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A dome assembly for a multiple annular combustor is disclosed as including an annular dome plate having at least two radial domes, wherein each of the radial domes include a plurality of circumferentially spaced openings therein. A heat shield is positioned within each of the openings, with a threaded forward end located upstream of the dome plate and an aft end located downstream of the dome plate. A retainer nut with threads formed on an annular surface thereof is matingly engagable with the forward end of each heat shield. When the retainer nut is tightened onto the heat shield forward end, the heat shield is mechanically attached to the dome plate. Preferably, at least one centerbody extends axially downstream from either the radially outer or inner side of the aft end. The dome assembly includes a ferrule within each of the dome plate openings for receiving an air/fuel mixer therein, the ferrule having an annular sealing flange extending radially therefrom. A retaining ring is...

InventorsJan C. Schilling, Edward C. Vickers
Original AssigneeGeneral Electric Company
Primary Examiner: Ted Kim
Current U.S. Classification60/747; 60/756; 60/800
International Classification: F02C 100

View patent at USPTO
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Citations

Cited PatentFiling dateIssue dateOriginal AssigneeTitle
US3901446May 9, 19741975INDUCED VORTEX SWIRLER
US4162611Jul 5, 1977Jul 31, 1979Societe Nationale d'Etude et de Construction de Moteurs d'AviationCombustion chamber for turbo engines
US4870818Apr 18, 1986Oct 3, 1989United Technologies CorporationFuel nozzle guide structure and retainer for a gas turbine engine
US4914918Sep 26, 1988Apr 10, 1990United Technologies CorporationCombustor segmented deflector
US4934145Oct 12, 1988Jun 19, 1990United Technologies CorporationCombustor bulkhead heat shield assembly
US5197289Nov 26, 1990Mar 30, 1993General Electric CompanyDouble dome combustor
US5220795Apr 16, 1991Jun 22, 1993General Electric CompanyMethod and apparatus for injecting dilution air
US5285632Feb 8, 1993Feb 15, 1994General Electric CompanyLow NO.sub.x combustor
US5323604Nov 16, 1992Jun 28, 1994General Electric CompanyTriple annular combustor for gas turbine engine
US5479772Dec 16, 1993Jan 2, 1996General Electric CompanyFilm cooling starter geometry for combustor liners

Referenced by

Citing PatentFiling dateIssue dateOriginal AssigneeTitle
US5682747Apr 10, 1996Nov 4, 1997General Electric CompanyGas turbine combustor heat shield of casted super alloy
US6298667Jun 22, 2000Oct 9, 2001General Electric CompanyModular combustor dome
US6358041Apr 21, 2000Mar 19, 2002Eastman Chemical CompanyThreaded heat shield for burner nozzle face
US6442940Apr 27, 2001Sep 3, 2002General Electric CompanyGas-turbine air-swirler attached to dome and combustor in single brazing operation
US6546733Jun 28, 2001Apr 15, 2003General Electric CompanyMethods and systems for cooling gas turbine engine combustors
US6557349Apr 17, 2000May 6, 2003General Electric CompanyMethod and apparatus for increasing heat transfer from combustors
US6655027Jan 15, 2002Dec 2, 2003General Electric CompanyMethods for assembling gas turbine engine combustors
US6758045Aug 30, 2002Jul 6, 2004General Electric CompanyMethods and apparatus for operating gas turbine engines
US6904676Dec 4, 2002Jun 14, 2005General Electric CompanyMethods for replacing a portion of a combustor liner
US6932093Feb 24, 2003Aug 23, 2005General Electric CompanyMethods and apparatus for washing gas turbine engine combustors
US6983605Apr 7, 2000Jan 10, 2006General Electric CompanyMethods and apparatus for reducing gas turbine engine emissions
US6986253Jul 16, 2003Jan 17, 2006General Electric CompanyMethods and apparatus for cooling gas turbine engine combustors
US7065955Jun 18, 2003Jun 27, 2006General Electric CompanyMethods and apparatus for injecting cleaning fluids into combustors
US7140560Sep 24, 2004Nov 28, 2006Parker-Hannifin CorporationNozzle assembly with fuel tube deflector
US7596949Feb 23, 2006Oct 6, 2009General Electric CompanyMethod and apparatus for heat shielding gas turbine engines
US7617689Mar 2, 2006Nov 17, 2009Honeywell International Inc.Combustor dome assembly including retaining ring
US7762070May 11, 2006Jul 27, 2010Siemens Energy, Inc.Pilot nozzle heat shield having internal turbulators
US7765809Nov 10, 2006Aug 3, 2010General Electric CompanyCombustor dome and methods of assembling such
US7856826Nov 10, 2006Dec 28, 2010General Electric CompanyCombustor dome mixer retaining means
US8033113May 15, 2007Oct 11, 2011Pratt & Whitney Canada Corp.Fuel injection system for a gas turbine engine
US8122727Nov 5, 2009Feb 28, 2012United Technologies CorporationCompliant metal support for ceramic combustor liner in a gas turbine engine

Claims

1. A dome assembly for a multiple annular combustor, comprising

(a) an annular dome plate having at least two radial domes, each of said radial domes including a plurality of circumferential openings therein;
(b) a heat shield positioned within each of said openings, said heat shield having a forward end located upstream of said dome plate and an aft end located downstream of said dome plate, wherein said forward end of said heat shield has threads formed thereon; and
(c) a retainer nut having an inner annular surface with threads formed thereon, said retainer nut threads being matingly engagable with said heat shield threads;

wherein said heat shield is mechanically attached to said dome plate by said retainer nut.

