Rotor balancing

Patent metadata

Field	Value
Publication number	US-9938832-B2
Application number	US-201514694778-A
Country	US
Kind code	B2
Filing date	Apr 23, 2015
Priority date	May 23, 2014
Publication date	Apr 10, 2018
Grant date	Apr 10, 2018

Abstract

A balancing kit and balancing method is provided for balancing a rotating component. The balancing kit comprises a receptacle and a balancing mass. The balancing mass comprises a pin that may be passed through a corresponding slot in a plate of the receptacle during installation. To complete installation, the balancing mass is rotated so that the pin can no longer pass through the slot, and is instead retained in an installed position in which the pin rests on a lower surface of the plate. The balancing mass can be removed by the reverse process.

First claim

I claim:

1. A balancing kit for balancing a rotating part of a gas turbine engine comprising:
a balancing mass having:
an interface portion defining tooling interface;
a retaining member; and
a resilient member located between the interface portion and the retaining member, and

a receptacle for receiving the balancing mass having:
a receiving opening for receiving the balancing mass; and
a retaining plate having an upper surface and a lower surface, and a hole extending therethrough, the hole being non-axisymmetric about a longitudinal axis of the receptacle, wherein:

the retaining member of the balancing mass is arranged to be able to pass through the hole for installation in the receptacle, and the balancing mass can be rotated via its tooling interface such that the retaining member rests on the lower surface of the retaining plate to thereby removably secure the balancing mass to the receptacle in an installed position under the action of the resilient member.

2. A balancing kit according to claim 1 , wherein:
the hole extending through the retaining plate comprises at least one slot; and
the retaining member is arranged to pass through the slot for installation in the receptacle.

3. A balancing kit according to claim 1 , wherein, in the installed position the resilient member is compressed between the interface portion of the balancing mass and the upper surface of the retaining plate of the receptacle.

4. A balancing kit according to claim 1 , wherein:
the balancing mass extends along a longitudinal axis, with the interface portion at a proximal end region of the longitudinal axis, and the retaining member at an opposing distal end region of the longitudinal axis.

5. A balancing kit according to claim 4 , wherein:
the interface portion has a cross-section that has an outer perimeter that is axisymmetric about the longitudinal axis of the balancing mass;
the receiving opening has a cross-section that has an inner perimeter that is axisymmetric about the longitudinal axis of the balancing mass; and
the tooling interface is arranged so as to be able to rotate the balancing mass about the longitudinal axis of the balancing mass into the installed position.

6. A balancing kit according to claim 4 , wherein:
the balancing mass comprises a main body extending from the interface portion along the longitudinal axis of the balancing mass; and
the retaining member extends from the main body and is not axisymmetric about the longitudinal axis of the balancing mass.

7. A balancing kit according to claim 6 , wherein the main body is axisymmetric about the longitudinal axis of the balancing mass.

8. A balancing kit according to claim 6 , wherein the retaining member comprises at least one elongate pin extending in a plane perpendicular to the longitudinal axis of the balancing mass.

9. A balancing kit according to claim 6 , wherein at least a part of the main body passes through the hole in the retaining plate when in the installed position.

10. A balancing kit according to claim 1 , wherein the lower surface of the retaining plate comprises a retaining recess having a shape that corresponds to that of the retaining member, such that in the installed position, the retaining member engages the retaining recess.

11. A rotor for a gas turbine engine comprising at least one balancing kit according to claim 1 , wherein the receptacle of the or each balancing kit is provided to the rotor, and at least one of the or each receptacle is provided with its respective balancing mass.

12. A rotor for a gas turbine engine according to claim 11 comprising at least two balancing kits, wherein at least one of the receptacles is not provided with a respective balancing mass.

13. A rotor for a gas turbine engine according to claim 11 comprising at least two balancing kits, wherein at least two receptacles are provided with balancing masses that have different masses to each other.

14. A gas turbine engine comprising a rotor balanced using the balancing kit according to claim 1 .

15. A method of balancing a rotor of a gas turbine engine comprising:
providing the rotor with at least one receptacle for receiving a respective balancing mass, the receptacle having:
a receiving opening for receiving the balancing mass; and
a retaining plate having an upper surface and a lower surface, and a hole extending therethrough, the hole being non-axisymmetric about a longitudinal axis of the receptacle the method further comprising

installing a balancing mass to one or more selected receptacles in order to balance the rotor, the balancing mass having:
an interface portion defining tooling interface;
a retaining member; and
a resilient member located between the interface portion and the retaining member,

wherein the step of installing the balancing mass to its respective receptacle comprises:
passing the retaining member through the hole; and
rotating the balancing mass into an installed position by providing torque to its tooling interface, in which installed position the retaining member rests on the lower surface of the retaining plate to thereby removably secure the balancing mass to the receptacle under the action of the resilient member.

16. A method of balancing a rotor according to claim 15 , wherein, during the step of passing the retaining member through the hole, the resilient member is supported on the upper surface of the plate so as to be compressed between the plate and the interface portion.

17. A gas turbine engine comprising a rotor balanced using the method according to claim 15 .

Assignees

• Rolls Royce Plc

Inventors

• Bakker Mattheus

Classifications

• F05D2260/30

  Retaining components in desired mutual position · CPC title

• F01D5/027 Primary

  Arrangements for balancing (for balancing rotating bodies in general F16F15/32; for compensating imbalance G01M1/36) · CPC title

• B25B23/105

  the gripping device being an integral part of the driving bit · CPC title

• F05D2260/15

  Load balancing · CPC title

• B25B13/481

  for operating in areas having limited access · CPC title