TOOL FOR BALANCING A TURBINE ENGINE MODULE COMPRISING A CANTILEVERED STATOR

• US 20200131908A1
• Filed: 10/30/2019
• Published: 04/30/2020
• Est. Priority Date: 10/31/2018
• Status: Active Grant

• Current Assignee: Safran Aircraft Engine Company
• Original Assignee: Safran Aircraft Engine Company
• Inventors: LUINAUD, Alain Roland, DECOCQ, Alain
• Granted Patent: US 11,143,031 B2
• Time in Patent Office: Days
• CPC Class Codes: B23P 6/005 using only replacement pieces of a particular form
• CPC Class Codes: F01D 5/005 Repairing methods or devices
• CPC Class Codes: F05D 2220/323 for aircraft propulsion, e.g. jet engines
• CPC Class Codes: F05D 2230/80 Repairing, retrofitting or upgrading methods
• CPC Class Codes: G01M 1/04 Adaptation of bearing support assemblies for receiving the body to be tested
• CPC Class Codes: G01M 1/16 by oscillating or rotating the body to be tested

Abstract

A tool for balancing a turbine engine module in a balancer, the module including a stator, a rotor and a shaft, the balancer including at least one power drive unit and a table equipped with two support of the shaft of the module. The tool includes at least: one stator support, fixed on the table of the balancer behind the supports, a tubular false bearing, configured to support a bearing for guiding the rotor in the stator and protruding outside of the stator, a guiding sleeve of the shaft, confining a support of the false bearing, and received on the supports of the balancer, a rear support plate of the stator, fixed to the support of the stator, and immobilising the rotor with respect to the stator, a front support plate of the stator, fixed to the stator support, and immobilising and centring the false bearing.

Claims

1. Tool for balancing a turbine engine module in a balancer, said module comprising at least one stator and one rotor comprising a shaft of longitudinal axis A configured to be guided by a guiding bearing inside the stator and at least one blades stage which is connected to a longitudinal end portion of said shaft and which is surrounded by said stator, and said balancer comprising at least, from the front to the rear, a power drive unit and a table provided with two front and rear supports for maintaining the shaft of the module, wherein said tool comprises at least:

one stator support, intended to be fixed axially adjustably on the table of the balancer behind the supports for maintaining the shaft (18) of the module,

a tubular false bearing, configured to support a guiding bearing of the rotor in the stator and comprising a front fixing support configured to extend outside of the stator,

a guiding sleeve, comprising a rear end configured to confine the front fixing support of the false bearing, a front end comprising inner guiding means of the shaft of the rotor, and which is configured to be received on the rear and front supports of the table of the balancer,

a rear support plate of the stator, intended to be fixed to the support of the stator, and comprising means for immobilising the rotor with respect to the stator,

a front support plate of the stator, intended to be fixed to the support of the stator, and comprising means for immobilising and centring the false bearing.

2. Tool according to claim 1, wherein the stator support comprises two front and rear plates, vertically and transversally adjustable independently and configured to support the front and rear ends of said stator.

3. Tool according to claim 2, wherein the rear plate has the shape of a disk pierced with a circular opening in its centre, which comprises:

a lower foot for fixing to the rear plate,

means for fixing the stator on its outer periphery, and

radial arms, radially adjustable by sliding, which extend radially inwards from the edges of the circular opening of the rear plate and which comprise at their free ends of the axial buttons which are configured to extend axially inside a pin of the rotor and to cooperate with an inner support of said pin to immobilise it with respect to the stator.

4. Tool according to claim 2, wherein the front plate has the shape of a disk pierced with a circular opening in its centre, and which comprises:

a lower foot for fixing to the front plate,

means for fixing the stator on its outer periphery, and

at least three radial arms, radially adjustable by sliding which extend radially inwards from the edges of the circular opening of the front plate, and which comprise at their free ends, cylinder angular section-shaped supports which are complementary to an outer periphery of the false bearing.

5. Tool according to claim 4, wherein the tubular false bearing comprises a rear, inner support forming a track of the bearing for guiding the rotor, and on its periphery, behind its outer support for fixing to the sleeve, an outer groove for receiving the ends of the radial arms of the front plate.

