Modular gas turbine engine assembly

• US 4,030,288 A
• Filed: 11/10/1975
• Issued: 06/21/1977
• Est. Priority Date: 11/10/1975
• Status: Expired due to Term

• Current Assignee: Caterpillar Incorporated
• Original Assignee: Caterpillar Tractor Co (Caterpillar Incorporated)
• Inventors: Keedy, David Edward, Davis, Warren Wiley
• Primary Examiner(s): Croyle, Carlton R.
• Assistant Examiner(s): Casaregola, L. J.
• Application Number:
  US05/630,476
• Time in Patent Office: 589 Days
• Field of Search: 415/68, 415/189, 415/201, 60/39.16, 60/39.31, 60/39.32
• US Class Current: 60/791
• CPC Class Codes: F01D 11/005 Sealing means between non relatively rotating elements
• CPC Class Codes: F01D 11/08 for sealing space between rotor blade tips and stator specially-shaped blade tips therefor F01D5/20
• CPC Class Codes: F01D 25/24 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 Class Codes: F01D 25/30 Exhaust heads, chambers, or the like
• CPC Class Codes: F01D 9/04 forming ring or sector
• CPC Class Codes: F02C 3/103 the compressor being of the centrifugal type

Abstract

The invention is concerned with a modular gas turbine engine assembly. The assembly includes a tubular case to which are assembled a gasifier module and a power output module. The gasifier module and the power output module are each slidably sealed to respective inwardly extending, generally removable flanges within the case. The gasifier module has a first tubular housing fixedly detachably attachable with a first end thereof adjacent a first end of the case with the axis of the first housing aligned generally with the axis of the case, a compressor generally within a second end of said first housing, a combustor generally extending outwardly from said first end of said first housing and a first integral shaft extending from the compressor to adjacent the combustor. A gasifier turbine extends generally outwardly radially from the shaft and has first blades positioned to be in the path of the exhaust gases exiting the combustor to drive the first shaft and thereby drive the compressor. The power output module has a second tubular housing fixedly detachably attachable with a first end thereof adjacent a second end of the case with the axis of the second housing aligned generally with the axis of the case, a power turbine generally extending outwardly from the first end of the second housing having second blades positioned to be in the path of the exhaust gases exiting the gasifier turbine, output gear means, and a second shaft driven by said power turbine and driving said output gear means.

Claims

1. A modular gas turbine engine assembly, comprising:

1. a tubular case;

3. An assembly as in claim 1, including means extending from the exterior of said case for mounting it to a frame.

4. An assembly as in claim 1, wherein said gasifier turbine is detachably attachable to said first shaft so that removal of said gasifier turbine provides access to said combustor.

5. An assembly as in claim 1, including a detachably attachable extension shaft drivingly communicating said second shaft with said output gear means.

6. An assembly as in claim 1, wherein said gasifier module includes an auxiliary gear box intermediate said compressor and said combustor driven by said first shaft.

7. An assembly as in claim 1, including, extending from said second annular flange means in the gas flow path from said combustor to said power turbine:

a plurality of fixedly adjustable vanes.

8. An assembly as in claim 6, wherein said vanes receive the exhaust gases from said annular channel means and said annular channel means are supported by said second annular flange means.

9. An assembly as in claim 1, including a heat exchanger in fluid flow connection to an outlet of said compressor, an air inlet of said combustor and an exhaust outlet of said turbine attached to receive compressed gas from said compressor, heat said compressed gas therein and pass the resulting heated compressed gas to said combustor and to receive said exhaust gases from said power turbine, cool said exhaust gases therein while transferring some of the heat thereof to said compressed gas and pass the resulting cooled exhaust gases to the exterior of said heat exchanger.

10. An assembly as in claim 8, including a plurality of struts supported by said power output module and radially extending outwardly adjacent said power turbine said struts supporting at an outer end thereof an outer shroud which is positioned to direct flow of said exhaust gases from said power turbine to said heat exchanger.

11. An assembly as in claim 9, including an inner shroud supported at an inner end of said struts generally parallel to said outer shroud, said inner and outer shrouds being shaped to reduce losses due to turbulence in the flow of said exhaust gases from said power turbine to said heat exchanger.

12. An assembly as in claim 9, wherein said second slidable sealing means extends between said outer ends of said struts and said second extending means.

