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특허 상세정보

Aircraft configuration

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64C-001/00   
미국특허분류(USC) 244/119; 244/1170R; 244/054; 244/055
출원번호 US-0307271 (2006-01-30)
등록번호 US8016233 (2011-08-30)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Moore & Van Allen PLLC
인용정보 피인용 횟수 : 7  인용 특허 : 27
초록

An aircraft configuration that may reduce the level of noise, infrared radiation, sonic boom, or combination thereof directed towards the ground from an aircraft in flight. In accordance with an embodiment of the present invention, an aircraft includes a tubular fuselage, two delta 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. Each wing may include a wing strake at the leading edge of the wing and extending to the fuselage and an aft deck. The ...

대표
청구항

What is claimed is: 1. A non-blended wing body aircraft comprising:a tubular fuselage;two wings with two wing strakes mounted to the tubular fuselage, the wings and strakes in a substantially delta wing configuration and each including a leading edge and a top surface, the wings each including a trailing edge;a plurality of shrouded turbofan engines, each engine with a nacelle mounted to the aircraft, each engine and nacelle completely and directly above the respective wing, strake, or a combination thereof, each nacelle including a leading end, a traili...

이 특허에 인용된 특허 (27)

  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.
  27. Clifton Robert T. (Houston TX) Cook Woodrow L. (Lake Almanor Peninsula CA). Vertical/short take-off and landing aircraft. USP1989054828203.