• 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

Airplane configuration

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64C-001/40    B62D-027/00   
미국특허분류(USC) 244/001N; 244/054
출원번호 US-0947169 (2010-11-16)
등록번호 US-8087607 (2012-01-03)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Witsil, Matthew W.
인용정보 피인용 횟수 : 5  인용 특허 : 26

An aircraft configuration that may reduce the level of noise, infrared radiation, or combination thereof directed towards the ground from an aircraft in flight. An embodiment of an aircraft includes a fuselage, two forward swept wings, at least one engine mounted to the aircraft and higher than the wings, and vertical stabilizers mounted on each wing outboard of the outermost engine. The leading edge of the wing may extend forward of the leading end of the engine, and the trailing edge of the aft deck may extend aft of the trailing end of the engine. The...


1. An aircraft comprising: a tubular fuselage having a longitudinal axis;two main wings mounted to the tubular fuselage, each main wing in a substantially forward swept wing configuration and including a leading edge, a trailing edge, and an upper surface;a plurality of engines each with at least one unshrouded propeller, each engine mounted to the aircraft and including a leading end and a trailing end, wherein each engine has a central longitudinal axis that is directly above one of the two main wings, the engines and propellers completely above the ma...

이 특허에 인용된 특허 (26)

  1. Gratzer Louis B. (Seattle WA) Gillette Walter B. (Issaquah WA). Aerodynamically contoured, low drag wing engine and engine nacelle combination. USP1984054449680.
  2. Miller, Jr., William McE.. Airborne surveillance platform. USP1991075034751.
  3. Wintersdorff Robert W. (San Diego CA) Cota George R. (La Jolla CA). Aircraft of low observability. USP1977044019699.
  4. Franklin, III, Walter M.; Morgenstern, John M.; Lee, Howard; Quayle, Brian; Hajic, Ken; Scarcello, John; Arslan, Alan E.. Aircraft tail configuration for sonic boom reduction. USP2004116824092.
  5. Krenz Gunter (Bremen DEX). Aircraft wing with engine mount. USP1979104171786.
  6. Blythe Alan Avery (St. Albans EN) Milligan Robert Ian (Belfast EK). Combined noise shield and thrust reverser. USP1976023936017.
  7. Koenig David G. (Sunnyvale CA) Aoyagi Kiyoshi (Mountain View CA) Dudley Michael R. (Los Altos CA) Schmidt Susan B. (Pensacola FL). High performance forward swept wing aircraft. USP1988084767083.
  8. Retz, Kevin M.; Voogt, Nicholaas; Friend, Michael G.; Holtorf, Christopher R.; Wallace, Mannon L.; Sones, Andrew. Integrated aircraft windshields and associated methods. USP2004116817571.
  9. Nelson, Chester P.. Integrated and/or modular high-speed aircraft. USP2003066575406.
  10. Gerhardt Heinz Adolf ; Kerswell James Franklin ; Priestley Richard Thomas ; Gibson Berry Thomas. Laminar supersonic transport aircraft. USP1998125842666.
  11. Frediani Aldo,ITX. Large dimension aircraft. USP1999055899409.
  12. Bath, David L.; Carta, Salvatore; Jones, Kelly T.; Kramer, Brian J.; Nelson, Chester P.; Penhall, Pieter S.; Pineda, Joseph R.; Sheppard, Andrew. Method and apparatus for installing and actuating movable airfoils, including canards. USP2005086929216.
  13. Bath, David L.; Jones, Kelly T.; McKinney, P. Brian; Pineda, Joseph R.. Method and apparatus for rotatably supporting movable components, including canards. USP2005016843450.
  14. Fujino Michimasa,JPX ; Kawamura Yuichi,JPX. Method for reducing wave resistance in airplane. USP2001106308913.
  15. Kumata Hirotaka,JPX ; Katahira Kiyoshi,JPX ; Wakita Shuichi,JPX ; Nishikawa Toshihiro,JPX. Method for reducing wave resistance in airplane. USP2000086102328.
  16. Finch Thomas (San Antonio TX). Modifications to jet aircraft having aft fuselage-mounted nacelles overlapping the wing assemblies. USP1982014311289.
  17. Lion Charles E. (253 Euclid Ave. Ridgway PA 15853). Reduced noise monolithic wing-stabilizer aircraft. USP1984054447022.
  18. Cymara Hermann K. (106 Stonehaven Cir. Newfield NY 14867). Retractable canard wing surfaces for airplanes. USP1996035495999.
  19. Schairer George S. (Bellevue WA). Retractable engine noise suppression system for over-the-wing jet aircraft. USP1977074036452.
  20. Martens, Steven. Shelf truncated chevron exhaust nozzle for reduction of exhaust noise and infrared (IR) signature. USP2003036532729.
  21. Parikh Pradip G. (Renton WA). Supersonic aircraft and method. USP1994095348256.
  22. Chang, Ming; Meza, Victor; Morgenstern, John M.; Arslan, Alan E.. Supersonic aircraft with channel relief control. USP2005076921045.
  23. Rudolph Peter K. C. (Seattle WA). Supersonic airplane with subsonic boost engine means and method of operating the same. USP1996065529263.
  24. Coe ; Jr. ; Paul L.. Supersonic transport. USP1978064093156.
  25. Wagenfeld Robert E. (New York NY). System for reducing aircraft noise and hush kit. USP1989064836469.
  26. Ross James C. ; Storms Bruce L.. Tip fence for reduction of lift-generated airframe noise. USP1998045738298.