Method of remanufacturing a machine component

Patent metadata

Field	Value
Publication number	US-9593595-B2
Application number	US-201414251804-A
Country	US
Kind code	B2
Filing date	Apr 14, 2014
Priority date	Apr 14, 2014
Publication date	Mar 14, 2017
Grant date	Mar 14, 2017

Abstract

A method is provided for remanufacturing a machine component having multiple holes. The holes are provided to match in alignment with corresponding holes of an adjacent component in a machine assembly. First and second sets of holes are selected from the holes of the machine component on the basis of being located within first and second limits of positional tolerance with respect to corresponding holes of the adjacent component. Each hole from the first set of holes is bored to define openings in axial alignment with holes of the adjacent component. Each hole from the second set of holes is bored to an enlarged diameter and then plugged with a deformable insert. Each of these inserts is then drilled to define openings in axial alignment with holes of the adjacent component.

First claim

We claim:

1. A method of remanufacturing a machine component having a plurality of holes, wherein the holes are to be matched with corresponding holes of an adjacent component in a machine assembly for co-axially receiving fasteners therein, the method of remanufacturing comprising:
selecting a first set of holes from the plurality of holes on the machine component that lie within a first limit of positional tolerance with respect to a first portion of the corresponding holes of the adjacent component;
boring each hole from the first set of holes to a first enlarged diameter to define openings in axial alignment with the first portion of the corresponding holes of the adjacent component;
selecting a second set of holes from the plurality of holes on the machine component that lie outside the first limit of positional tolerance with respect to a second portion of the corresponding holes of the adjacent component;
boring each hole from the second set of holes to a second enlarged diameter;
plugging each of the bored second set of holes with a deformable insert; and
drilling the inserts to define openings in axial alignment with the second portion of the corresponding holes of the adjacent component.

2. The method of claim 1 , wherein selecting the first set of holes and selecting the second set of holes includes selecting holes positioned at an axial offset from corresponding holes of the adjacent component.

3. The method of claim 1 , wherein the second set of holes are selected on the basis of the holes being located within a second limit of positional tolerance with respect to corresponding holes of the adjacent component.

4. The method of claim 3 , wherein the first limit is lesser than the second limit.

5. The method of claim 1 , wherein selecting the second set of holes includes selecting holes having a diameter greater than a diameter of the corresponding holes on the adjacent component.

6. The method of claim 1 , wherein an axis of drilling the inserts is co-axial to a centric axis of corresponding holes of the adjacent component.

7. A flange remanufactured using the method of claim 1 .

8. The flange of claim 7 , wherein the flange forms part of an exhaust diffuser of a gas turbine engine.

9. A method of configuring a deformed first flange for fitment onto a second flange, wherein the first flange comprises holes axially offset from corresponding holes of the second flange, the method comprising:
determining a first set of holes from the holes of the first flange that lie within a first limit of positional tolerance with respect to the corresponding holes of the second flange;
determining a second set of holes from the holes of the first flange that lie within a second limit of positional tolerance with respect to the corresponding holes of the second flange;
boring the first set of holes and the second set of holes to enlarged diameters to form a bored first set of holes and a bored second set of holes, wherein the bored first set of holes are disposed in axial alignment with the corresponding holes of the second flange to receive fasteners therethrough;
plugging each of the bored second set of holes with a deformable insert; and
drilling the deformable inserts to define openings in axial alignment with the corresponding holes of the second flange.

10. The method of claim 9 , wherein determining the second set of holes includes determines holes having a diameter greater than a diameter of the corresponding holes on the second flange.

11. The method of claim 9 , wherein an axis of drilling the inserts is co-axial to a centric axis of the corresponding holes of the adjacent component.

12. The method of claim 9 , wherein the first limit of positional tolerance and the second limit of positional tolerance are pre-defined tolerance limits.

13. The method of claim 9 , wherein the first limit of positional tolerance is lesser than the second limit of positional tolerance.

14. A flange of an exhaust diffuser, wherein the flange is remanufactured using the method of claim 9 .

15. A gas turbine engine employing the exhaust diffuser of claim 14 .

16. A remanufactured machine component for attachment to an adjacent component, the machine component comprising:
a flange configured to be coupled by a plurality of fasteners to the adjacent component in a machine assembly;
a first set of holes bored into the flange with a first enlarged diameter to define first openings in axial alignment with a first portion of corresponding holes of the adjacent component for co-axially receiving the fasteners;
a second set of holes bored into the flange, the second set of holes having a second enlarged diameter; and
a plurality of inserts disposed within the second set of holes, wherein the inserts define second openings in axial alignment with a second portion of the corresponding holes of the adjacent component for co-axially receiving the fasteners therethrough,
wherein the first set of holes are located within a first limit of positional tolerance with respect to the first portion of the corresponding holes of the adjacent component, and
wherein the second set of holes are located outside the first limit of positional tolerance with respect to the second portion of the corresponding holes of the adjacent component.

17. The remanufactured machine component of claim 16 , wherein the first set of holes are positioned in axial alignment with corresponding holes of the adjacent component.

Assignees

• Solar Turbines Inc
• Solar Turbines Inc

Inventors

• Nava Irene
• Mcclintic Glenn R

Classifications

• B23B35/00

  Methods for boring or drilling, or for working essentially requiring the use of boring or drilling machines; Use of auxiliary equipment in connection with such methods · CPC title

• F01D25/243 Primary

  Flange connections; Bolting arrangements (F01D25/265 takes precedence) · CPC title

• B23P6/002

  Repairing turbine components, e.g. moving or stationary blades, rotors, (B23P6/045 takes precedence) · CPC title

• B23B2215/76

  Components for turbines · CPC title

• F01D25/285

  Temporary support structures, e.g. for testing, assembling, installing, repairing; Assembly methods using such structures · CPC title