IP Library Granted Patent US 9,970,298
Granted Patent B2
US 9,970,298 · App. 14/761,178 · Granted May 15, 2018

Balancing screw, device and method for a rotating part of a turbine engine

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Quick Facts
Patent No.
US 9,970,298
App. No.
14/761,178
Granted
May 15, 2018
Kind
B2
Abstract

A balancing device for a rotating part of a turbomachine, includes a ferrule pierced with a plurality of ports, a balancing screw passing through each port, each balancing screw including a body and a head, the head of each balancing screw being pierced with a recess, the balancing screws being of at least one first type, the recess of the screws of the first type being formed by a driving recess from which an additional recess extends.

Claims (20)

1. A balancing device for a rotating part of a turbomachine, comprising a ferrule pierced with a plurality of ports, and a balancing screw passing through each port of the plurality of ports, each balancing screw including a body and a head, the head being pierced with a recess, wherein the balancing screws are of a first type and a second type, wherein the recess of the balancing screw of the first type is formed by a driving recess and by an additional recess, the driving recess having a bottom, the bottom of the driving recess being pierced with the additional recess, and wherein the recess of the balancing screw of the second type is formed only by a second driving recess.

2. The balancing device according to claim 1 , wherein:

the balancing screws of the first type are made of a material having a first density m 1 ,

the balancing screws of the second type are made of a material having a second density m 2 , m 2 being strictly higher than m 1 .

3. The balancing device according to claim 2 , wherein:

the balancing screws of the first type are made of titanium;

the balancing screws of the second type are made of steel.

4. The balancing device according to claim 1 , wherein:

the screws of the first type have a length l 1 ;

the screws of the second type have a length l 2 , l 2 >l 1 .

5. The balancing device according to claim 1 , wherein the balancing screw heads are cylindrical.

6. The balancing device according to claim 1 , wherein:

the head of each balancing screw of the first type has a mass at least equal to 60% of a total mass of said balancing screw; and/or

the head of each balancing screw of the second type has a mass at least equal to 40% of a total mass of said balancing screw.

7. The balancing device according to claim 1 , further comprising additional balancing screws, each additional balancing screw having a mass between the mass of one of the screws of the first type and the mass of one of the screws of the second type.

8. A method for balancing a rotating part of a turbomachine provided with the balancing device according to claim 1 , the method comprising adjusting a depth of the recess of the balancing screw of the first type and/or the recess of the balancing screw of the second type so as to balance the rotating part.

9. The balancing method according to claim 8 , further comprising adjusting one or more of the following parameters to balance the rotating part:

external dimensions of each of the heads;

a shape of the screw heads;

a material of the balancing screws.

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 Jul 15, 2015
From: LE STRAT, JEAN-LUC; POHIER, HERVÉ; THORY, ROMAIN JEAN-LOUIS ROBERT
To: SNECMA
Reel/Frame 036097/0506 →