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Combustor tuning 원문보기

IPC분류정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판)
  • F02C-009/00
출원번호 US-0250912 (1999-02-16)
발명자 / 주소
  • Dean Anthony John
출원인 / 주소
  • General Electric Company
대리인 / 주소
    Patnode
인용정보 피인용 횟수 : 16  인용 특허 : 15

초록

A variable length pre-mixer assembly comprises an upstream end for receiving compressed air from a compressor and a downstream end disposed in flow communication with a combustor. Pre-mixer assembly comprises an upstream forward clamp, a swirler assembly having a plurality of circumferentially space

대표청구항

[ What is claimed is:] [2.]2. An industrial turbine engine comprising:a variable length pre-mixer assembly comprising an upstream end for receiving compressed air from a compressor and a downstream end disposed in flow communication with a combustor, said pre-mixer assembly comprising:an upstream fo

이 특허에 인용된 특허 (15)

  1. Pandalai Raghavan P. (Cincinnati OH) Carter Bruce A. (West Chester OH) Hehmann Horst W. W. (Cincinnati OH), Acoustic damper for a gas turbine engine combustor.
  2. Acton Elizabeth (Cambridge GB2) Cargill Alexander M. (Derby GB2) Ross Colin F. (Cambridge GB2) Eatwell Graham P. (Cambridge GB2), Active control of unsteady motion phenomena in turbomachinery.
  3. Acton Elizabeth (Cambridge GB2) Cargill Alexander M. (Derby GB2) Ross Colin F. (Cambridge GB2) Eatwell Graham P. (Cambridge GB2), Active control of unsteady motion phenomena in turbomachinery.
  4. Acton Elizabeth (Cambridge GB2) Cargill Alexander M. (Derby GB2) Ross Colin F. (Cambridge GB2) Eatwell Graham P. (Cambridge GB2), Active control of unsteady motion phenomena in turbomachinery.
  5. Acton Elizabeth (Cambridge GB2) Cargill Alexander M. (Derby GB2) Ross Colin F. (Cambridge GB2) Eatwell Graham P. (Cambridge GB2), Active control of unsteady motion phenomena in turbomachinery.
  6. Nakae Tomoyoshi,JPX, Annular type gas turbine combustor.
  7. Black Stephen H. (Duanesburg NY), Apparatus for reducing fuel/air concentration oscillations in gas turbine combustors.
  8. Zarzalis Nikolaos (Dachau DEX) Joos Franz (MDEX), Burner for gas turbine engines.
  9. Zarzalis Nikolaos (Dachau DEX) Joos Franz (Munich DEX), Burner for gas turbine engines with axially adjustable swirler.
  10. Richards George A. ; Gemmen Randall S., Combustor oscillation attenuation via the control of fuel-supply line dynamics.
  11. Lovett Jeffery Allan ; Goebel Steven George, Dynamically uncoupled low NOx combustor having multiple premixers with axial staging.
  12. Mongia Hukam C. (Tempe AZ) Coleman Edwin B. (Tempe AZ) Bruce Thomas W. (Pheonix AZ), Gas turbine engine variable geometry combustor apparatus.
  13. Dean Anthony John, Low emissions combustor premixer.
  14. Wilson Kenneth (1213 Flora Way Ridgecrest CA 93555) Schadow Klaus (100 W. Sydnor Ridgecrest CA 93555) Smith Robert (315 Rancho Ridgecrest CA 93555) Gutmark Ephraim (602 Rio Bravo Ridgecrest CA 93555), Method and apparatus for active control of combustion devices.
  15. Overton Dennis L. (Bristol GB3), Variable geometry air-fuel injector.

이 특허를 인용한 특허 (16)

  1. McManus, Keith; Sanderson, Simon; Goldmeer, Jeffrey, Acoustic impedance-matched fuel nozzle device and tunable fuel injection resonator assembly.
  2. Mendoza, Robert Eleazar; Morrison, Paul Elliot; Leon, Marco Ezra; Bognuda, Tiziano Marco; Ito, Satoshi; Turner, legal representative, Shari, Active combustion control for a turbine engine.
  3. Alkabie,Hisham, Aerodynamic trip for a combustion system.
  4. Popovic, Predrag; Kraemer, Gilbert Otto; Ross, William Thomas; Belvaev, Vladimir, Fuel nozzle and method for operating a combustor.
  5. Bailey, Donald Mark; Simmons, Scott R.; Huffman, Marcus B., Fuel nozzle assembly for a gas turbine engine.
  6. Popovic, Predrag; Baruah, Abinash; Kraemer, Gilbert Otto; Ross, William Thomas, Gas turbine combustor having a fuel nozzle for flame anchoring.
  7. Burrus, David Louis; Joshi, Narendra Digamber; Haynes, Joel Meier; Feitelberg, Alan S., Gas turbine engine combustor can with trapped vortex cavity.
  8. Haynes, Joel Meier; Feitelberg, Alan S.; Burrus, David Louis; Joshi, Narendra Digamber, Gas turbine engine combustor can with trapped vortex cavity.
  9. Savary, Nicolas; Berat, Claude; Vignau, Hubert Hippolyte; Viguier, Christophe Nicolas Henri, Method for injecting fuel into a combustion chamber of a gas turbine, and injection system for implementing same.
  10. McMahan, Kevin Weston; Hadley, Mark Allan; Myers, Geoffrey D.; Draper, Sam D., Methods and systems for inducing combustion dynamics.
  11. Oskooei, Saeid, Nozzle design to reduce fretting.
  12. Oskooei, Saeid, Nozzle design to reduce fretting.
  13. Oskooei, Saeid; Hope, Nicholas, Nozzle repair to reduce fretting.
  14. Draper, Samuel David, System and method for exhaust gas use in gas turbine engines.
  15. Davis, Jr., Lewis Berkley; Citeno, Joseph Vincent; Johnson, Thomas Edward; Ziminsky, Willy Steve, Traversing fuel nozzles in cap-less combustor assembly.
  16. Scarinci, Thomas, Two-branch mixing passage and method to control combustor pulsations.
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