Rotor tip clearance

Patent metadata

Field	Value
Publication number	US-9957829-B2
Application number	US-201414890939-A
Country	US
Kind code	B2
Filing date	May 12, 2014
Priority date	May 29, 2013
Publication date	May 1, 2018
Grant date	May 1, 2018

Abstract

A method of setting a clearance between a rotor and a stator of a rotor assembly for a turbine engine. The rotor assembly has a plurality of rotor-to-stator stages and the stator has a nominal centerline. Typically the stator is a casing or an array of vane tips. The method includes (i) correlating in-service rotor-to-stator rub patterns for a rotor-to-stator stage of a number of turbine engines, (ii) setting a position of a machining centerline relative to the nominal centerline of the stator, the position being towards a heavy rub, (iii) machining the stator about the machining centerline, (iv) repeating steps (i) to (ii) for each rotor-to-stator stage of the plurality of the rotor-to-stator stages, wherein the machined stator having been formed by at least two machining steps having different center-lines.

First claim

The invention claimed is:

1. A method of setting a clearance between a rotor and a stator of a rotor assembly for a turbine engine, the rotor assembly having a plurality of rotor-to-stator stages, the stator having a nominal centerline, wherein the rotor assembly comprises either;
the rotor assembly having the rotor including an array of radially extending blades and the stator including a casing and the clearance is defined between the blades and the casing, or
the rotor assembly having the rotor including a rotor drum and the stator having an array of radially extending stator vanes and the clearance is defined between the rotor drum and the stator vanes, wherein the method comprising:
(i) correlating in-service rotor-to-stator rub patterns for a rotor-to-stator stage of a number of turbine engines,
(ii) setting a position of a machining centerline relative to the nominal centerline of the stator, the position being towards a heavy rub,
(iii) machining the stator about the machining centerline,
(iv) repeating steps (i) to (iii) for each rotor-to-stator stage of the plurality of the rotor-to-stator stages,
wherein the machined stator having been formed by at least two machining steps at different axial positions having different center-lines.

2. The method of setting a clearance between a rotor and a stator of a rotor assembly as claimed in claim 1 ,
wherein the stator has a nominal diameter,
the method further comprises:
setting a machining diameter of the stator relative to the nominal diameter of the stator.

3. The method of setting a clearance between a rotor and a stator of a rotor assembly as claimed in claim 2 ,
wherein the step of setting a machining diameter of the stator relative to the nominal diameter of the stator is completed only where there are no opposing light rub marks.

4. The method of setting a clearance between a rotor and a stator of a rotor assembly as claimed in claim 2 ,
wherein the step of setting a machining diameter of the stator relative to the nominal diameter of the stator involves a reduction in the machining diameter.

5. The method of setting a clearance between a rotor and a stator of a rotor assembly as claimed in claim 1 , wherein the method further comprises:
machining the stator an axial extent based on the axial extent of the rotor-to-stator rub.

6. The method of setting a clearance between a rotor and a stator of a rotor assembly as claimed in claim 1 , wherein the method further comprises:
machining the stator an axial extent based the axial extent of the rotor or stator stage.

7. The method of setting a clearance between a rotor and a stator of a rotor assembly as claimed in claim 1 ,
wherein the step of machining the stator includes machining a smooth blend between the two machining steps having different center-lines.

8. The method of setting a clearance between a rotor and a stator of a rotor assembly as claimed in claim 1 ,
wherein the rotor assembly comprises a rotor having the array of radially extending blades and the casing, the clearance is defined between the blades and the casing.

9. The method of setting a clearance between a rotor and a stator of a rotor assembly as claimed in claim 8 ,
wherein the casing comprises an abradable coating at least in a location radially outwardly of the rotor,
the method further comprising:
reducing the clearance on stages with an abradable coating to a greater extent than on stages without an abradable coating.

10. The method of setting a clearance between a rotor and a stator of a rotor assembly as claimed in claim 1 ,
wherein the rotor assembly comprises a rotor having the rotor drum and the stator having the array of radially extending stator vanes, and the clearance is defined between the rotor drum and the stator vanes.

11. The method of setting a clearance between a rotor and a stator of a rotor assembly as claimed in claim 1 ,
wherein the stator is any one or both of the casing or the stator vane.

12. The method of setting a clearance between a rotor and a stator of a rotor assembly as claimed in claim 1 ,
wherein the step of correlating in-service rotor-to-stator rub patterns includes recording the circumferential positions of the start and the end of a rub to determine a rub length.

13. The method of setting a clearance between a rotor and a stator of a rotor assembly as claimed in claim 12 ,
wherein the step of correlating in-service rotor-to-stator rub patterns includes setting a predetermined rub length where a rub length greater than the predetermined length is indicative of the heavy rub.

14. The method of setting a clearance between a rotor and a stator of a rotor assembly as claimed in claim 13 , where the (ii) setting step comprises setting the position of the machining centerline towards the heavy rub to increase the clearance at the heavy rub.

15. The method of setting a clearance between a rotor and a stator of a rotor assembly as claimed in claim 14 , wherein a rub length less than the predetermined length is indicative of a light rub and wherein the (ii) setting step further comprises setting the position of the machining centerline to maintain the clearance at the light rub.

16. The method of setting a clearance between a rotor and a stator of a rotor assembly as claimed in claim 1 , wherein the casing of the stator surrounds the plurality of the rotor-to-stator stages and supports the array of radially extending stator vanes with rotatable mountings.

17. The method of setting a clearance between a rotor and a stator of a rotor assembly as claimed in claim 1 , wherein the turbine engine further comprises:
a compressor section;
a combustor section; and
a turbine section;
a shaft;
wherein the compressor section, the combustor section and the turbine section are generally arranged in flow series and generally in a direction of a longitudinal axis;
wherein the shaft is rotatable about the longitudinal axis and wherein the shaft drivingly connects turbine section to the compressor section;
wherein the rotor assembly is one of the compressor section and the turbine section and wherein the different axial positions correspond to different stages of the rotor assembly spaced apart along the longitudinal axis.

18. The method of setting a clearance between a rotor and a stator of a rotor assembly as claimed in claim 17 , wherein the combustor section comprises a burner plenum, a plurality of combustion chambers positioned within the burner plenum and a plurality of burners wherein a respective burner is fixed to each combustion chamber.

Assignees

• Siemens Ag

Inventors

• Shepherd Andrew

Classifications

• F05D2220/32

  in gas turbines · CPC title

• F05D2240/55

  Seals · CPC title

• F01D9/041

  using blades (F01D5/148 takes precedence) · CPC title

• F01D25/24

  Casings (modified for heating or cooling F01D25/14); Casing parts, e.g. diaphragms, casing fastenings (casings for rotary machines or engines in general F16M {; special arrangements in stators dealing with breaking-off of part of rotor F01D21/045}) · CPC title

• F01D5/12

  Blades ({specially adapted for radial flow machines or engines F01D5/04}; blade roots F01D5/30; rotors with blades adjustable in operation F01D7/00; stator blades F01D9/02) · CPC title