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특허 상세정보

MyON담기
내보내기 페이스북 공유 카카오톡 공유

Integrated support and mixer for turbo machinery

특허상세정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F02K-001/38   
미국특허분류(USC) 060/262; 060/770; 060/0395; 181/220
출원번호 US-0770262 (2007-06-28)
등록번호 US7882696 (2011-01-26)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Ingrassia Fisher & Lorenz, P.C.
인용정보 피인용 횟수 : 10  인용 특허 : 41
초록
▼

A support and air mixer includes an inner annular member, an outer annular member shaped and positioned such that an annular air gap is formed between the inner annular member and the outer annular member, and a plurality of air mixing members, each air mixing member having a mixing passageway therethrough and each air mixing member having an inner portion connected to the inner annular member, an outer portion connected to the outer annular member, and first and second opposing side portions interconnecting the inner and outer portions and the inner and...

대표
청구항
▼

What is claimed is: 1. An integrated support and air mixer for turbo machinery comprising:an inner annular member;an outer annular member shaped and positioned such that an annular air gap is formed between the inner annular member and the outer annular member; anda plurality of air mixing members, each air mixing member having a mixing passageway therethrough and each air mixing member having an inner portion connected to the inner annular member, an outer portion connected to the outer annular member, and first and second opposing side portions interco...

이 특허에 인용된 특허 (41)

  1. Steckbeck James F. (San Diego CA) Naik Sharad (Chula Vista CA). Aerodynamic stiffening ring for an aircraft turbine engine mixer. USP1993115265807.
  2. Presz ; Jr. Walter M. ; Reynolds Gary. Alternating lobed mixer/ejector concept suppressor. USP1999035884472.
  3. Kirker Timothy J. (Alvaston GB2). By-pass gas turbine engines. USP1980104227370.
  4. Maguire, Addison C.. Bypass gas turbine aeroengines and exhaust mixers therefor. USP1985104548034.
  5. DiSabato Vincent J. (Southington CT). Combined guide vane and mixer for a gas turbine engine. USP1977094045957.
  6. Anderson,Morris G.; Gerrard,John C.; Ruiz,Ron G.; Mitchell,Robert D.. Compact mixer with trimmable open centerbody. USP2009037506501.
  7. Presz ; Jr. Walter M. ; Reynolds Gary. Contoured thrust reverser and lobed nozzle noise suppressor for gas turbine engines. USP2001056233920.
  8. Zysman Steven H. (Middletown CT) Lord Wesley K. (Glastonbury CT) Barber Thomas J. (West Hartford CT). Double lobed mixer with major and minor lobes. USP1997065638675.
  9. Lair, Jean-Pierre. Duplex mixer exhaust nozzle. USP2004096786038.
  10. Kirker, Timothy J.. Exhaust flow mixers and nozzles. USP1985104543784.
  11. Siefker, Robert G.; Vittal, Baily Ramachandra; Baker, Von David; Khalid, Syed Arif; Loebig, James Carl. Exhaust mixer and apparatus using same. USP2003086606854.
  12. Mavrocostas George (Lanarca CYX). Exhaust mixer for turbofan aeroengine. USP1986034576002.
  13. Rodgers Leonard J. (Spondon GB2). Exhaust mixer for turbofan aeroengine. USP1984124487017.
  14. Torkelson Delbert W. (Catoosa OK) Jannetta Thomas J. (Tulsa OK) Nikkanen John P. (West Hartford CT) Webb Daniel E. (Wethersfield CT) Zysman Steven H. (Middletown CT) Colletti William D. (Cromwell CT). Fixed geometry mixer/ejector suppression system for turbofan aircraft engines. USP1995085440875.
  15. Lord,Wesley K.; Zysman,Steven H.; Howlett,Matthew J.. Fluid mixer with an integral fluid capture ducts forming auxiliary secondary chutes at the discharge end of said ducts. USP2008107434384.
  16. Johnson ; Joseph M.. Gas turbine exhaust nozzle for controlled temperature flow across adjoining airfoils. USP1978014066214.
  17. Ayyagari ; Radhakrishna. Gas turbine mixer apparatus for suppressing engine core noise and engine fan noise. USP1978034077206.
  18. Braithwaite Anthony (Nottingham GB2). Gas turbine nozzles. USP1989034813230.
  19. Horgan John J. (Wethersfield CT). Gas turbine outlet arrangement. USP1987094696159.
  20. Wright Charles P. (Seattle WA) Thornock Russel L. (Seattle WA). Jet engine multiduct noise suppressor. USP1981034254620.
  21. Torkelson Delbert W. (Claremore OK). Jet engine noise suppression system. USP1990034909346.
  22. Syltebo Bjarne Elroy (Bellevue WA). Jet engine nozzle for controlling the direction of thrust. USP1977094050631.
  23. Seiner John M. ; Gilinsky Mikhail M.. Jet nozzle having centerbody for enhanced exit area mixing. USP1999075924632.
  24. Eiler Donald C. (South Windsor CT). Lobe mixer for gas turbine engine. USP1983084401269.
  25. Wynosky Thomas A. (Madison CT) Streib Richard A. (Palm Beach Gardens FL) Campbell Charles A. (Palm Beach Gardens FL). Lobe mixer for gas turbine engine. USP1979044149375.
  26. Michael John Dowhan CA; Joseph Horace Brand CA; Andreas Eleftheriou CA; Andrew Robertson Waterston CA. Method of manufacturing seamless self-supporting aerodynamically contoured sheet metal aircraft engine parts using nickel vapor deposition. USP2002106463992.
  27. Zysman Steven H. ; Lord Wesley K. ; Barber Thomas J.. Method of noise suppression for a turbine engine. USP1998075775095.
  28. Koshoffer John M. (Cincinnati OH) Pfefferle Richard A. (Cincinnati OH) Larson Harold A. (Cincinnati OH). Mixed flow augmentor incorporating a fuel/air tube. USP1987084686826.
  29. Conete, Eric; Philippe, Eric; Baroumes, Laurent. Mixer for separate-flow nozzle. USP2010037677026.
  30. Batey John G. (Cordova TN) Burrets Park W. (Memphis TN) Grewe William F. (Memphis TN) Whitestone Bruce G. (Germantown TN) Yerger Mark D. (Collierville TN). Noise reduction kit for jet turbine engines. USP1992075127602.
  31. Neal ; Brian ; Andersen ; Lars Q.. Noise suppressing exhaust mixer assembly for ducted-fan, turbojet engine. USP1978104117671.
  32. Hauser Joseph R.. Noise suppressing fluid mixing system for a turbine engine. USP2000016012281.
  33. Zauner,Gunter. Pre-converter device for cleaning exhaust gas for an internal combustion engine. USP2008067384609.
  34. Balzer, Ronald L.. Segmented mixing device having chevrons for exhaust noise reduction in jet engines. USP2003096612106.
  35. Martens, Steven. Shelf truncated chevron exhaust nozzle for reduction of exhaust noise and infrared (IR) signature. USP2003036532729.
  36. Kraemer Gilbert O. ; Berry Jonathan Dwight. Swirling flashback arrestor. USP2001016179608.
  37. Laskody Jerome R. (Bellevue WA). Thrust correlated engine pressure ratio indicator and method for turbofan engines with mixer-type nozzles. USP1977014003249.
  38. Prior Barry (San Diego CA). Turbo fan engine mixer. USP1981104292803.
  39. Nikkanen John P. ; Jannetta Thomas J.. Turbofan engine exhaust mixing area modification for improved engine efficiency and noise reduction. USP1998035722233.
  40. Anderson,Morris G.; Ross,David F.. Twisted mixer with open center body. USP2008067389635.
  41. Shannon Aubrey J. (407 94th S.E. Bellevue WA 98004). Variable geometry nozzle. USP1988074754924.

