$\require{mediawiki-texvc}$
  • 검색어에 아래의 연산자를 사용하시면 더 정확한 검색결과를 얻을 수 있습니다.
  • 검색연산자
검색연산자 기능 검색시 예
() 우선순위가 가장 높은 연산자 예1) (나노 (기계 | machine))
공백 두 개의 검색어(식)을 모두 포함하고 있는 문서 검색 예1) (나노 기계)
예2) 나노 장영실
| 두 개의 검색어(식) 중 하나 이상 포함하고 있는 문서 검색 예1) (줄기세포 | 면역)
예2) 줄기세포 | 장영실
! NOT 이후에 있는 검색어가 포함된 문서는 제외 예1) (황금 !백금)
예2) !image
* 검색어의 *란에 0개 이상의 임의의 문자가 포함된 문서 검색 예) semi*
"" 따옴표 내의 구문과 완전히 일치하는 문서만 검색 예) "Transform and Quantization"

특허 상세정보

Supersonic external-compression diffuser and method for designing same

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64D-033/02   
미국특허분류(USC) 244/053.B; 137/015.1
출원번호 US-0382437 (1999-08-25)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Alston & Bird LLP
인용정보 피인용 횟수 : 26  인용 특허 : 16
초록

A supersonic external-compression inlet comprises a generally scoop-shaped supersonic compression section for diffusing a supersonic free stream flow. The supersonic compression section includes a main wall having a leading edge and a throat portion downstream of the leading edge, and side portions joined to opposite side edges of the main wall so as to form a generally scoop-shaped structure. The side portions advantageously extend into the supersonic flow stream far enough to encompass the initial oblique shock wave that is attached to the leading edge...

대표
청구항

1. An external-compression supersonic inlet comprising:a supersonic compression section for diffusing a supersonic free stream flow, the supersonic compression section including a main wall having a leading edge and a throat portion downstream of the leading edge, the supersonic compression section having side portions joined to opposite side edges of the main wall so as to form a generally scoop-shaped structure, the main wall having an inner surface formed generally as a circumferentially extending portion of a surface of revolution, said inner surface...

이 특허에 인용된 특허 (16)

  1. Nangia Rajendar Kumar (Bristol EN). Aircraft air intakes. USP1976033941336.
  2. Gruensfelder Cynthia Ann. Auxiliary inlet for a jet engine. USP2000066079667.
  3. Tindell Runyon H. (Old Bethpage NY). Blown boundary layer control system for a jet aircraft. USP1995095447283.
  4. Brossier Pascal N. (Lieusaint FRX) Mazeaud Georges (Yerres FRX) Wurniesky Pascal C. (Savigny Le Temple FRX). Combined jet engine with RAM jet and turbojet. USP1994095347807.
  5. Ferguson, Stanley D.; Eastman, Donald W.. High performance submerged air inlet. USP1983034378097.
  6. Kutschenreuter ; Jr. Paul H. (Loveland OH). High performance supersonic bleed inlet. USP1995035397077.
  7. Bichler Bartholomus (Raubling DEX) Jost Michael (Mnchen DEX). Inlet ramp for supersonic or hypersonic aircraft. USP1992015078341.
  8. Bichler Bartholomus (Raubling DEX) Jost Michael (Munich DEX). Inlet system for supersonic or hypersonic aircraft. USP1992055116251.
  9. Koncsek Joseph L. ; Marrs Kenneth J.. Internal compression supersonic engine inlet. USP1999035881758.
  10. John Helmut (Munich DEX) Herrmann Otfrid (Hohenthann DEX). Propulsion system for hypersonic flight. USP1990044919364.
  11. Syberg Jan (Kent WA). Supersonic inlet having variable area sideplate openings. USP1983024372505.
  12. Kutschenreuter ; Jr. Paul H. (Loveland OH). Telescoping centerbody wedge for a supersonic inlet. USP1994045301901.
  13. 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.
  14. Koncsek Joseph L. (Seattle WA). Two-stage supersonic inlet. USP1991024991795.
  15. Dobie William B. S. (Bristol GB2) Penistone Nigel (North Humberside GB2). Variable air intake ramps for aerospace vehicles. USP1991065026004.
  16. Kepler Charles Edward (East Hartford CT). Variable geometry ramjet engine. USP1976083974648.

