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.
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
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