Actuator mechanism for variable angle vane arrays

• US 5,620,301 A
• Filed: 04/05/1996
• Issued: 04/15/1997
• Est. Priority Date: 06/05/1995
• Status: Expired due to Fees

• Current Assignee: Rolls-Royce PLC (Rolls-Royce Holdings Plc)
• Original Assignee: Rolls-Royce PLC (Rolls-Royce Holdings Plc)
• Inventors: Lawer, Steven D.
• Primary Examiner(s): KWON, JOHN
• Application Number:
  US08/628,156
• Time in Patent Office: 375 Days
• Field of Search: 415/150, 415/159, 415/160, 415/162, 74/109
• US Class Current: 415/150
• CPC Class Codes: F01D 17/162 for axial flow, i.e. the vanes turning around axes which are essentially perpendicular to the rotor centre line F01D17/167 takes precedence
• CPC Class Codes: F05D 2260/74 by turning around an axis perpendicular the rotor centre line
• CPC Class Codes: F05D 2260/76 the adjusting mechanism using auxiliary power sources
• CPC Class Codes: Y10T 74/18976 Rack and pinion

Abstract

A power turbine includes a stage of pivotable nozzle vanes. The individual vanes are pivoted by connecting them to a toothed unison ring via actuating levers in the form of gear segments. The gear segments only have sufficient teeth to enable pivoting of the vanes between normal maximum and minimum operating angles. If an emergency closure of the nozzle is required, the unison ring pivots the gear therewith, whereupon pins on the unison ring engage projections on each segment, thus causing the segments to continue pivoting the vanes to a closed position.

Claims

1. An actuator mechanism for a variable angle vane array for use in a fluid flow machine of the type having an axis and a casing,

the variable angle vane array comprising a plurality of vanes, the vanes are pivotably mounted in the casing about radial axes, the vanes are pivotable between a first position giving maximum fluid flow delivery, and a second position giving minimum fluid flow delivery, each vane having a radially outer end,

the mechanism comprising a lever arm in the form of a gear segment secured to the radially outer end of each vane for effecting pivoting movement thereof, and

a toothed unison ring meshing with the gear segments for simultaneous transmission of pivoting movement to each vane through their respective gear segments,

wherein, the gear segments and the unison ring are provided with emergency drive means which engage to cause the gear segments to turn beyond toothed engagement with the unison ring so as to pivot their respective vanes to an effective zero fluid delivery position.

2. The mechanism of claim 1, wherein the emergency drive means comprises a first projection from each gear segment and corresponding second projections on the unison ring, said first and second projections being positioned so as to simultaneously engage, one first projection with each second projection, when the gear segments reach a limit of toothed engagement with the unison ring, thereby to cause further pivoting of the gear segments to the effective zero fluid delivery position.

3. The mechanism of claim 2, wherein the gear segments include abutment features positioned to engage each other just as the vanes reach the effective zero fluid delivery position, thereby to prevent fluid deflecting portions of the vanes contacting each other.

4. The mechanism of claim 1, wherein the gear segments include further abutments which are so positioned with respect to each other and the teeth of their respective gear segments as to ensure correct engagement of the gear segments with the unison ring when the vanes with their attached gear segments are assembled into the fluid flow machine at an extremity of operational movement of the vanes.

5. The mechanism of claim 1, wherein each gear segment has a first projection and each unison ring has second projections and the first projection from each gear segment extends radially from the gear segment and the second projections on the unison ring extend axially from the unison ring.

6. The mechanism of claim 5, wherein the first projection from each gear segment extends radially outwardly from the gear segment.

7. The mechanism of claim 1, wherein the variable angle vane array is in a turbine.

8. The mechanism of claim 1, wherein the variable angle vane array is in a power turbine.

9. The mechanism of claim 1, wherein the variable angle vane array is in a gas turbine engine.

10. A variable angle vane having first and second ends and an axis of rotation extending longitudinally of the vane,

the vane having a lever arm in the form of a gear segment secured to, and extending substantially perpendicular from the first end of the vane, the gear segment having first and second extremities,

the lever arm having a projection extending substantially longitudinally, relative to the vane, from the lever arm, the projection being located at the first extremity of the gear segment.

11. A variable angle vane as claimed in claim 10, wherein the projection extends away from the vane.