发明名称 |
Coupling device for gas turbine engine |
摘要 |
A gas turbine engine of the type comprising a compressor and an expansion turbine of which the respective rotors are mutually joined together in rotation and in axial traction by a main coupling device. The engine includes, in addition, a safety coupling device joining together these two rotors only in axial traction but allowing them to turn one with respect to the other in case of accidental fracture of the main coupling device.
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申请公布号 |
US4037404(A) |
申请公布日期 |
1977.07.26 |
申请号 |
US19760701418 |
申请日期 |
1976.06.30 |
申请人 |
SOCIETE NATIONALE D'ETUDE ET DE CONSTRUCTION DE MOTEURS D'AVIATION |
发明人 |
BOUGAIN, GEORGES |
分类号 |
F01D5/02;(IPC1-7):F02K3/00 |
主分类号 |
F01D5/02 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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