Device for the individual adjustment of a plurality of variable-pitch radial stator vanes in a turbomachine

Patent metadata

Field	Value
Publication number	US-10598039-B2
Application number	US-201615550998-A
Country	US
Kind code	B2
Filing date	Feb 9, 2016
Priority date	Feb 19, 2015
Publication date	Mar 24, 2020
Grant date	Mar 24, 2020

Abstract

A device for adjusting the pitch of at least one annular row of stator vanes for a turbine engine module. The device includes a first control ring mounted to rotate freely about an axis of the turbine engine. The device also includes connecting rods for connecting the first control ring to the vanes and a second control ring mounted to rotate freely about the axis. Each vane of the at least one row is simultaneously connected to the first and second control rings by a set of at least two connecting rods. The device is suitable for use as part of a module and is suitable for use in a turbine engine.

First claim

The invention claimed is:

1. A device for adjusting the pitch of at least one annular row of stator vanes for a turbine engine module, the device comprising:
a first control ring mounted to rotate about an axis of the turbine engine;
a plurality of connecting rods configured for connecting said first control ring to the stator vanes of said at least one annual row of stator vanes; and
a second control ring mounted to rotate about said axis,
wherein each stator vane is simultaneously connected to said first and second control rings by a set of at least two connecting rods of said plurality of connecting rods configured to independently adjust the pitch of said stator vanes.

2. The device according to claim 1 , wherein said set of at least two connecting rods being articulated successively pairwise about radial articulation shafts, a first connecting rod of said set of at least two connecting rods is mounted to rotate about a first and a second radial pivot shaft, the first pivot shaft being mounted on said first control ring and the second pivot shaft being configured to be positioned independent of the position of the first control ring, and a second connecting rod of said set of at least two connecting rods is pivotally mounted on the first connecting rod about a first articulation shaft located at a first distance from said second pivot shaft that is determined for each vane.

3. The device according to claim 2 , wherein said first articulation shaft is located between the first and second pivot shafts.

4. The device according to claim 2 , comprising, for each stator vane of said at least one annular row of stator vanes, a pivot connection arranged to connect said stator vane to said at least two connecting rods about a third radial pivot shaft connected to the stator vane and offset relative to a pitch shaft of said stator vane, along said axis of the turbine engine.

5. The device according to claim 4 , wherein said at least two connecting rods includes a third connecting rod, and wherein the second pivot shaft is mounted on a stator casing and the third connecting rod is mounted to rotate about a fourth substantially radial pivot shaft mounted on said second control ring.

6. The device according to claim 5 , wherein the fourth pivot shaft is located on the third connecting rod between a second articulation shaft with the second connecting rod and a third articulation shaft with a fourth connecting rod, said fourth connecting rod being pivotally mounted about the third pivot shaft.

7. The device according to claim 5 , wherein, for each stator vane, the fourth pivot shaft is substantially in the same plane perpendicular to said axis of the turbine engine as a pitch shaft of the vane.

8. The device according to claim 5 , wherein the first and third connecting rods are substantially parallel to said axis of the turbine engine for at least one position of the control rings.

9. The device according to claim 4 , wherein, for at least one stator vane, the second pivot shaft is mounted on the second control ring and wherein the second connecting rod is pivotally mounted about the third pivot shaft.

10. A turbine engine module, comprising:
at least one annular row of stator vanes extending substantially radially about an axis of the turbine engine
at least one stator casing extending radially inside or outside the stator vanes; and
a device for adjusting the pitch of said at least one annular row of stator vanes according to claim 1 .

11. A turbine engine comprising:
at least one device according to claim 1 , wherein said at least one device according to claim 1 is placed upstream of a fan, downstream of a fan or inside a compressor.

12. The device according to claim 1 , wherein each stator vane is simultaneously connected to said first and second control rings by a separate set of said at least two connecting rods.

13. A turbine engine module, comprising:
at least one annular row of variable-pitch stator vanes extending substantially radially about an axis of a turbine engine;
at least one stator casing extending radially inside or outside the vanes; and
a device configured to adjust the pitch of said at least one annular row of vanes, said device comprising a first control ring mounted to rotate about an axis of the turbine engine, connecting rods configured for connecting said first control ring to said stator vanes, and a second control ring mounted to rotate about said axis, wherein each stator vane is simultaneously connected to said first and second control rings by at least two of said connecting rods configured to independently adjust the pitch of said vanes;
wherein the module is placed-upstream of a fan, downstream of a fan or inside a compressor.

14. A method for adjusting the pitch of at least one annular row of stator vanes using a device according to claim 5 during a turbine engine maintenance or set-up operation, comprising a preliminary step that comprises determining, for each vane, values of said first distance on the first connecting rod and a second distance that is defined by the gap between the third pivot shaft and an articulation shaft of the connecting rod of said set mounted on said third pivot shaft, said values allowing a given evolution rule to be obtained for the pitch angles as a function of the movement of the positions of the first and the second control ring, which method subsequently comprises a step a) that comprises adjusting the second distance for at least one vane and/or a step b) that comprises adjusting the first distance for at least one vane.

Assignees

• Safran Aircraft Engines

Inventors

• Bordoni Nils

Classifications

• F05D2250/42

  with two degrees of freedom · CPC title

• F05D2260/50

  Kinematic linkage, i.e. transmission of position · CPC title

• F05D2250/40

  Movement of components · CPC title

• F01D17/162 Primary

  for axial flow, i.e. the vanes turning around axes which are essentially perpendicular to the rotor centre line (F01D17/167 takes precedence) · CPC title

• F05D2240/12

  Fluid guiding means, e.g. vanes · CPC title