Variable stator vane actuating mechanism
AssigneeRolls-Royce (1971) Limited
InventorLeonard Stanley Snell
Life of this patent
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Abstract
A mechanism for varying the angle of attack of stator vanes of a compressor in a turbo machine. The vanes in each row are all connected to a respective encircling ring. The rings from all the rows of variable stators are connected to a beam which lies along the outside of the casing. The beam is connected at about its middle to a screw jack actuator which is bolted to the casing and one end of the beam is pivotted to the casing with a compound pivot which accommodates the compound movement of the beam caused by the straight line movement of the screw jack actuator.
Claims3
In a turbo-machine having a casing and a compressor with at least one row of stator vanes which are angularly adjustable, a mechanism comprising a beam connected at one end to the casing through a universal joint and a pivot offset therefrom, a beam driving member, means mounting said member for movement in a straight line tangent to an imaginary circle, which is coaxial with the compressor casing, an actuator for driving said beam driving member along said straight line, means pivotally connecting said beam to said beam driving member at a position remote from the end of the beam, which is connected to the casing through said universal joint and said pivot, said pivot being offset from said universal joint so as to enable the beam to move in the direction of its own longitudinal length relative to said casing by motion at the pivot and at the universal joint and to enable the beam simultaneously to move by motion at the universal joint when the beam driving member is driven along said straight line by the actuator, a ring, and means connecting the beam through universal joints to said ring, and means connecting said ring to the stator vanes whereby movement of the driving member causes variation of the angles of the stator vanes.
Dependencies are inferred from the claim text.