IP Library Granted Patent US 9,540,093
Granted Patent B2
US 9,540,093 · App. 14/236,254 · Granted Jan 10, 2017

Bladed rotor wheel for a turbine engine

View Patent ↗
Loading inventors, assignments & file history…
Monitor This Case
Get email alerts when status or documents change.
Order Certified Copies
Most orders are placed with the USPTO same day — all within 24 business hours.
Order via The Patent Place →
Pre-filled with this patent's details
Quick Facts
Patent No.
US 9,540,093
App. No.
14/236,254
Granted
Jan 10, 2017
Kind
B2
Abstract

A bladed rotor wheel for a turbine engine, the rotor wheel including a disk including, formed in its outer periphery, at least one slot for mounting the roots of blades, and a spacer mounted between each blade root and a bottom of the slot. The spacer includes at least one member of type that is bistable in position and that can occupy a first stable position for assembly or disassembly in which the member does not exert force on the blade root, and a second stable position in which the bistable member exerts a radial force on the blade root. The spacer also includes at least one resilient damper member mounted between the bottom of the slot and the blade root.

Claims (20)

1. A bladed rotor wheel for a turbine engine, the rotor wheel comprising:

a disk including, formed in an outer periphery thereof, a slot for assembling a root of a blade; and

a spacer mounted between the blade root and a bottom of the slot, the spacer including

a member of type that is bistable in position and that can occupy a first stable position for assembly or disassembly in which the bistable member does not exert force on the blade root, and a second stable position which the bistable member exerts a radial force on the blade root for holding the blade stationary and stabilizing the blade in a final position,

a resilient damper member mounted between the bottom of the slot and the blade root, the blade root configured to bear against the resilient damper member, at least prior to the bistable member occupying the second stable position, and

a support of elongate shape, including a first zone in which the resilient damper member is mounted and a second zone in which a bistable spring in a form of a resilient strip is mounted, the spring being deformable between the first and second stable positions,

wherein, in the second zone, the support includes a base and two branches projecting from the base, and the spring is fastened to ends of the branches.

2. A rotor wheel according to claim 1 , wherein the bistable member is made of a shape memory material that is deformable by mechanical, thermal, or electrical stress.

3. A rotor wheel according to claim 1 , wherein the support including at least one access opening for passing a tool for causing the bistable member to pass from the second stable position to the first stable position.

4. A rotor wheel according to claim 1 , wherein the resilient damper member is in a form of at least one pad of resilient material, or of elastomer.

5. A rotor wheel according to claim 1 , wherein shape and mass of the bistable member are determined so that the bistable member is caused to pass from the first stable position to the second stable position by centrifuging.

6. A rotor wheel according to claim 5 , wherein the shape and the mass of the bistable member are determined so that the bistable member is caused to pass from the first stable position to the second stable position by rotating a wheel at a speed greater than 2000 rpm.

7. A rotor wheel according to claim 1 , wherein, in the second zone, the support presents a generally U-shaped section in which the base is beside a bottom of the slot and the two branches project therefrom.

8. A rotor wheel according to claim 7 , wherein the spring includes a flyweight.

9. A rotor wheel according to claim 7 , wherein the branches of the support include grooves or notches.

10. A method of assembling and balancing a rotor wheel according to claim 1 , the method comprising:

assembling the blade and the spacer in an assembly position in the slot of the disk;

rotating the rotor wheel at a speed that is sufficient to cause the blade to move by centrifuging into a normal operating position, and to cause the bistable member to pass into the second stable position to stabilize the blade in the operating positions; and

reducing unbalance of the rotor wheel.

11. A method according to claim 10 , wherein the reducing unbalance of the rotor wheel is performed by disassembling and interchanging the blade.

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 30, 2014
From: CHATENET, LUC HENRI; LE QUELLEC, JOHN
To: SNECMA
Reel/Frame 032096/0958 →