TURBOMASCHINE MIT EINER BREMSEINRICHTUNG ZWISCHEN TURBINENROTOR UND AUSLASSGEHAEUSE.
摘要
In the event of a break of the common shaft of the turbine and compressor rotors of a turbo machine, the turbine is braked by means of a device consisting of a conical ring (9) carried by the turbine rotor and capable of being blocked in contact with a structural element (17) of general conical shape carried by the exhaust housing (5). …<IMAGE>…
申请公布号
DE68906662(D1)
申请公布日期
1993.06.24
申请号
DE1989606662
申请日期
1989.12.06
申请人
SOCIETE NATIONALE D'ETUDE ET DE CONSTRUCTION DE MOTEURS D'AVIATION, (S.N.E.C.M.A.), EVRY, FR
