MOBILE REPAIR AND MANUFACTURING APPARATUS AND METHOD FOR GAS TURBINE ENGINE MAINTENANCE

• US 20160229005A1
• Filed: 01/20/2016
• Published: 08/11/2016
• Est. Priority Date: 02/05/2015
• Status: Abandoned Application

• Current Assignee: Siemens Energy Incorporated (Siemens AG)
• Original Assignee: Siemens Energy Incorporated (Siemens AG)
• Inventors: Ryan, Daniel J., Kamel, Ahmed, Bruck, Gerald J., Jouini, Dhafer
• Application Number:
  US15/001,276
• Publication Number:
  US 20160229005A1
• Time in Patent Office: Days
• US Class Current: 1/1
• CPC Class Codes: B22F 10/25 Direct deposition of metal particles, e.g. direct metal deposition [DMD] or laser engineered net shaping [LENS]
• CPC Class Codes: B22F 10/64 by thermal means control of energy beam parameters for post heating B22F10/364
• CPC Class Codes: B22F 12/41 characterised by the type, e.g. laser or electron beam
• CPC Class Codes: B22F 5/009 of turbine components other than turbine blades of turbine blades B22F5/04
• CPC Class Codes: B23K 1/0018 Brazing of turbine parts
• CPC Class Codes: B23K 1/0056 soldering by means of beams, e.g. lasers, E.B.
• CPC Class Codes: B23K 1/19 taking account of the properties of the materials to be soldered
• CPC Class Codes: B23K 1/20 Preliminary treatment of work or areas to be soldered, e.g. in respect of a galvanic coating preparation of surfaces in particular ways, see the relevant classes for the treatments or the materials treated, e.g. C04B, C23C
• CPC Class Codes: B23K 2101/001 Turbines
• CPC Class Codes: B23K 2103/26 Alloys of Nickel and Cobalt and Chromium
• CPC Class Codes: B23K 26/0869 Devices involving movement of the laser head in at least one axial direction
• CPC Class Codes: B23K 26/14 using a fluid stream, e.g. a jet of gas, in conjunction with the laser beam; Nozzles therefor B23K26/12 takes precedence
• CPC Class Codes: B23K 26/342 Build-up welding
• CPC Class Codes: B23K 26/70 Auxiliary operations or equipment
• CPC Class Codes: B23K 26/702 Auxiliary equipment
• CPC Class Codes: B23K 37/0294 Transport carriages or vehicles
• CPC Class Codes: B23P 6/002 Repairing turbine components, e.g. moving or stationary blades, rotors, B23P6/045 takes precedence
• CPC Class Codes: B33Y 10/00 Processes of additive manufacturing
• CPC Class Codes: B33Y 30/00 Apparatus for additive manufacturing; Details thereof or accessories therefor
• CPC Class Codes: C21D 1/38 Heating by cathodic discharges
• CPC Class Codes: C21D 9/50 : for welded joints
• CPC Class Codes: F01D 25/285 : Temporary support structures, e.g. for testing, assembling, installing, repairing; Assembly methods using such structures
• CPC Class Codes: F01D 5/005 : Repairing methods or devices
• CPC Class Codes: Y02P 10/25 : Process efficiency
• CPC Class Codes: Y02T 50/60 : Efficient propulsion technologies, e.g. for aircraft

Abstract

Refurbishment of hot gas path components of gas turbine engines can now be performed locally in lieu of the traditional use of a specialized fixed regional repair facility. A mobile manufacturing platform (10) is provided with the capability to inspect and to repair ceramic coated superalloy alloy components, including the ability to perform flux assisted laser processing (68) of powdered materials. The mobile platform may include a powder mixing capability (32) for custom on-site mixing of proprietary powder compositions from a standardized powder inventory (34). A communications element (36) conveys the proprietary powder compositions from a remote home office location (38). Superalloy components can now be repaired (62) or fabricated (80) on-site by qualified technicians rather than certified welders. The mobile platform may be self-powered by a vehicle hybrid power unit or a renewable energy source.

Claims

1. A method comprising:

providing a mobile manufacturing platform comprising a laser processing element;

transporting the mobile manufacturing platform to proximate a location of a gas turbine engine to be serviced;

transferring a service run hot gas path component removed from the gas turbine engine to the mobile manufacturing platform;

inspecting the service run component and determining a necessary repair or alternatively a need for the service run component to be scrapped and replaced with a replacement component;

repairing a superalloy material portion of the service run component, or alternatively fabricating the replacement component comprising superalloy material, with the laser processing element using a flux assisted process; and

installing the repaired component, or alternatively the replacement component, into the gas turbine engine.

2. The method of claim 1, further comprising mixing a powder mixture appropriate for the repairing or fabricating step in a powder mixing element of the mobile manufacturing platform.

3. The method of claim 2, further comprising providing instructions for performing the mixing step from a remote location via a communications element of the mobile manufacturing platform such that a formulation of the powder mixture exists at the mobile manufacturing platform only as a transient electronic instruction.

4. The method of claim 2, further comprising mixing the appropriate powder mixture from a group of constituent powders maintained in a powder inventory of the mobile manufacturing platform.

5. The method of claim 4, wherein the powder inventory comprises at least two of the group of metal, alloy, ceramic and flux powders.

6. The method of claim 1, further comprising preparing a powder appropriate for the repairing or fabricating step in a powder manufacturing element of the mobile manufacturing platform.

7. The method of claim 6, further comprising preparing a powder comprising composite alloy/flux particles in the powder manufacturing element.

8. The method of claim 1, further comprising utilizing the laser processing element to perform a flux assisted cleaning of the service run component.

9. The method of claim 1, further comprising utilizing the laser processing element to perform a heat treatment of the repaired component or alternatively the replacement component.

10. The method of claim 1, further comprising providing the laser processing element to have a tunable laser frequency capability to facilitate processing of a plurality of types of materials.

11. A mobile manufacturing platform apparatus comprising:

a transportation element configured for movement among any of a plurality of locations;

a laser processing element disposed on the transportation element; and

a powder mixing element disposed on the transportation element for mixing powder material compositions for use by the laser processing element.

12. The apparatus of claim 11, further comprising a communications element associated with the transportation element operable to receive transient electronic powder material composition information from a remote location for operating the powder mixing element.

13. The apparatus of claim 12, further comprising an inventory of constituent powders in a powder inventory.

14. The apparatus of claim 13, further comprising a flux material in the powder inventory.

15. The apparatus of claim 14, further comprising no shielding gas stored on the transportation element.

16. The apparatus of claim 11, wherein the transportation element comprises a hybrid drive system configured to function as a power element to provide electrical power for the mobile manufacturing platform.

17. The apparatus of claim 11, wherein the laser processing element comprises a tunable laser.

18. The apparatus of claim 11, wherein the laser processing element comprises a powder manufacturing element.

19. The apparatus of claim 11, further comprising a heat treating element, wherein the heat treating element comprises a laser of the laser processing element.

20. The apparatus of claim 11, further comprising a component preparation element, wherein the component preparation element comprises a laser of the laser processing element.