13. An assembly as in claim 9, including a power turbine shroud supported by said outer end of said struts and extending therefrom about said second blades in spaced relation therefrom and towards said second extending means and wherein said second slidable sealing means extends between said power turbine shroud and said extending means.

16. An assembly as in claim 13, wherein a cross-section of said bellows comprises a plurality of loops and wherein said bellows includes more of said loops opening towards a high pressure side thereof than opening towards a low pressure side thereof to provide added force against said second annular seal as said assembly operates and pressure differentials arise therewithin.

18. An assembly as in claim 8, wherein said gasifier module includes a turbine nozzle vane assembly attached to direct flow of said exhaust gases from said combustor to said first blades of said gasifier turbine, and wherein said first slidable sealing means extends between an outer ring of said turbine nozzle vane assembly and said first extending means.

21. An assembly as in claim 18, wherein said first annular fish mouth is fixedly attached to said first extending means and said first annular tongue is fixedly attached to said outer ring.

2. a gasifier module having a first tubular housing releasably secured with a first end thereof adjacent a first end of said case with the axis of said first housing aligned generally with the axis of said case, a compressor generally within a second end of said first housing, a combustor generally extending outwardly from said first end of said first housing, and a first shaft extending from said compressor to adjacent said combustor;

3. a gasifier turbine extending outwardly radially from said first shaft and having first blades positioned to be in the path of exhaust gases exiting said combustor to drive said first shaft and thereby drive said compressor;

4. a power output module having a second tubular housing releasably secured with a first end thereof adjacent a second end of said case with the axis of said second housing aligned generally with the axis of said case, a power turbine generally extending outwardly from said first end of said second housing having second blades positioned to be in the path of exhaust gases exiting said gasifier turbine, output gear means, and a second shaft driven by said power turbine and driving said output gear means;

5. annular channel means extending interiorly from said case intermediate said first and second extending means for directing said exhaust gases from said first blades to said second blades;

6. first flange means attached to the interior of said case and extending inwardly within said case generally towards said combustor;

7. second flange means attached to the interior of said case and extending inwardly within said case generally towards said power turbine;

8. first slidable sealing means for slidably adjustably sealing said gasifier module adjacent said combustor to said first extending means; and

9. second slidable sealing means for sealing said power output module adjacent said power turbine to said second extending means.

14. A modular gas turbine engine assembly, comprising:

1. A tubular case;

2. a gasifier module having a first tubular housing releasably secured with a first end thereof adjacent a first end of said case with the axis of said first housing aligned generally with the axis of said case, a compressor generally within a second end of said first housing, a combustor generally extending outwardly from said first end of said first housing, and a first shaft extending from said compressor to adjacent said combustor;

3. a gasifier turbine extending outwardly radially from said first shaft and having first blades positioned to be in the path of exhaust gases exiting said combustor to drive said first shaft and thereby drive said compressor;

17. An assembly as in claim 14, wherein said high pressure side of said bellows is exposed to pressure from said exhaust gases adjacent said power turbine and said low pressure side of said bellows is exposed to pressure from said exhaust gases after expansion and exterior of said outer shroud.

15. a power output module having a second tubular housing releasably secured with a first end thereof adjacent a second end of said case with the axis of said second housing aligned generally with the axis of said case, a power turbine generally extending outwardly from said first end of said second housing having second blades positioned to be in the path of exhaust gases exiting said gasifier turbine, output gear means, and a second shaft driven by said power turbine and driving said output gear means, said power output module including a power turbine shroud supported thereby and extending about said second blades in spaced relation therefrom;

5. first means extending inwardly within said case generally towards said combustor;

6. second means extending inwardly within said case generally towards said power turbine, said power turbine shroud extending towards said second extending means;

7. first slidable sealing means for slidably adjustably sealing said gasifier module adjacent said combustor to said first extending means; and

8. second slidable sealing means comprising a bellows fixedly attached at a first end thereof to a respective one of said power turbine shroud and said second extending means and a second annular seal fixedly attached to a second end of said bellows and slidably sealingly contacting a respective other of said power turbine shroud and second annular seal.

