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특허 상세정보

At least one combustion apparatus and duct structure for a gas turbine engine

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F02C-003/00   
미국특허분류(USC) 060/039.37; 060/732; 060/733
출원번호 UP-0498479 (2006-08-03)
등록번호 US-7836677 (2011-01-22)
발명자 / 주소
출원인 / 주소
인용정보 피인용 횟수 : 9  인용 특허 : 15
초록

A combustion apparatus and duct structure for a gas turbine engine are provided. The combustion apparatus comprises a combustion system to receive fuel and air, ignite at least a portion of the fuel and air and output a stream of first combustion products and any remaining fuel and air. The combustion apparatus further comprises structure positioned adjacent to the combustion system for receiving and accelerating the first combustion products and any remaining fuel and air from the combustion system. The duct structure receives the first combustion produ...

대표
청구항

What is claimed is: 1. At least one combustion apparatus and duct structure for a gas turbine engine comprising: at least one combustion apparatus comprising: a combustion system that receives fuel and air, ignites at least a portion of the fuel and air, and outputs a stream of first combustion products and any remaining fuel and air; and nozzle structure positioned adjacent to said combustion system, said nozzle structure comprising: an inlet that receives the first combustion products and any remaining fuel and air from said combustion system; an outl...

이 특허에 인용된 특허 (15)

  1. Stokes Mitchell O.. Annular premix section for dry low-NO.sub.x combustors. USP2000076082111.
  2. Lovett Jeffery Allan ; Goebel Steven George. Dynamically uncoupled low NOx combustor having multiple premixers with axial staging. USP1999085943866.
  3. Lovett Jeffery Allan ; Goebel Steven George. Dynamically uncoupled low nox combustor with axial fuel staging in premixers. USP2000126164055.
  4. Bland, Robert; Gulati, Anil; Battaglioli, John. Flashback resistant pre-mix burner for a gas turbine combustor. USP2004096786047.
  5. de Chair Rory Somerset (St. Osyth\s Priory St. Osyth ; Essex EN). Gas generators. USP1976073971209.
  6. Anatoly Rakhmailov RU. Gas turbine engine. USP2002106460343.
  7. Bland, Robert; Ellis, Charles; Tiemann, Peter. Gas turbine with a compressor for air. USP2004016672070.
  8. Mansour,Adel B.; Benjamin,Michael A.. Macrolaminate direct injection nozzle. USP2006047021562.
  9. Mansour,Adel B.; Odar,Andrew M.; Steinthorsson,Erlendur. Macrolaminate radial injector. USP2006047028483.
  10. Paul, Brian Kevin; Peterson, Richard Budd; Terhaar, Tyson Jedd. Microlamination method for making devices. USP2004096793831.
  11. Beebe Kenneth W.. Premixing dry low NOx emissions combustor with lean direct injection of gas fuel. USP2000046047550.
  12. Carelli, Eric V.; Holm, Richard D.; Lippert, Thomas E.; Bachovchin, Dennis M.. Reheat combustor for gas combustion turbine. USP2003096619026.
  13. Benjamin Michael A. ; Mansour Adel B.. Stable pre-mixer for lean burn composition. USP2001116311473.
  14. Chamberlain John (Lake Park FL). Staged combustor having aerodynamically separated combustion zones. USP1982114356698.
  15. Waldherr Gregor Arthur ; Campbell Robert Patrick ; Correa Sanjay Marc ; Dean Anthony John. Steam cooled fuel injector for gas turbine. USP2001116311471.