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특허 상세정보

Split shroud exhaust nozzle

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B63H-011/00    B64G-009/00    F02K-009/00    F03H-009/00    F23R-009/00   
미국특허분류(USC) 060/204; 060/770; 060/226.1; 239/265.33; 239/265.37
출원번호 US-0898035 (2004-07-23)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Adams Evans P.A.
인용정보 피인용 횟수 : 29  인용 특허 : 26
초록이 없습니다.
대표청구항이 없습니다

이 특허에 인용된 특허 (26)

  1. Speir Donald W. (Cincinnati OH) McHugh Donald P. (Cincinnati OH). Articulated plug nozzle. USP1977084043508.
  2. Butler, Lawrence; Johnson, James Edward; Dunbar, Lawrence Wayne. Combined cycle pulse detonation turbine engine. USP2003126666018.
  3. Johnson, James E.; Dunbar, Lawrence W.; Butler, Lawrence. Combined cycle pulse detonation turbine engine operating method. USP2003046550235.
  4. Hebert, Leonard J.. Convergent/divergent segmented exhaust nozzle. USP2004126826901.
  5. Birch, Nigel T; Webster, John R. Gas turbine engine exhaust nozzle having a noise attenuation device driven by shape memory material actuators. USP2004116813877.
  6. Seiner John M. ; Gilinsky Mikhail M.. Jet nozzle having centerbody for enhanced exit area mixing. USP1999075924632.
  7. Wallace ; Jr. Frank B. (Fairfield OH). Jet propulsion apparatus and methods. USP1985074527388.
  8. Wadia Aspi R. ; Szucs Peter N. ; Hemmelgarn Bruce A.. Leaned and swept fan outlet guide vanes. USP2001036195983.
  9. Smereczniak Philip (St. Peters MO) Spetnagel David R. (St. Charles MO). Method and apparatus for controlling the throat area, expansion ratio and thrust vector angle of an aircraft turbine eng. USP1997125694766.
  10. Robinson Michael R. ; Ouellette Richard P.. Multi axis thrust vectoring for turbo fan engines. USP1998015706649.
  11. Klees Garry W. (Mercer Island WA). Plug-type exhaust nozzle having a variable centerbody and translating shroud. USP1989024802629.
  12. Grieb Hubert (Germering DEX). Propelling nozzle for a hypersonic engine. USP1992115165227.
  13. Martens, Steven. Shelf truncated chevron exhaust nozzle for reduction of exhaust noise and infrared (IR) signature. USP2003036532729.
  14. Janardan, Bangalore Ananthamurthy; Brausch, John Francis. Stub airfoil exhaust nozzle. USP2003016502383.
  15. Jones Robert A. (Madison CT). Thrust reverser. USP1983024373328.
  16. Lawson Dale W. R. (Bonita CA). Thrust reverser - cascade type. USP1982074340178.
  17. Thornock Russel L. (Seattle WA). Translating jet engine nozzle plug. USP1986064592508.
  18. Charier Gilles Alain,FRX ; Andre Guyonnet Xavier Jean-Michel,FRX ; Rollin Gilles Louis,FRX. Turbojet engine thrust reverser and exhaust nozzle. USP2001096289670.
  19. Maiden ; Donald L.. Two dimensional wedge/translating shroud nozzle. USP1978054088270.
  20. Wynosky Thomas A. (Madison CT) Campbell Charles A. (Palm Beach Gardens FL). Two-dimensional nozzle. USP1981104295611.
  21. Seiner John M. ; Gilinsky Mikhail M.. Undulated nozzle for enhanced exit area mixing. USP2000076082635.
  22. Duesler Paul W. ; Loffredo Constantino V. ; Prosser ; Jr. Harold T. ; Jones Christopher W.. Variable area fan exhaust nozzle having mechanically separate sleeve and thrust reverser actuation systems. USP1998075778659.
  23. Rey, Nancy M.; Miller, Robin Mihekun; Tillman, Thomas G.; Rukus, Robert M.; Kettle, John L.. Variable area nozzle for gas turbine engines driven by shape memory alloy actuators. USP2004056735936.
  24. Nightingale, Douglas J.. Variable area nozzles for turbomachines. USP1985084537026.
  25. Wagenknecht Conrad D. (West Chester OH). Variable cycle plug nozzle and flap and method of operating same. USP1977084039146.
  26. Cariola Roy E. ; Aten Michael R.. Variable fan exhaust area nozzle for aircraft gas turbine engine with thrust reverser. USP1998095806302.

