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Compressor endwall bleed system 원문보기

IPC분류정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판)
  • F04D-029/70
출원번호 US-0527438 (2000-03-16)
발명자 / 주소
  • Robert A. Ress, Jr.
  • Jeffrey L. Hansen
출원인 / 주소
  • Allison Advanced Development Company
대리인 / 주소
    Woodard, Emhardt, Naughton, Moriarty & McNett
인용정보 피인용 횟수 : 18  인용 특허 : 19

초록

A compression system endwall bleed system having a plurality of bleed slots formed in a mechanical housing downstream of a rotating shrouded rotor. In one embodiment, the plurality of bleed slots bleed off a separated tip boundary layer to relieve back pressure associated with this blockage. A seali

대표청구항

1. A compression system, comprising:a mechanical housing; a wheel rotatable within said housing, said wheel having a plurality of blades coupled thereto; a shroud coupled to said plurality of blades so as to separate fluid flow within the compression system into a core stream and a bypass stream, sa

이 특허에 인용된 특허 (19)

  1. Meindl Thomas (Nussbaumen CHX) Meylan Pierre (Neuenhof CHX) Zierer Thomas (Wettingen CHX), Appliance for extracting secondary air from an axial compressor.
  2. Roberts William B. (Fremont CA), Area ruled fan blade ends for turbofan jet engine.
  3. Vincent de Paul Michel (Senlis FRX) Detanne Francois (Paris FRX), Blade array for turbomachines comprising suction ports in the inner and/or outer wall and turbomachines comprising same.
  4. Bobo Melvin (Cincinnati OH), Bleed air manifold.
  5. McCaughan John A. I.,GB5, Boundary layer control in aerodynamic low drag structures.
  6. Khalid Syed J. (Palm Beach Gardens FL), Compressor endwall treatment.
  7. Kerrebrock Jack L. ; Epstein Alan H., Counter-rotating compressors with control of boundary layers by fluid removal.
  8. Yasugahira Norio (Hitachi JPX) Sato Takeshi (Hitachi JPX) Tsubouchi Kuniyoshi (Hitachi JPX), Diaphragms for axial flow fluid machines.
  9. Nolcheff Nick A. (Palm Beach Gardens FL), Flow aligned plenum endwall treatment for compressor blades.
  10. McGreehan William F. (West Chester OH) Fintel Bradley W. (Fairfield OH) Lammas Andrew J. (Maineville OH), High pressure compressor flowpath bleed valve extraction slot.
  11. Blessing William D. (Brookeville IN) Stickles Richard W. (Cincinnati OH), Hoop shroud for the low pressure stage of a compressor.
  12. Cuthbertson Robert D. (Kirkland WA) Schaut Larry A. (Seattle WA), Inlet guide vane bleed system.
  13. Andre Pierre A. (Paris FRX) Thevenin Jean-Claude P. H. P. (Saint.-Maur-des-Fosses FRX) Girault Jean-Pierre Y. B. (Dammarie les Lys FRX) Richter Gerhard (Boissise le Roi FRX), Method and device for reducing the noise of turbo-machines.
  14. Wisser Gerhard (Grubweg 11 7745 Schonach DEX), Rotor or guide wheel of a turbine engine with shroud ring.
  15. Riollet Gilbert (Paris FRX) Bessay Raymond (Belfort FRX), Set of blades for a turbine.
  16. Riollet Gilbert (Paris FRX) Bessay Raymond (Belfort FRX), Set of blades for a turbine and a turbine which includes such a set of blades.
  17. Pierpoline Mario F. (Media PA), Steam turbine extraction system.
  18. Meauze Georges D. (Paris FR) Thibert Jean-Jacques (Verrieres-le-Buisson FR) Leynaert Jacky R. (Igny FR), Supersonic compressors.
  19. Braddy Bruce T. (Burlington MA) Eldrid Sacheveral Q. (Stoneham MA), Turbine blade with tip vent.

이 특허를 인용한 특허 (18)

  1. Hammar, John; Cheng, Po Lun; Li, Min, Centrifugal pump.
  2. Duong, Hien; Nichols, Jason; Townsend, Peter; Kandasamy, Vijay, Compressor bleed self-recirculating system.
  3. Nichols, Jason; Townsend, Peter; Duong, Hien; Kandasamy, Vijay, Compressor shroud reverse bleed holes.
  4. Pichel, Sacha, Cooling device for a jet engine.
  5. King, Jonathan M; Bolgar, Crispin D; Snowsill, Guy D, Gas turbine engine havinga rotatable off-take passage in a compressor section.
  6. Cloft, Thomas G.; Wiley, Richard H., Integral suction device with acoustic panel.
  7. Cloft, Thomas G.; Wiley, Richard H., Integral suction device with acoustic panel.
  8. Lardellier, Alain, Method for air circulation in a turbomachine compressor, compressor arrangement using this method, compression stage and compressor incorporating such a arrangement, and aircraft engine equipped with such a compressor.
  9. Martel, Alain C.; Gekht, Eugene, Particle separator and separating method for gas turbine engine.
  10. LeBlanc, Ryan Edward; Cummings, Kevin J.; Ali, Amr, Reduced height ligaments to minimize non-integral vibrations in rotor blades.
  11. Leblanc,Andr? Denis; Ouellet,Gilbert, Shockwave-induced boundary layer bleed.
  12. Hofer, Douglas Carl; Nagel, Zachary William; Holmes, David Graham, Supersonic compressor rotor and method of assembling same.
  13. Hofer, Douglas Carl; Gottapu, Dhananjayarao, Supersonic compressor rotor and method of compressing a fluid.
  14. Hofer, Douglas Carl; Nagel, Zachary William; Gottapu, D{acute over (h)}ananjayarao, Supersonic compressor rotor and methods for assembling same.
  15. Hofer, Douglas Carl; Gottapu, Dhananjayarao, Supersonic compressor startup support system.
  16. Vysohlid, Martin; Hofer, Douglas Carl, Supersonic compressor startup support system.
  17. Hofer, Douglas Carl; Michelassi, Vittorio, System and method of assembling a supersonic compressor system including a supersonic compressor rotor and a compressor assembly.
  18. Hofer, Douglas Carl; Gottapu, Dhananjayarao, System and methods of assembling a supersonic compressor rotor including a radial flow channel.
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