19. A modular gas turbine engine assembly, comprising:

1. a tubular case;

2. a gasifier module having a first tubular housing releasably secured with a first end thereof adjacent a first end of said case with the axis of said first housing aligned generally with axis of said case, a compressor generally within a second end of said first housing, a combustor generally extending outwardly from said first end of said first housing, and a first shaft extending from said compressor to adjacent said combustor, said gasifier module including a turbine nozzle vane assembly attached to direct flow of said exhaust gases from said combustor to said first blades of said gasifier turbine;

3. a gasifier turbine extending outwardly radially from said first shaft and having first blades positioned to be in the path of exhaust gases exiting said compressor to drive said first shaft and thereby drive said compressor, said gasifier module including a turbine nozzle vane assembly attached to direct flow of said exhaust gases from said combustor to said first blades of said gasifier turbine;

4. a power output module having a second tubular housing releasably secured with a first end thereof adjacent a second end of said case with the axis of said second housing aligned generally with the axis of said case, a power turbine generally extending outwardly from said first end of said second housing having second blades positioned to be in the path of exhaust gases exiting said gasifier turbine, output gear means, and a second shaft driven by said power turbine and driving said output gear means;

5. first means extending inwardly within said case generally towards said combustor;

6. second means extending inwardly within said case generally towards said power turbine;

7. first slidable sealing means extending between an outer ring of said turbine nozzle vane assembly and said first extending means for slidably adjustably sealing said gasifier module adjacent said combustor to said first extending means, said first slidable sealing means comprising a first bellows fixedly attached at a first end thereof to a respective one of said outer ring of said turbine nozzle vane assembly and said first extending means and a first annular seal fixedly attached to a second end of said first bellows and slidably sealingly contacting a respective other of said outer ring and said first annular seal; and

8. second slidable sealing means for sealing said power output module adjacent said power turbine to said second extending means.

20. A modular gas turbine engine assembly, comprising:

1. a tubular case;

2. a gasifier module having a first tublar housing releasably secured with a first end thereof adjacent a first end of said case with the axis of said first housing aligned generally with axis of said case, a compressor generally within a second end of said first housing, a combustor generally extending outwardly from said first end of said first housing, and a first shaft extending from said compressor to adjacent said combustor;

3. a gasifier turbine extending outwardly radially from said first shaft and having first blades positioned to be in the path of exhaust gases exiting said compressor to drive said first shaft and thereby drive said compressor, said gasifier module including a turbine nozzle vane assembly attached to direct flow of said exhaust gases from said combustor to said first blades of said gasifier turbine;

4. a power output module having a second tubular housing releasably secured with a first end thereof adjacent a second end of said case with the axis of said second housing aligned generally with the axis of said case, a power turbine generally extending outwardly from said first end of said second housing having second blades positioned to be in the path of exhaust gases exiting said gasifier turbine, output gear means, and a second shaft driven by said power turbine and driving said output gear means;

5. first means extending inwardly within said case generally towards said combustor;

6. second means extending inwardly within said case generally towards said power turbine;

7. first slidable sealing means extending between an outer ring of said turbine nozzle vane assembly and said first extending means for slidably adjustably sealing said gasifier module adjacent said combustor to said first extending means, said first slidable sealing means comprising a first annular mouth formed of a pair of annular rings joined and fixedly attached at a base thereof to a respective one of said outer ring of said turbine nozzle vane assembly and said first extending means and a first annular tongue for slidably fitting in said first annular mouth fixedly attached to a respective other of said outer ring and said first extending means; and

8. second slidable sealing means for sealing said power output module adjacent said power turbine to said second extending means.

24. An assembly as in claim 20, wherein said second annular fish mouth is fixedly attached to said second extending means and said second annular tongue is fixedly attached to said power turbine shroud.

29. An assembly as in claim 24, wherein said second shroud is fixedly attached to said power turbine shroud and said second ring seal is fixedly attached to said second extending means.

22. A modular gas turbine engine assembly, comprising:

1. a tubular case;

2. a gasifier module having a first tubular housing releasably secured with a first end thereof adjacent a first end of said case with the axis of said first housing aligned generally with the axis of said case, a compressor generally within a second end of said first housing, a combustor generally extending outwardly from said first end of said first housing, and a first shaft extending from said compressor to adjacent said combustor;

3. a gasifier turbine extending outwardly radially from said first shaft and having first blades positioned to be in the path of exhaust gases exiting said combustor to drive said first shaft and thereby drive said compressor;

26. An assembly as in claim 22, wherein said first shroud is fixedly attached to said outer ring and said first ring seal is fixedly attached to said first extending means.