이 특허를 인용한 특허 피인용횟수: 10

  1. Sonokawa, Masayoshi; Witlicki, Russell B.; Larson, Christopher J.; Stutz, Robert C.; Mundell, Eric Charles; Muldoon, Marc J.. Buffer airflow to bearing compartment. USP20190110167734.
  2. Halbei, Julia; Rudelt, Josef; Neumann, Felix; Meiser, Sabine; Horn, Matthias; Hofmann, Thomas Christian. Exhaust gas system for an internal combustion engine. USP2011077975472.
  3. Yan, Guorong; Cunningham, Mark; Di Paola, Franco. Gas turbine engine ejector. USP20190210197009.
  4. Di Paola, Franco; Lefebvre, Guy; L'Esperance, Patrick; Emard-Parent, Gabriel. Gas turbine engine exhaust ejector/mixer. USP2017089745919.
  5. Marques, Edward C.; Moore, Matthew D.. Internal mixing of a portion of fan exhaust flow and full core exhaust flow in aircraft turbofan engines. USP2013018341935.
  6. Moore, Matthew D.; Marques, Edward C.. Internal mixing of a portion of fan exhaust flow and full core exhaust flow in aircraft turbofan engines. USP20181010094334.
  7. Düsing, Michael. Reheat burner and method of mixing fuel/carrier air flow within a reheat burner. USP2017019541293.
  8. Kim, Ju-In. Tailpipe for muffler of vehicle having multiple inner pipes. USP2017059638087.
  9. Durocher, Eric; Lefebvre, Guy. Turbine exhaust case mixer of gas turbine with variable thickness. USP20190110190536.
  10. Moore, Matthew D.; Marques, Edward C.. Turbofan engine with variable exhaust cooling. USP2017029574518.

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