F02C7/262 |
主分类号 |
F02C3/113 |
代理机构 |
|
代理人 |
|
主权项 |
|
地址 |
|