23. a power output module having a second tubular housing releasably secured with a first end thereof adjacent a second end of said case with the axis of said second housing aligned generally with the axis of said case, a power turbine generally extending outwardly from said first end of said second housing having second blades positioned to be in the path of exhaust gases exiting said gasifier turbine, output gear means, and a second shaft driven by said power turbine and driving said output gear means, said power output module including a power turbine shroud supported thereby and extending about said second blades in spaced relation therefrom;

5. first means extending inwardly within said case generally towards said combustor;

6. second means extending inwardly within said case generally towards said power turbine said power turbine shroud extending towards said second extending means;

7. first slidable sealing means for slidably adjustably sealing said gasifier module adjacent said combustor to said first extending means;

8. second slidable sealing means extending between said power turbine shroud and said second extending means for sealing said power output module adjacent said power turbine to said second extending means;

9. said second slidable sealing means comprising a second annular mouth formed of a pair of annular rings joined and fixedly attached at a base thereof to a respective one of said power turbine shroud and said second extending means and a second annular tongue for slidably fitting in said second annular mouth fixedly attached to a perspective other of said power turbine shroud and said second extending means.

25. A modular gas turbine engine assembly, comprising:

1. a tubular case;

2. a gasifier module having a first tubular housing releasably secured with a first end thereof adjacent a first end of said case with the axis of said first housing aligned generally with the axis of said case, a compressor generally within a second end of said first housing, a combustor generally extending outwardly from said first end of said first housing, and a first shaft extending from said compressor to adjacent said combustor;

3. a gasifier turbine extending outwardly radially from said first shaft and having first blades positioned to be in the path of exhaust gases exiting said compressor to drive said first shaft and thereby drive said compressor, said gasifier module including a turbine nozzle vane assembly attached to direct flow of said exhaust gases from said combustor to said first blades of said gasifier turbine;

4. a power output module having a second tubular housing releasably secured with a first end thereof adjacent a second end of said case with the axis of said second housing aligned generally with the axis of said case, a power turbine generally extending outwardly from said first end of said second housing having second blades positioned to be in the path of exhaust gases exiting said gasifier turbine, output gear means, and a second shaft driven by said power turbine and driving said output gear means;

5. first means extending inwardly within said case generally towards said combustor;

6. second means extending inwardly within said case generally towards said power turbine;

7. first slidable sealing means comprising a first shroud fixedly attached to a respective one of said outer ring of said turbine nozzle vane assembly and said first extending means and a first ring seal for slidably fitting against a surface of said first shroud fixedly attached to a respective other of said outer ring and said first extending means for slidably adjustably sealing said gasifier module adjacent said combustor to said first extending means; and

8. second slidable sealing means for sealing said power output module adjacent said power turbine to said second extending means.

27. A modular gas turbine engine assembly, comprising:

1. a tubular case;

28. a gasifier modular having a first tubular housing releasably secured with a first end thereof adjacent a first end of said case with the axis of said first housing aligned generally with the axis of said case, a compressor generally within a second end of said first housing, a combustor generally extending outwardly from said first end of said first housing, and a first shaft extending from said compressor to adjacent said combustor;

3. a gasifier turbine extending outwardly radially from said first shaft and having first blades positioned to be in the path of exhaust gases exiting said combustor to drive said first shaft and thereby drive said compressor;

4. a power output module having a second tubular housing releasably secured with a first end thereof adjacent a second end of said case with the axis of said second housing aligned generally with the axis of said case, a power turbine generally extending upwardly from said first end of said second housing having second blades positioned to be in the path of exhaust gases exiting said gasifier turbine, output gear means, and a second shaft driven by said power turbine and driving said output gear means said power output module including a power turbine shroud supported thereby and extending about said second blades in spaced relation therefrom;

5. first means extending inwardly within said case generally towards said combustor;

6. second means extending inwardly within said case generally toward said power turbine;

7. first slidable sealing means for slidably adjustably sealing said gasifier module adjacent said combustor to said first extending means; and

8. second slidable sealing means extending between said power turbine shroud and said second extending means for sealing said power output module adjacent said power turbine to said second extending means, said second slidable sealing means comprising a shroud fixedly attached to a respective one of said power turbine shroud and said second extending means and a ring seal for slidably fitting against a surface of said shroud fixedly attached to a respective other of said power turbine shroud and said second extending means.