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특허 상세정보

Aircraft air intakes

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64D-033/02   
미국특허분류(USC) 244/53B ; 137/151
출원번호 US-0474856 (1974-05-30)
우선권정보 UK-0026136 (1973-05-31); UK-0053123 (1973-11-15)
발명자 / 주소
출원인 / 주소
인용정보 피인용 횟수 : 26  인용 특허 : 0
초록

A supersonic two-dimensional intake arrangement for two or more jet propulsion engines has a duct for each engine, a mouth region for each duct, said mouth regions being positioned in adjacent rearewardly staggered rearwardly such that at least one shock wave is common to all mouth regions. Preferably one duct wall is common to adjacent intake mouths.

대표
청구항

An air intake arrangement for at least two jet propulsion engines for a supersonic aircraft the air intake arrangement comprising: means defining a first intake duct, including four bounding sidewall means in two pairs of opposing sidewall means defining a first forward facing intake duct mouth region of generally rectangular shape; means defining a second intake duct, including four bounding sidewall means in two pairs of opposing sidewall means defining a second forward facing intake duct mouth region of generally rectangular shape; the intake ducts be...

이 특허를 인용한 특허 피인용횟수: 26

  1. Sanders, Bobby W.; Sanders, Charlotte A.; Weir, Lois J.. Airflow controller. USP2005076920890.
  2. Haas Jan T. (Hamburg DEX) Hadwin Robin-Leslie (Buxtehude DEX). Controllable diffuser for an air intake of an aircraft. USP1987024641678.
  3. Smith, Thomas R.; Espinosa, Angel M.; Farrell, Daniel J.; Robertson, Andrew; Leylegian, John C.; Tyll, Jason S.; Girlea, Florin; Alifano, Joseph A.; Chue, Randy S. M.. Hypersonic inlet systems and methods. USP2012108292217.
  4. Nelson, Chester P.. Integrated and/or modular high-speed aircraft. USP2005096938854.
  5. Koncsek Joseph L. ; Marrs Kenneth J.. Internal compression supersonic engine inlet. USP1999105971000.
  6. Koncsek Joseph L. ; Marrs Kenneth J.. Internal compression supersonic engine inlet. USP1999035881758.
  7. Conners, Timothy R.; Henne, Preston A.; Howe, Donald C.. Isentropic compression inlet for supersonic aircraft. USP2016119482155.
  8. Conners, Timothy R.; Howe, Donald C.; Henne, Preston A.. Isentropic compression inlet for supersonic aircraft. USP2012128333076.
  9. Henne, Preston A.; Conners, Timothy R.; Howe, Donald C.. Isentropic compression inlet for supersonic aircraft. USP2012128327645.
  10. Henne, Preston A.; Conners, Timothy R.; Howe, Donald C.. Isentropic compression inlet for supersonic aircraft. USP2012108286434.
  11. Lebas, Guillaume. Jet engine nacelle for a supersonic aircraft. USP2009127631836.
  12. Conners, Timothy R.. Low shock strength inlet. USP2013038393158.
  13. Conners, Timothy R.. Low shock strength propulsion system. USP2014068739514.
  14. Conners, Timothy R.. Low shock strength propulsion system. USP2014078783039.
  15. Koncsek, Joseph L.; McMahon, Steven L.; Bultman, Myron L.; Sangwin, Michael L.. Method and apparatus for controlling aircraft inlet air flow. USP2003106634595.
  16. Scarton Henry A. (Troy NY) Kennedy Warren C. (Pittsburgh PA) Gaylo Keith R. (Syosset NY). Method and apparatus for treating exhaust gases particularly for air-operated tools. USP1982054327817.
  17. Scarton Henry A. (Troy NY) Kennedy Warren C. (Pittsburgh PA) Gaylo Keith R. (Syosset NY). Method and apparatus for treating exhaust gases particularly for air-operated tools. USP1981014244442.
  18. Parikh, Pradip G.. Passive removal of suction air for laminar flow control, and associated systems and methods. USP2011017866609.
  19. Livingston David E. (Huntsville AL) Kornell Thomas J. (Federal Way WA). Single-piece, flexible inlet ramp. USP1991075033693.
  20. Henne, Preston A.; Conners, Timothy R.; Howe, Donald C.. Supersonic aircraft jet engine installation. USP2016059334801.
  21. Henne, Preston A.; Howe, Donald C.; Wolz, Robert R.; Hancock, Jr., Jimmy L.. Supersonic aircraft with spike for controlling and reducing sonic boom. USP2014078789789.
  22. Sanders, Bobby W.; Koncsek, Joseph L.; Hedges, Linda S.. Supersonic external-compression diffuser and method for designing same. USP2004096793175.
  23. Falempin Francois (Saint Michel sur Orge FRX). Symmetrical, two dimensional, supersonic and hypersonic air intake for the combustion air of an aircraft engine. USP1991045004187.
  24. Falempin Francois (Saint Arnoult en Yvelines FRX) Fourt Olivier (Jouy en Josas FRX) Pastre Jean-Louis (Sainte Genevieve des Bois FRX). Two-dimensional supersonic and hypersonic air intake, with three movable ramps, for the combustion air of an aircraft en. USP1996125586735.
  25. Koncsek Joseph L. (Seattle WA). Two-stage supersonic inlet. USP1991024991795.
  26. Karanian Arthur J. (Wethersfield CT). Variable-geometry inlet. USP1986114620679.