IP Library Granted Patent US 7,427,186
Granted Patent B2
US 7,427,186 · App. 11/260,207 · Granted Sep 23, 2008

Rotary engine with shaft bearing having two stiffnesses, rotary engine shaft and means of connection between a rotary engine shaft and a bearing

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Quick Facts
Patent No.
US 7,427,186
App. No.
11/260,207
Granted
Sep 23, 2008
Kind
B2
Abstract

A shaft mounted to rotate with respect to another fixed or rotary element of a rotary engine to which the shaft is connected by at least one bearing, it being possible for the engine to operate in at least two different operating speeds, the shaft comprising a connection to the bearing that has a state of stiffness that varies with engine operating speed. The connection comprises a squirrel cage comprising at least two points of attachment, one to the bearing and one to the shaft, between which points there extends a flexible portion, the shaft comprises an actuator able to adopt at least two positions for controlling the state of stiffness of the squirrel cage, the actuator comprises a piston designed to be displaced by oil pressure in a chamber formed between the piston and shaft from a rigid state of stiffness position to a soft state of stiffness position.

Claims (12)

1. Rotary engine comprising at least one shaft mounted to rotate with respect to another element of the engine, fixed or rotary, to which it is connected by at least one bearing, it being possible for the engine to operate in at least two different operating speeds, the shaft comprising means of connection to the bearing that have a state of stiffness that can vary with the engine operating speed, characterized in that the connecting means comprise a squirrel cage comprising at least two points of attachment, on the one hand to the bearing and, on the other hand, to the shaft, between which points there extends a portion that is flexible in bending, the shaft comprises an actuator able to adopt at least two positions for controlling the state of stiffness of the squirrel cage, the actuator comprises a piston designed to be displaced, against the action of return means, by a pressure of oil in a chamber formed between the piston and the shaft from a rigid state of stiffness position to a soft state of stiffness position, and vice versa.

2. Rotary engine according to claim 1 , in which the actuator can adopt a first position, out of contact with the squirrel cage, in which position the squirrel cage is in a soft state of stiffness, and a second position, in abutment between a wall of the shaft and a wall of the squirrel cage, in which position the squirrel cage is in a rigid state of stiffness.

3. Rotary engine according to claim 1 , in which the stiffness of the connecting means varies automatically with the engine speed.

4. Rotary engine according to claim 3 , in which the oil pressure is controlled by the engine speed, by centrifugal force.

5. Engine according to claim 4 , in which the oil pressure in the chamber varies with the centrifugal force exerted by the rotation of the shaft of the engine.

6. Rotary engine according to claim 1 , which is a twin spool turbine engine in which the shaft is the low-pressure turbine shaft and the other element of the engine is the high-pressure turbine shaft.

7. Rotary engine shaft comprising means of connection to a bearing having a state of stiffness that can vary with the operating speed of the engine, characterized in that the connecting means comprise a squirrel cage comprising at least two points of attachment, on the one hand to the bearing and, on the other hand, to the shaft, between which points there extends a portion that is flexible in bending, the shaft comprises an actuator able to adopt at least two positions for controlling the state of stiffness of the squirrel cage, the actuator comprises a piston designed to be displaced, against the action of return means, by a pressure of oil in a chamber formed between the piston and the shaft from a rigid state of stiffness position to a soft state of stiffness position, and vice versa.

8. Shaft according to claim 7 , in which the actuator can adopt a first position, out of contact with the squirrel cage, in which position the squirrel cage is in a soft state of stiffness, and a second position, in abutment between a wall of the shaft and a wall of the squirrel cage, in which position the squirrel cage is in a rigid state of stiffness.

9. Shaft according to claim 8 , which is a low-pressure turbine shaft of a twin spool turbine engine.

10. Connecting means between a shaft of a rotary engine and a bearing connected to the shaft, which have a state of stiffness that can vary with the operating speed of the engine, and which are characterized in that they comprise a squirrel cage comprising at least two points of attachment, intended to be attached on the one hand to the bearing and, on the other hand, to the shaft, between which points there extends a portion that is flexible in bending and an actuator able to adopt at least two positions for controlling the state of stiffness of the squirrel cage, the actuator comprising a piston designed to be displaced, against the action of return means, by a pressure of oil in a chamber formed between the piston and the shaft from a rigid state of stiffness position to a soft state of stiffness position, and vice versa.

11. Connecting means according to claim 10 , in which the actuator can adopt a first position, out of contact with the squirrel cage, in which position the squirrel cage is in a soft state of stiffness, and a second position, in abutment between a wall of the shaft and a wall of the squirrel cage, in which position the squirrel cage is in a rigid state of stiffness.

12. Connecting means according to claim 10 , forming means of connection between the low-pressure turbine shaft and the inter-shaft bearing between the low-pressure turbine shaft and the high-pressure turbine shaft of a twin spool turbine engine.

Assignments (3)
CORRECTIVE ASSIGNMENT TO CORRECT THE COVER SHEET TO REMOVE APPLICATION NOS. 10250419, 10786507, 10786409, 12416418, 12531115, 12996294, 12094637 12416422 PREVIOUSLY RECORDED ON REEL 046479 FRAME 0807. ASSIGNOR(S) HEREBY CONFIRMS THE CHANGE OF NAME. Recorded Aug 24, 2018
From: SNECMA
To: SAFRAN AIRCRAFT ENGINES
Reel/Frame 046939/0336 →
CHANGE OF NAME Recorded May 23, 2018
From: SNECMA
To: SAFRAN AIRCRAFT ENGINES
Reel/Frame 046479/0807 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jan 18, 2006
From: GEREZ, VALERIO; JADCZAK, EDOUARD, JOSEPH; POINSOT-BERTHELOT, FLORIAN
To: SNECMA
Reel/Frame 017474/0604 →