EP 0795681 B1 20000426 - Actuation mechanism for variable inlet vanes in turbomachine compressor
Title (en)
Actuation mechanism for variable inlet vanes in turbomachine compressor
Title (de)
Antriebsvorrichtung für verstellbare Leitschaufeln eines Turbomaschinenkompressors
Title (fr)
Dispositif de commande d'aubes à calage variable pour compresseur de turbomachine
Publication
Application
Priority
FR 9603203 A 19960314
Abstract (en)
[origin: EP0795681A1] 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.
IPC 1-7
IPC 8 full level
F01D 17/16 (2006.01); F04D 29/56 (2006.01)
CPC (source: EP US)
F01D 17/162 (2013.01 - EP US); F04D 29/563 (2013.01 - EP US); F05D 2230/60 (2013.01 - EP US); F05D 2240/61 (2013.01 - EP US); F05D 2260/20 (2013.01 - EP US); F05D 2260/50 (2013.01 - EP US); F05D 2260/74 (2013.01 - EP US)
Designated contracting state (EPC)
DE FR GB
DOCDB simple family (publication)
EP 0795681 A1 19970917; EP 0795681 B1 20000426; CA 2197398 A1 19970915; CA 2197398 C 20040427; DE 69701759 D1 20000531; DE 69701759 T2 20001130; FR 2746141 A1 19970919; FR 2746141 B1 19980417; US 5795128 A 19980818
DOCDB simple family (application)
EP 97400549 A 19970313; CA 2197398 A 19970212; DE 69701759 T 19970313; FR 9603203 A 19960314; US 81434097 A 19970311