Turbine engine having a stage of variable-pitch stator vanes with independent control

Patent metadata

Field	Value
Publication number	US-9429169-B2
Application number	US-201013511068-A
Country	US
Kind code	B2
Filing date	Nov 19, 2010
Priority date	Nov 20, 2009
Publication date	Aug 30, 2016
Grant date	Aug 30, 2016

Abstract

A turbine engine including a stator including variable-pitch vanes that are controlled stage by stage. An actuator ring connected by crank-arms to the variable-pitch vanes is coupled to at least one adjacent specific drive unit in a general form of an actuator.

First claim

The invention claimed is:

1. A turbine engine comprising:
a casing housing at least one stator stage including variable-pitch vanes controlled by an actuator ring coaxially surrounding the casing, wherein the ring is constrained to move in turning only about an axis of the casing and being connected by crank-arms to the variable-pitch vanes,
wherein the actuator ring is coupled to at least one adjacent specific drive unit generally in a form of an actuator and comprising first and second portions forming a cylinder and a rod extending from the cylinder, wherein the first portion is hinged to the casing, and the second portion is directly hinged to a lateral extension of the ring, the lateral extension of the ring being rotationally stationary relative to the ring,
wherein the rod is directly hinged to the ring and the cylinder is hinged to the casing, and
wherein the hinge between the cylinder and the casing is arranged in a vicinity of an end of the cylinder from which the rod extends.

2. A turbine engine according to claim 1 , wherein the rod of the actuator-forming drive unit extends along an axis lying in a plane parallel to a midplane of the actuator ring.

3. A turbine engine according to claim 1 , wherein the hinge is situated substantially in a middle of the actuator when the rod is deployed to its maximum stroke.

4. A turbine engine according to claim 1 , wherein the lateral extension includes a fork, and an end of the rod is directly hinged to the fork about an axis parallel to the axis of the casing.

5. A turbine engine according to claim 4 , wherein the fork of the lateral extension includes first and second plates, and the end of the rod includes a flat portion inserted between the first and second plates of the fork.

6. A turbine engine according to claim 1 , wherein the cylinder includes a lateral tab hinged to a fork secured to the casing.

7. A turbine engine according to claim 1 , wherein the actuator is of linear motion electric motor type.

8. A turbine engine according to claim 1 , wherein each actuator ring is coupled to two adjacent specific drive units that are substantially diametrically opposite.

9. A turbine engine according to claim 1 , wherein a first end of the rod is inside the cylinder and a second end of the rod is directly hinged to the casing.

10. A turbine engine according to claim 1 , wherein the lateral extension of the ring is fixedly attached to the ring.

11. A turbine engine comprising:
a casing housing several stator stages including variable-pitch vanes, each stator stage being controlled independently by an actuator ring coaxially surrounding the casing, wherein said ring is constrained to move in turning only about an axis of the casing and being connected by crank-arms to the variable-pitch vanes of said stator stage,
wherein each actuator ring is coupled to at least one adjacent specific drive unit generally in a form of an actuator and comprising first and second portions forming a cylinder and a rod extending from the cylinder, wherein the first portion is hinged to the casing, and the second portion is directly hinged to a lateral extension of the ring, the lateral extension of the ring being rotationally stationary relative to the ring.

Assignees

• Bouru Michel Andre
• Kettler Daniel Germain Alexis
• Snecma

Inventors

• Bouru Michel Andre
• Kettler Daniel Germain Alexis

Classifications

• Y02T50/671

  Cross-Sectional Technologies · mapped topic

• F05D2260/50

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

• F01D17/162

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

• F04D29/563 Primary

  specially adapted for elastic fluid pumps · CPC title

• F05D2270/62

  Electrical actuators · CPC title