이 특허를 인용한 특허 피인용횟수: 26

  1. Adamson, Eric E; Fugal, Spencer Robert. Flow inlet. USP2018029896219.
  2. Bulman, Melvin J.; Billig, Frederick S.; Baumler, legal representative, Linda A.. Integrated air inlet system for multi-propulsion aircraft engines. USP201210RE43731.
  3. Elvin, John D.. Integrated inward turning inlets and nozzles for hypersonic air vehicles. USP2011017866599.
  4. Conners, Timothy R.; Henne, Preston A.; Howe, Donald C.. Isentropic compression inlet for supersonic aircraft. USP2016119482155.
  5. Conners, Timothy R.; Howe, Donald C.; Henne, Preston A.. Isentropic compression inlet for supersonic aircraft. USP2012128333076.
  6. Henne, Preston A.; Conners, Timothy R.; Howe, Donald C.. Isentropic compression inlet for supersonic aircraft. USP2012128327645.
  7. Henne, Preston A.; Conners, Timothy R.; Howe, Donald C.. Isentropic compression inlet for supersonic aircraft. USP2012108286434.
  8. Lebas, Guillaume. Jet engine nacelle for a supersonic aircraft. USP2009127631836.
  9. Conners, Timothy R.. Low shock strength inlet. USP2013038393158.
  10. Conners, Timothy R.. Low shock strength inlet. USP2015059027583.
  11. Conners, Timothy R.. Low shock strength propulsion system. USP2014068739514.
  12. Conners, Timothy R.. Low shock strength propulsion system. USP2015038973370.
  13. Conners, Timothy R.. Low shock strength propulsion system. USP2014078783039.
  14. Yao, Jixian; Pastouchenko, Nikolai N.; Malcevic, Ivan. Nacelle for an aircraft aft fan. USP20190310220952.
  15. Petty, Dale William. Sliding ramp nozzle system for a gas turbine engine. USP2014068739548.
  16. Chase, James D.; Garzon, German Andres. Supersonic aircraft jet engine. USP2010117837142.
  17. Chase, James D.; Garzon, German Andres. Supersonic aircraft jet engine installation. USP2011067967241.
  18. Henne, Preston A.; Conners, Timothy R.; Howe, Donald C.. Supersonic aircraft jet engine installation. USP2016059334801.
  19. Henne, Preston A.; Howe, Donald C.; Wolz, Robert R.; Hancock, Jr., Jimmy L.. Supersonic aircraft with spike for controlling and reducing sonic boom. USP2014078789789.
  20. Adamson, Eric E.; Fink, Lawrence E.; Fugal, Spencer R.. Supersonic elliptical ramp inlet. USP2016099447731.
  21. Baruzzini, Dan J.; Miller, Daniel N.; Domel, Neal D.; Hakes, Jeff G.. Suprression of shock-induced airflow separation. USP20180810054048.
  22. Troia, Trajaen J.; Mangus, John F.. Swept gradient boundary layer diverter. USP2017099758253.
  23. Lundy,Brian F.; Klinge,John D.; Leland,Bradley C.. System, method, and apparatus for designing streamline traced, mixed compression inlets for aircraft engines. USP2007047207520.
  24. Leland, Bradley C.; Lundy, Brian F.; Klinge, John D.. System, method, and apparatus for throat corner scoop offtake for mixed compression inlets on aircraft engines. USP2010047690595.
  25. Brown, Dewain Ray. Turbofan jet engine. USP2013118579584.
  26. Huynh, Thuy. Variable-geometry rotating spiral cone engine inlet compression system and method. USP2014048690097.