SYSTEM TO CONTROL TURBOJET ENGINE STATOR VANES WITH VARIABLE MOUNTING ANGLE Russian patent published in 2010 - IPC F01D17/16 

Abstract RU 2396438 C2

FIELD: engines and pumps.

SUBSTANCE: proposed system comprises drive element to revolve control ring of one of the stages by means of drive member arranged to turn on the casing, synchro lever to transmit aforesaid lever rotation to control ring of the other stage by means of servo element arranged to turn on aforesaid casing, and additional rotary member arranged between servo element and driven ring. Note here that said additional rotary member is arranged to turn simultaneously on the casing and said servo element.

EFFECT: possibility to vary vane mounting angle with acceleration (or deceleration) at certain local zone of control trajectory.

6 cl, 3 dwg

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RU 2 396 438 C2

Authors

Burju Mishel'

Dates

2010-08-10Published

2006-05-16Filed