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... |
Citations|
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Referenced by|
| US5682747 | Apr 10, 1996 | Nov 4, 1997 | General Electric Company | Gas turbine combustor heat shield of casted super alloy | | US6298667 | Jun 22, 2000 | Oct 9, 2001 | General Electric Company | Modular combustor dome | | US6358041 | Apr 21, 2000 | Mar 19, 2002 | Eastman Chemical Company | Threaded heat shield for burner nozzle face | | US6442940 | Apr 27, 2001 | Sep 3, 2002 | General Electric Company | Gas-turbine air-swirler attached to dome and combustor in single brazing operation | | US6546733 | Jun 28, 2001 | Apr 15, 2003 | General Electric Company | Methods and systems for cooling gas turbine engine combustors | | US6557349 | Apr 17, 2000 | May 6, 2003 | General Electric Company | Method and apparatus for increasing heat transfer from combustors | | US6655027 | Jan 15, 2002 | Dec 2, 2003 | General Electric Company | Methods for assembling gas turbine engine combustors | | US6758045 | Aug 30, 2002 | Jul 6, 2004 | General Electric Company | Methods and apparatus for operating gas turbine engines | | US6904676 | Dec 4, 2002 | Jun 14, 2005 | General Electric Company | Methods for replacing a portion of a combustor liner | | US6932093 | Feb 24, 2003 | Aug 23, 2005 | General Electric Company | Methods and apparatus for washing gas turbine engine combustors | | US6983605 | Apr 7, 2000 | Jan 10, 2006 | General Electric Company | Methods and apparatus for reducing gas turbine engine emissions | | US6986253 | Jul 16, 2003 | Jan 17, 2006 | General Electric Company | Methods and apparatus for cooling gas turbine engine combustors | | US7065955 | Jun 18, 2003 | Jun 27, 2006 | General Electric Company | Methods and apparatus for injecting cleaning fluids into combustors | | US7140560 | Sep 24, 2004 | Nov 28, 2006 | Parker-Hannifin Corporation | Nozzle assembly with fuel tube deflector | | US7596949 | Feb 23, 2006 | Oct 6, 2009 | General Electric Company | Method and apparatus for heat shielding gas turbine engines | | US7617689 | Mar 2, 2006 | Nov 17, 2009 | Honeywell International Inc. | Combustor dome assembly including retaining ring | | US7762070 | May 11, 2006 | Jul 27, 2010 | Siemens Energy, Inc. | Pilot nozzle heat shield having internal turbulators | | US7765809 | Nov 10, 2006 | Aug 3, 2010 | General Electric Company | Combustor dome and methods of assembling such | | US7856826 | Nov 10, 2006 | Dec 28, 2010 | General Electric Company | Combustor dome mixer retaining means | | US8033113 | May 15, 2007 | Oct 11, 2011 | Pratt & Whitney Canada Corp. | Fuel injection system for a gas turbine engine | | US8122727 | Nov 5, 2009 | Feb 28, 2012 | United Technologies Corporation | Compliant metal support for ceramic combustor liner in a gas turbine engine |
Claims1. 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. |