Combustor and method for supplying fuel to a combustor
원문보기
IPC분류정보
국가/구분
United States(US) Patent
등록
국제특허분류(IPC7판)
F23N-001/00
F23R-003/28
출원번호
US-0294247
(2011-11-11)
등록번호
US-8894407
(2014-11-25)
발명자
/ 주소
Stoia, Lucas John
Melton, Patrick Benedict
출원인 / 주소
General Electric Company
대리인 / 주소
Dority & Manning, PA
인용정보
피인용 횟수 :
1인용 특허 :
24
초록▼
A combustor includes an end cap, a combustion chamber downstream from the end cap, and a plurality of tubes that extends through the end cap to provide fluid communication through the end cap to the combustion chamber. A casing surrounds the end cap, and a conduit extends from the casing to the end
A combustor includes an end cap, a combustion chamber downstream from the end cap, and a plurality of tubes that extends through the end cap to provide fluid communication through the end cap to the combustion chamber. A casing surrounds the end cap, and a conduit extends from the casing to the end cap. A duct extends around the conduit and inside the end cap to provide fluid communication to the end cap. A method for supplying fuel to a combustor includes flowing a working fluid through a plurality of tubes that extends axially through an end cap, supplying a first fluid through a conduit into the end cap, and supplying a second fluid through a duct spiraling around the conduit into the end cap.
대표청구항▼
1. A combustor, comprising: an end cover coupled to one end of a casing, the casing at least partially surrounding the combustor housing;an end cap assembly that extends radially and circumferentially within the casing with respect to an axial centerline of the combustor, the end cap assembly includ
1. A combustor, comprising: an end cover coupled to one end of a casing, the casing at least partially surrounding the combustor housing;an end cap assembly that extends radially and circumferentially within the casing with respect to an axial centerline of the combustor, the end cap assembly including an upstream plate, a downstream plate, a circumferentially extending cap shield that extends axially therebetween, a fuel plenum defined within the end cap assembly and a tube bundle, the tube bundle comprising a plurality of tubes that provide for fluid communication through the upstream surface, the fuel plenum and the downstream surface;a first fuel conduit that extends from the end cover and through the fuel plenum of the end cap; anda fuel duct external to the conduit that spirals around and makes contact with the conduit for heat exchange, the conduit between the end cover and the upstream surface, wherein the duct extends through the upstream surface and provides for fluid communication between the end cover and the fuel plenum; anda barrier that extends radially inside the end cap assembly with respect to an axial centerline of the end cap assembly to at least partially define the fuel plenum, wherein the barrier axially separates the fuel plenum from a diluent plenum, where the fuel plenum is upstream of the diluent plenum, defined inside the end cap assembly with respect to the axial centerline of the combustor,wherein the conduit extends inside the diluent plenum to provide fluid communication to the diluent plenum. 2. The combustor as in claim 1, further comprising one or more fuel ports through the plurality of tubes, wherein the one or more fuel ports provide fluid communication from the fuel plenum into the plurality of tubes. 3. The combustor as in claim 1, wherein the end cap assembly includes a plurality of tube bundles, the end cap assembly further comprising a divider that extends axially through the end cap assembly with respect to an axial centerline of the end cap assembly to separate adjacent tube bundles of the plurality of tube bundles. 4. The combustor as in claim 1, further comprising a fuel nozzle that extends from the end cover axially into the end cap assembly with respect to the axial centerline of the end cap assembly. 5. A method for supplying fuel to a combustor, comprising: Providing a combustor, the combustor having:an end cover coupled to one end of a casing, the casing at least partially surrounding the combustor housing;an end cap assembly that extends radially and circumferentially within the casing with respect to an axial centerline of the combustor, the end cap assembly including an upstream plate, a downstream plate, a circumferentially extending cap shield that extends axially therebetween, a fuel plenum defined within the end cap assembly and a tube bundle, the tube bundle comprising a plurality of tubes that provide for fluid communication through the upstream surface, the fuel plenum and the downstream surface;a first fuel conduit that extends from the end cover and through the fuel plenum of the end cap; anda fuel duct external to the conduit that spirals around and makes contact with the conduit for heat exchange, the conduit between the end cover and the upstream surface, wherein the duct extends through the upstream surface and provides for fluid communication between the end cover and the fuel plenum; anda barrier that extends radially inside the end cap assembly with respect to an axial centerline of the end cap assembly to at least partially define the fuel plenum, wherein the barrier axially separates the fuel plenum from a diluent plenum, where the fuel plenum is upstream of the diluent plenum, defined inside the end cap assembly with respect to the axial centerline of the combustor,wherein the conduit extends inside the diluent plenum to provide fluid communication to the diluent plenum, andflowing a working fluid through a plurality of tubes that extends axially through the end cap assembly, andsupplying a fuel into the fuel plenum defined within the end cap assembly via the fuel duct that spirals around an outer surface of the conduit. 6. The method as in claim 5, further comprising supplying a fluid to a diluent plenum defined inside the end cap assembly. 7. The method as in claim 6, further comprising separating the fluid from the fuel inside the end cap assembly. 8. The method as in claim 5, further comprising mixing a fluid with the fuel inside the end cap assembly.
연구과제 타임라인
LOADING...
LOADING...
LOADING...
LOADING...
LOADING...
이 특허에 인용된 특허 (24)
Fujimura Hidekazu (Mito JPX) Koyama Kazuhito (Hitachi JPX) Nakamura Shozo (Hitachioota JPX) Moritomo Yoshikazu (Hitachi JPX), Apparatus and method for mixing gaseous fuel and air for combustion including injection at a reverse flow bend.
Fraas Lewis M. (Issaquah WA), Cylindrical electric power generator using low bandgap thermophotovolatic cells and a regenerative hydrocarbon gas burne.
Vandervort, Christian L.; Bourgeois, Richard S., Fuel system configuration and method for staging fuel for gas turbines utilizing both gaseous and liquid fuels.
Ansart Denis R. H. (Bois Le Roi FRX) Desaulty Michel A. A. (Vert Saint Denis FRX) Sandelis Denis J. M. (Nangis FRX), Fuel/oxidizer premixing combustion chamber.
Oblnder Kurt (Kernen DEX) Fricker Ludwig (Stuttgart DEX) Anderson Alexander (Stuttgart DEX) Weining Hans-Karl (Esslingen DEX) Geldec Selcuk (Talheim DEX) Krukenberg Ralf (Aichwald DEX) Fingerle Gerha, Mixture-compressing internal-combustion engine with secondary-air injection and with air-mass metering in the suction pi.
Ansart Denis R. H. (Bois le Roi FRX) Commaret Patrice A. (Maincy FRX) David Etienne S. R. (Bois le Roi FRX) Desaulty Michel A. A. (Vert Saint Denis FRX) Quinquenneau Bruno M. M. (Massy FRX) Sandelis , Pre-mixing injection system for a turbojet engine.
Joshi Mahendra L. ; Borders Harley A. ; Marin Ovidiu ; Charon Olivier, Self-cooled oxygen-fuel burner for use in high-temperature and high-particulate furnaces.
Richard Sterling Tuthill ; William Theodore Bechtel, II ; Jeffrey Arthur Benoit ; Stephen Hugh Black ; Robert James Bland ; Guy Wayne DeLeonardo ; Stefan Martin Meyer ; Joseph Charles Taura ;, Swozzle based burner tube premixer including inlet air conditioner for low emissions combustion.
※ AI-Helper는 부적절한 답변을 할 수 있습니다.