이 특허를 인용한 특허 피인용횟수: 29

  1. Zsurka, Mark. Aerodynamic track fairing for a gas turbine engine fan nacelle. USP20190310240561.
  2. Wick, Hal Gerard. Aircraft engine management for fuel conservation. USP2010087769503.
  3. Wick, Hal Gerard. Aircraft engine management for fuel conservation method. USP2013038401719.
  4. Wick, Hal Gerard. Aircraft engine management for fuel conservation method and apparatus. USP2011098014913.
  5. Baker, Von David. Aircraft nozzle having actuators capable of changing a flow area of the aircraft nozzle. USP2013068459036.
  6. Lerg, Bryan H.; Bergeron, Stephen A.; Harding, Benjamin R.. Aircraft nozzle system. USP2018019856824.
  7. Kubiak, Benoit. Control system for turbojet engine nacelle. USP2013118578699.
  8. Pinto, Geoffrey P.. Dual panel actuator system for jet engines. USP20180810040563.
  9. Sutterfield, David Levi. Exhaust for a gas turbine engine. USP2014098844262.
  10. Chanez, Philippe Gerard; Zeggai, Kamel. Gas exhaust nozzle for a bypass turbomachine having an exhaust or throat section that can be varied by moving the secondary cowl. USP2009107600384.
  11. Petty, Dale William; Swanson, Timothy A.; McMahon, Shawn M.. Gas turbine engine systems involving variable nozzles with flexible panels. USP2016029267463.
  12. Petty, Dale William; McMahon, Shawn M.; Murphy, Michael Joseph; Zamora, Sean P.; Swanson, Timothy A.. Gas turbine engine systems involving variable nozzles with sliding doors. USP2013018356483.
  13. Blackwell, Geoffrey T.; McVey, William J.; Tempelman, William G.. Gas turbine engine variable area fan nozzle control. USP2014108869508.
  14. Blackwell, Geoffrey T.; McVey, William J.; Tempelman, William G.. Gas turbine engine variable area fan nozzle control. USP20180610006406.
  15. Zamora, Sean P.; Murphy, Michael Joseph. Gas turbine engine with variable area fan nozzle. USP2012038141366.
  16. McVey, William J.. Managing low pressure turbine maximum speed in a turbofan engine. USP2017019541028.
  17. Swanson, Timothy A.; Zamora, Sean P.; Bush, Robert H.; Simpson, Alex J.. Nozzle-area ratio float bias. USP2011017874160.
  18. Swanson, Timothy A.; Zamora, Sean P.; Bush, Robert H.; Simpson, Alex J.. Nozzle-area ratio float bias. USP2014058733107.
  19. Place, Emma J; Peters, Donald W. Rod-and-bracket connector system for securing a pivoting member to a guide anchor moveably secured within a guide track. USP2018019856956.
  20. Cowan, Curtis C.; Bush, Robert H.. Rollertrack pivoting axi-nozzle. USP2011098020386.
  21. Blodgett,Keith Edward James; Early,Kevin Sean; Martens,Steven; Bailey,William Andrew; Price,Kenneth Daniel. Sinuous chevron exhaust nozzle. USP2007127305817.
  22. Hasting, William Howard; Crall, David William; Higgins, Craig William; Krammer, Erich Alois. System and method for active clearance control. USP2016029260974.
  23. Schirtzinger, Gary A.. Valve system for a gas turbine engine. USP2013038402744.
  24. Schirtzinger, Gary A.. Valve system for a gas turbine engine. USP2012088240126.
  25. Schirtzinger, Gary A.. Valve system for a gas turbine engine. USP2013118578716.
  26. Schirtzinger, Gary A.; Wurzbacher, Lance; Orr, Joseph L.. Valve system for a gas turbine engine. USP2012108286416.
  27. Murphy, Michael J.. Variable area fan nozzle. USP20180810041442.
  28. Schwark, Jr., Fred W.; Atassi, Oliver V.; Owen, William D.. Variable area fan nozzle bearing track. USP2013058443586.
  29. Thomas, Russell H.; Kinzie, Kevin W.. Wet active chevron nozzle for controllable jet noise reduction. USP2011098015819.