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High pressure inlet bleed heat system for the compressor of a turbine 원문보기

IPC분류정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판)
  • F04D-003/00
출원번호 US-0085910 (1998-05-27)
발명자 / 주소
  • Arar Malath Ibrahim
  • Kemp Timothy Robert
  • Hubschmitt George Raymond
  • DeAngelis David Anthony
  • Eignor James Giles
출원인 / 주소
  • General Electric Co.
대리인 / 주소
    Nixon & Vanderhye
인용정보 피인용 횟수 : 32  인용 특허 : 3

초록

The high pressure inlet bleed heat system includes a plurality of tubes which receive heated compressed air from the compressor extraction discharge manifold. The tubes extend into the inlet duct of the compressor, are uniformly spaced one from the other and have a uniform distribution of laterally

대표청구항

[ What is claimed is:] [1.] An inlet bleed heat system for the compressor of a turbine, comprising:an air inlet duct for delivering ambient air along a flow path to the compressor;a plurality of tubes, generally parallel to one another in the flow path of said air inlet duct and distributed substant

이 특허에 인용된 특허 (3)

  1. Anderson Rodger O. (Scotia NY) Burrow Julian D. (Ballston Lake NY) Vandervort Christian L. (Voorheesville NY), Gas turbine inlet heating system using jet blower.
  2. Cummins ; Jr. James R. (Ballston Lake NY), Heat recovery anti-icing system.
  3. Napier James C. (San Diego CA) Thompson Robert G. (San Diego CA), Turbine inlet silencer.

이 특허를 인용한 특허 (32)

  1. Kraft, Robert J., Aero boost—gas turbine energy supplementing systems and efficient inlet cooling and heating, and methods of making and using the same.
  2. Kraft, Robert J., Aero boost—gas turbine energy supplementing systems and efficient inlet cooling and heating, and methods of making and using the same.
  3. Miranda, Carlos Miguel; Beadie, Douglas Frank, Apparatus and method for testing a compressor.
  4. Martin,Nicholas Francis; Cencula,James Edward, Bolt-on radial bleed manifold.
  5. Kraft, Robert J., Compressed air injection system method and apparatus for gas turbine engines.
  6. Flanagan, Mark W.; Tillery, Steven W., Compressor clearance control system using bearing oil waste heat.
  7. Tillery, Steven W.; Flanagan, Mark W.; Snider, David A., Compressor clearance control system using turbine exhaust.
  8. Tillery, Steven William; Snider, David August, Compressor start bleed system for a turbine system and method of controlling a compressor start bleed system.
  9. Ekanayake, Sanji; Scipio, Alston Ilford; Mestroni, Julio Enrique; Rehg, Timothy Joseph, Compressor wash system with spheroids.
  10. Betti, Tommaso; Baldassarre, Antonio; Viti, Filippo; Meucci, Stefano; Lazzeri, Marco; Merlo, Roberto; Marcucci, Daniele, Device and method for gas turbine unlocking.
  11. Guidati, Gianfranco Ludovico, Energy storage system and method for energy storage.
  12. Kraft, Robert J.; Auerbach, Scott, Gas turbine air injection system control and method of operation.
  13. Mazumder, Indrajit; Saha, Rajarshi; Gulen, Seyfettin Can; Devarajan, Sabarinath; Kumar, Prashant, Gas turbine anti-icing system.
  14. Sandberg,Peter; Ekberg,Tord; Johansson,Peter, Gas turbine arrangement having an integrated filter housing and compressor bleed duct.
  15. Arar, Malath Ibrahim; Anllo, Anna Valeria, Gas turbine inlet heating system.
  16. Mullen, Michael Corey; Morgan, Rex Allen, Gas turbine inlet system and method.
  17. Zhang, Jianmin; Hu, Tailai; Kippel, Bradly Aaron, Gas turbine power augmentation system.
  18. Scimone, Michael J., Heated screen for air intake of aircraft engines.
  19. Hart, Andrew Clifford; Desai, Tushar Sharadchandra; Dimmick, III, John Herbert; Forcier, Matthew Paul; Han, Chunlian; Smith, Charles Alexander, Impeller tube assembly.
  20. So, Peter; Sewell, Jesse; Adams, Donald, Inlet bleed heat and power augmentation for a gas turbine engine.
  21. Merchant, Laxmikant; Avishetti, Srinivas; Ponyavin, Valery Ivanovich; Byrd, Doug, Inlet bleed heat system and related method for a compact gas turbine inlet.
  22. Tillery, Steven William, Inlet bleed heat system thermal lag mitigation using compressor interstage bleeds.
  23. Hao, Yongjiang; Byrd, Douglas Scott; Zhang, Hua; Kippel, Bradly Aaron; Zhang, Jianmin, Inlet bleed heat system with integrated air knife/silencer panels.
  24. Poccia, Nicholas Philip; Kenny, III, Laurence Ambrose; Westphal, Karl Kurt Rocco; Balasubramanyam, Diwakar; Carberg, William George, Inlet bleed heater for heating inlet air to a compressor and methods of fabricating and transporting the heater.
  25. Roth, Bryce Alexander, Operating line control of a compression system with flow recirculation.
  26. Feher, Peter; Motakef, Abbas, System and method for changing the efficiency of a combustion turbine.
  27. Velez, Tomas Antonio, System and method for recirculating and recovering energy from compressor discharge bleed air.
  28. Chillar, Rahul Jaikaran; Upadhyay, Siddharth Girishkumar, System for heating an airstream by recirculating waste heat of a turbomachine.
  29. Ekanayake, Sanji; Scipio, Alston Ilford; Klosinski, Joseph; Semel, Pierre Antoine, Systems and methods for utilizing gas turbine compartment ventilation discharge air.
  30. Erickson, Donald Charles; Anand, Gopalakrishnan, Thermally powered turbine inlet air chiller heater.
  31. Kumar, Prashant; Devarajan, Sabarinath; Thiruvettipuram Madhivanan, Vivekanandhan; Mazumder, Indrajit; Puri, Hemant; Pushkaran, Chandrasekhar; Saha, Rajarshi, Turbomachine inlet bleed heating assembly.
  32. Vega, Santiago; Ellis, Charlie; Kastelic, Roger; Leahy, James; Raguraman, Janak, Utilizing inlet bleed heat to improve mixing and engine turndown.
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