发明名称 Actuation mechanism for variable inlet vanes in turbomachine compressor
摘要 The blade pivoting control, which is integral in the manifold (5), has a pivot (3) mounted in a bore in a platform (4) fixed to the air manifold by upstream (7) and downstream (8) flanges. The pivot is fixed by a hollow friction casing (11) in the platform bore. The casing has a circumferential slot in which the upstream part (12) of a rod is inserted. Directional control of a movable blade (2) is mounted outside the manifold. Corresponding apertures are located in the manifold and in the platform so as to enable movement of the variable wedging control by the rod. The rod upstream part has an eye into which is inserted the hollow pivot. The rod downstream part (13) is located outside the manifold and is connected to the blade directional control.
申请公布号 EP0795681(A1) 申请公布日期 1997.09.17
申请号 EP19970400549 申请日期 1997.03.13
申请人 SOCIETE NATIONALE D'ETUDE ET DE CONSTRUCTION DE MOTEURS D'AVIATION, "S.N.E.C.M.A." 发明人 EICHSTADT, FREDERIC PAUL
分类号 F01D17/16;F04D29/56;(IPC1-7):F01D17/16 主分类号 F01D17/16
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