| 发明名称 |
FLAP ACTUATING DEVICE FOR THE NOZZLE OF A GAS TURBINE ENGINE |
| 摘要 |
The invention concerns a system for controlling the flaps of a turbine engine nozzle. High-pressure air P4 is bled from the compressor of the turbine engine to feed a compressed-air engine. The shaft of the engine rotates a constant-capacity displacement pump which sends hydraulic liquid into a jack controlling the flap or flaps of the nozzle. The invention is applicable to the control of all movable flaps of turbine engine nozzles. |
| 申请公布号 |
DE3173891(D1) |
申请公布日期 |
1986.04.03 |
| 申请号 |
DE19813173891 |
申请日期 |
1981.09.25 |
| 申请人 |
SOCIETE NATIONALE D'ETUDE ET DE CONSTRUCTION DE MOTEURS D'AVIATION, "S.N.E.C.M.A." |
发明人 |
FONDACCI, JEAN-LUC;FRANCOIS, YVES-MARIE M. R. |
| 分类号 |
F02K1/12;F02C7/32;F02K1/06;F02K1/15;F02K1/76;(IPC1-7):F02K1/76 |
主分类号 |
F02K1/12 |
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