6. Tool according to claim 1, wherein the tubular guiding sleeve is produced in the form of two respectively lower and upper, contiguous shells along a horizontal plane and configured to be fixed together, which each comprise, at their rear end, a semi-cylindrical, inner housing complementary to the front support for fixing to the false bearing, said lower shell comprising, outside of each of its rear and front ends, means for fixing to the rear and front supports for maintaining the balancer, and, inside its front end, a transversal plate supporting two rollers of longitudinal axis on which the shaft of the module is intended to roll, the position of said plate being vertically and transversally adjustable with respect to said front end of the lower shell of the guiding sleeve.

7. Calibration assembly for adjusting a tool according to claim 6, wherein it comprises a standard rotor, of moment of inertia and out-of-balance corresponding substantially to the rotor of the module to be balanced, comprising a standard rotor mass and a standard rotor shaft, and an adapter ring configured to receive a rear end of the standard rotor shaft and to be received in the rear support of the balancer.

8. Method for balancing a standard rotor according to claim 7, wherein it comprises a first step, during which the standard rotor is inserted in the adapter ring, a second step, during which the standard rotor is arranged in the rear support of the balancer and during which it is coupled with the power drive unit, and a third step, during which the standard rotor is balanced.

9. Method for adjusting a tubular sleeve and a stator support of a tool according to claim 1 using a standard rotor, of moment of inertia and out-of-balance corresponding substantially to the rotor of the module to be balanced, comprising a standard rotor mass and a standard rotor shaft, and an adapter ring configured to receive a rear end of the standard rotor shaft and to be received in the rear support of the balancer, balanced according to a method comprising a first step, during which the standard rotor is inserted in the adapter ring, a second step, during which the standard rotor is arranged in the rear support of the balancer and during which it is coupled with the power drive unit, and a third step, during which the standard rotor is balanced, wherein said method for adjusting said tubular sleeve comprises:

a first step, during which the standard rotor is inserted in the false bearing,

a second step, during which the false bearing equipped with the standard rotor shaft is inserted in the tubular guiding sleeve, a third step, during which the standard rotor equipped with the tubular guiding sleeve is arranged in the front and rear supports of the balancer,

a fourth step, during which the standard rotor is rotated to determine its axis default and during which said default is corrected by adjusting the transversal and horizontal positions of the plate of the tubular guiding sleeve,

a fifth step, during which the standard rotor of the false bearing is dismounted and the false bearing is dismounted from the guiding sleeve,

a sixth step, during which the front support plate of the stator is assembled to the false bearing,

a seventh step, during which the standard rotor is inserted in the false bearing,

an eighth step, during which the stator of the front plate and the rear plate are assembled to the stator to constitute a standard module,

a ninth step, during which the guiding sleeve is assembled to the false bearing,

a tenth step, during which the standard module equipped with the guiding sleeve is arranged on the rear and front supports for maintaining the module and on the stator support,

an eleventh step, during which the front and rear plates of the stator support are adjusted so as to support the front and rear support plates of the stator, while allowing the free rotation of the standard rotor in the stator.

10. Method for balancing a turbine engine module using a tool according to claim 1, wherein it comprises:

a first step, during which the front plate is assembled to the false bearing,

a second step, during which the rear support plate of the stator is assembled to the stator and to the blades stage,

a third step, during which the stator rear support plate, the stator, and the blades stage already assembled, are assembled to the front plate and to the false bearing,

a fourth step, during which the guiding sleeve is assembled to the false bearing,

a fifth step, during which the module equipped with the guiding sleeve is arranged on the rear and front supports for maintaining the shaft of the module and on the stator support,

a sixth step of balancing the module in the balancer.

11. Assembly table for assembling a turbine engine module to a tool according to claim 1, wherein it comprises a mounting plate in the form of a disk, complementary of the front support plate of the stator, comprising a circular opening in its centre, on the edges of which are arranged at least three centring legs extending axially from said mounting plate and arranged according to a diameter corresponding to that of an outer support of the false bearing.