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Air modulation apparatus 원문보기

IPC분류정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판)
  • F02C-007/18
출원번호 US-0238257 (1981-02-25)
발명자 / 주소
  • Lenahan Dean T. (Cincinnati OH) Corsmeier Robert J. (Cincinnati OH) Sterman
  • deceased Albert P. (late of Cincinnati OH by Florence G. Sterman
  • executor)
출원인 / 주소
  • The United States of America as represented by the Administrator of the National Aeronautics and Space Administration (Washington DC 06)
인용정보 피인용 횟수 : 35  인용 특허 : 8

초록

An air modulation apparatus, such as for use in modulating cooling air to the turbine section of a gas turbine engine. The apparatus includes valve means disposed around an annular conduit, such as a nozzle, in the engine cooling air circuit. The valve means, when in a closed position, blocks a port

대표청구항

In a gas turbine engine having a cooling air circuit therein for directing cooling air to an engine rotor component, an air modulation apparatus comprising: (a) an annular nozzle including a plurality of circumferentially spaced vanes and a plurality of flow passages, each of said flow passages bein

이 특허에 인용된 특허 (8)

  1. Williams James R. (Martinsville IN), Cooling air control valve.
  2. Lee ; Richard M. ; Szema ; Li C., Cooling system for a gas turbine engine.
  3. Jenkinson John (Bristol GB2), Gas turbine engine cooling system.
  4. Laurello Vincent P. (Guilford CT), Gas turbine engine having bleed apparatus with dynamic pressure recovery.
  5. Patterson William R. (Cincinnati OH), Thermal actuated valve for clearance control.
  6. Adamson Arthur P. (Cincinnati OH), Turbine cooling air modulation apparatus.
  7. Swayne Kenny M. (North Palm Beach FL), Turbine cooling air regulation.
  8. Hoff Richard W. (Newington CT), Turbine vane cooling.

이 특허를 인용한 특허 (35)

  1. Chillar, Rahul J.; Smith, Raub Warfield; Scipio, Alston Ilford, Air bypass system for gas turbine inlet.
  2. Rice, Edward C.; King, Brian P., Apparatus for forming a combustion mixture in a gas turbine engine.
  3. Pineo Frederick J. (Hampton NH) Alvarez Jose T. (Boxford MA), Blade cooling.
  4. Cederwall Philip J. (San Diego CA) Evans David M. (Chula Vista CA) Glezer Boris (San Diego CA) Hensley John J. (San Diego CA), Changeable cooling control system for a turbine shroud and rotor.
  5. Weiler Wolfgang (Dachau DEX), Cooled gas turbine operable with a controlled cooling air quantity.
  6. Tiemann,Peter, Cooling air and injected liquid system for gas turbine blades.
  7. Gebre-Giorgis Yoseph ; Johnson Mark C. ; Kolodziej Michael J. ; Voron Daniel M. ; Wilson Bruce D., Cooling airflow vortex spoiler.
  8. Laborie Daniel J. ; Mc Nulty Michael, Core compartment valve cooling valve scheduling.
  9. Daguenet, Luc Henri Claude, Device for guiding a stream of air entering a combustion chamber of a turbomachine.
  10. Pidcock,Anthony; Close,Desmond, Diffuser for gas turbine engine.
  11. Commaret, Patrice Andre; Hernandez, Didier Hippolyte; Lunel, Romain Nicolas, Diffuser for turbine engine including indented annular webs.
  12. McCaffrey, Michael G., Gas turbine engine component cooling assembly.
  13. Alary Jean-Paul D. (Saint Maur des Fosses FRX) Barbier Gerard Y. G. (Morangis FRX) Delahaye Corine G. (Mormant FRX) Havard Jacques G. W. R. (Moissy Cramayel FRX) Mackovic Paul (Villiers S/Marne FRX) , Gas turbine engine having an integral guide vane and separator diffuser.
  14. Caprario, Joseph T.; Gregg, Shawn J.; Hyland, Dave J., Gas turbine engine including a pre-diffuser heat exchanger.
  15. Coulon,Sylvie; Taillant,Jean Claude; Hacault,Michel, Gas turbine with stator shroud in the cavity beneath the chamber.
  16. Lebel, Jean-Francois; Davies, Alex; Haselbach, Frank; Fletcher, Paul, Method and apparatus for controlling modulated cooling of a gas turbine component.
  17. Corsmeier, Donald Michael; Perveiler, David Andrew; Johnson, George Joseph, Method and apparatus for regulating fluid flow through a turbine engine.
  18. Sal Albert Leone ; Matthew David Book ; Christopher R. Banares, Method for pressure modulation of turbine sidewall cavities.
  19. Rahaim, John Joseph; Fusinato, Daniel John; Hunter, Scott David; Kirk, Joel Francis; Melzak, Michael Robert; Stover, Curtis Walton, Modulated turbine cooling system.
  20. Palmer Donald L., Passive turbine coolant regulator responsive to engine load.
  21. Zhang, Jianmin; Kippel, Brad Aaron, Pre-filtration bypass for gas turbine inlet filter house.
  22. Thiyagarajan, Manikandan; Rangaswamy, Anantha Ramesh; Gopal, Pugalenthi Nanda, Pressure-actuated plug.
  23. Scheffler Charles E. (Macomb MI) McClelland Richard E. (Imlay City MI), Pulsation valve.
  24. Duncan ; III Garland H. (Tequesta FL) Cooper David L. (North Palm Beach FL), Strutless diffuser for gas turbine engine.
  25. Sal Albert Leone ; Matthew David Book ; Christopher R. Banares, System for pressure modulation of turbine sidewall cavities.
  26. Casoni, Andrea, System to feed cooling air into a gas turbine rotor.
  27. Upadhyay, Siddharth; Chillar, Rahul J., Systems and methods for bypassing an inlet air treatment filter.
  28. Glezer Boris ; Bagheri Hamid, Turbine blade clearance control system.
  29. Maclin Harvey M. (Cincinnati OH) Lenahan Dean T. (Cincinnati OH) Tuley ; Eugene N. (Hamilton OH), Turbine cooling air modulation.
  30. Schwarz Frederick M. (Glastonbury CT) Griffin James G. (West Hartford CT), Turbine cooling air supply system.
  31. Hagle Michael P. (Erie PA) McKay John P. (Newport KY), Turbine cooling flow modulation apparatus.
  32. Smith Raymond (Monclova OH) Peregoy Quentin Z. (Toledo OH) Richardson George E. (Sylvania OH), Turbine engine blade variable cooling means.
  33. Corsmeier, Donald Michael; Dawson, David Lynn, Turbine engine valve assembly and method of assembling the same.
  34. Guimier Michel S. (Mormani FRX) Kapala Patrick (Claye Souilly FRX) Paris Philippe (Le Mee sur Seine FRX), Turbo-engine exhaust gas housing with temperature control device.
  35. Charbonnel, Jean-Louis; Debeneix, Pierre; Glynn, Christopher C.; Marey, Daniel J.; Mourlan, Jean-Pierre A. J.; Naudet, Jacky S.; Receveur, Gerard; Rigaud, Yann J. M.; Walker, Roger C., Turbomachine stator having a double skin casing including means for preventing gas flow longitudinally therethrough.
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