2. The dome assembly of claim 1, further comprising:

(a) an annular flange extending radially outward from said heat shield, said flange being located downstream of said threaded forward end; and
(b) an annular groove formed in an inner annular surface defining said dome plate opening;

wherein said heat shield flange rests within said groove and causes said heat shield to be drawn to a desired fit with said dome plate as said retainer nut is tightened on said heat shield forward end.

3. The dome assembly of claim 2, said heat shield further comprising a hollow centerbody extending axially downstream from one of a radially inner and outer side of said aft end.

4. The dome assembly of claim 3, further comprising cooling passages formed in said retaining nut and said heat shield flange, wherein air flowing to said dome plate is able to flow through said cooling passages and communicate with the interior of said centerbody.

5. The dome assembly of claim 3, said centerbody further comprising a non-linear wall including a first portion extending radially from said heat shield aft end, a second portion extending axially downstream away from said dome plate, a third portion again extending radially from said second portion, and a fourth portion extending axially upstream terminating adjacent said dome plate.

6. The dome assembly of claim 5, further comprising a notch in an upstream surface of said centerbody fourth portion adjacent said dome plate and a seal therebetween.

7. The dome assembly of claim 6, wherein a predetermined gap between said dome plate and said centerbody fourth portion is provided to prevent crushing of said seal.

8. The dome assembly of claim 5, further comprising:

(a) a flange extending radially from said centerbody fourth portion with a notch therein; and
(b) a pin inserted through said flange notch into said dome plate;

wherein said centerbody is prevented from rotating due to torque loads.

9. The dome assembly of claim 1, wherein said heat shield forward end is annular.

10. The dome assembly of claim 1, wherein said heat shield aft end is substantially square.

11. The dome assembly of claim 1, said heat shield further comprising a centerbody extending axially downstream from a radially outer side of said aft end.

12. The dome assembly of claim 11, said heat shield further comprising a centerbody extending axially downstream from a radially inner side of said aft end.

13. The dome assembly of claim 1, said heat shield further comprising a centerbody extending axially downstream from a radially inner side of said aft end.

14. The dome assembly of claim 1, further comprising:

(a) a ferrule within said dome plate opening for receiving an air/fuel mixer therein, said ferrule having an annular sealing flange extending radially therefrom; and
(b) a retaining ring positioned upstream of said heat shield forward end to provide a gap therebetween;

wherein said ferrule sealing flange is positioned within said gap so that said ferrule is permitted to move circumferentially and radially therein.

15. The dome assembly of claim 1, said retainer nut further comprising a plurality of lugs and slots at a forward end thereof.

16. A dome assembly for a triple annular combustor of a gas turbine engine, comprising:

(a) an annular dome plate having an outer dome, a middle dome, and an inner dome, each of said domes having a plurality of circumferentially spaced openings therein;
(b) an outer heat shield positioned within each of said outer dome openings;
(c) a middle heat shield positioned within each of said middle dome openings; and
(d) an inner heat shield positioned within each of said inner dome openings;

wherein said outer, middle, and inner heat shields each have a threaded forward end located upstream of said dome plate and an aft end located downstream of said dome plate;
(e) an outer retainer nut threadingly engaged with each of said outer heat shield forward ends;
(f) a middle retainer nut threadingly engaged with each of said middle heat shield forward ends; and
(g) an inner retainer nut threadingly engaged with each of said inner heat shield forward ends; wherein said outer, middle, and inner heat shields are mechanically attached to said dome plate by said outer, middle, and inner retaining nuts.

17. The dome assembly of claim 16, further comprising:

(a) an outer, middle, and inner ferrule within each of said outer, middle, and inner dome openings, respectively, for receiving air/fuel mixers therein, said outer, middle and inner ferrules each having an annular sealing flange extending radially therefrom; and
(b) a retaining ring positioned upstream of each of said outer, middle and inner heat shield forward ends to provide a gap between said retaining rings and said heat shields;

wherein said ferrule flanges are positioned within said gaps so that said outer, middle and inner ferrules are permitted to move circumferentially and radially therein.

18. The dome assembly of claim 17, wherein said ferrule flanges of said outer, middle, and inner ferrules are located at varying axial positions.

19. The dome assembly of claim 18, wherein said outer, middle, and inner heat shields have forward threaded ends of varying axial length and said retainer nuts are of corresponding axial length.

20. The dome assembly of claim 16, said triple annular combustor including an outer liner affixed to a radially outer end of said dome plate and an inner liner affixed to a radially inner end of said dome plate, wherein said outer heat shields include a centerbody extending axially downstream from an outer radial side thereof to insulate said outer liner, said inner heat shields include a centerbody extending axially downstream from an inner radial side thereof to insulate said inner liner, and said middle heat shields include a first centerbody extending axially downstream from an outer radial side thereof to separate said outer and middle domes and a second centerbody extending axially downstream from an inner radial side thereof to separate said middle and inner domes.