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특허 상세정보

Supersonic airplane

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64C-023/00    B64C-003/10   
미국특허분류(USC) 244/15 ; 244/45R ; 244/91 ; 244/117R
출원번호 US-0477289 (1983-03-21)
발명자 / 주소
출원인 / 주소
인용정보 피인용 횟수 : 22  인용 특허 : 0
초록

A twin-engine supersonic airplane having an arrow-shaped wing and an elongated fuselage extending approximately equally forward and rearward of the wing. The fuselage is configured for six passengers in a staggered two-abreast seating arrangement and for two pilots seated in tandem. A forebody section of the fuselage, which extends substantially forward of the wing, is of a specific geometric cross-sectional design, i.e., it is an egg-shaped cross section with opposite sidewalls sloping vertically inward in an upward direction. The sidewalls are only of ...

대표
청구항

A supersonic arrow-shaped main wing airplane, comprising: a fuselage having a forebody section located generally forward of said main wing, a center-body section structurally integrated with said main wing, and an aft-body section extending aft of the trailing edge of said main wing; said forebody section and a portion of said center-body section, having side walls sloping vertically inward in an upward direction such that an upward projection therefrom forms an intersection an said intersection, in a longitudinal direction, forms a continuous curved lof...

이 특허를 인용한 특허 피인용횟수: 22

  1. Stuhr, Victor K.. Aircraft engine nacelles and methods for their manufacture. USP2003116651928.
  2. Stuhr, Victor K.. Aircraft engine nacelles and methods for their manufacture. USP2005116966524.
  3. Saint-Jalmes, Bruno; Zaneboni, Jason; Belleville, Mathieu. Aircraft fuselage. USP2012128336823.
  4. O'Boyle Brian J. ; Adamson Eric E. ; Schramm Michael R.. Aircraft support pylon. USP1998095810287.
  5. Morgenstern,John M.; Arslan,Alan E.. Aircraft thickness/camber control device for low sonic boom. USP2006077070146.
  6. Tracy Richard R.. Aircraft wing and fuselage contours. USP2000116149101.
  7. Harrison, Kenneth M.; Powell, Donald T.; Schnelz, James R.; Whitmer, Brett D.. Apparatuses and methods for attaching engine nacelles to aircraft. USP2004076758439.
  8. Seidel, Gerhard E.. Asymmetric passenger arrangement. USP2005126971609.
  9. Sankrithi,Mithra M. K. V.. Cross section for a supersonic airplane. USP2006027000869.
  10. Lugg, Richard H.. Hypersonic aircraft. USP20190310232937.
  11. Retz, Kevin M.; Voogt, Nicholaas; Friend, Michael G.; Holtorf, Christopher R.; Wallace, Mannon L.; Sones, Andrew. Integrated aircraft windshields and associated methods. USP2004116817571.
  12. Nelson, Chester P.. Integrated and/or modular high-speed aircraft. USP2005096938854.
  13. Saiz, Manuel Munoz. Lifting arrangement for aircraft fuselages. USP2005106957792.
  14. Espagnan, Lionel; Hormiere, Arnaud; Guillaumel, Francois. Method for improving the performance of an aircraft. USP2012078210472.
  15. Morgenstern,John M.; Arslan,Alan E.; Moose,Garret A.. Methods for incorporating area ruled surfaces in a supersonic aircraft. USP2007127311287.
  16. Rouleau, Bruce S.; Graham, David H.; Reynolds, Ross S.; Wainfan, Barnaby S.. Supersonic aircraft. USP200303D471854.
  17. Lugg, Richard H.. Supersonic aircraft with shockwave canceling aerodynamic configuration. USP2013068453961.
  18. Jacobson Clayton. Surface effect craft. USP2000016014940.
  19. Barmichev, Sergey D.; Eckert, David W.. Synthetic aisle configuration for an aircraft. USP2012078220741.
  20. Prampolini, Marco; Coraboeuf, Yohann. Ultra-rapid air vehicle and related method for aerial locomotion. USP2015079079661.
  21. Morgenstern,John M.; Arslan,Alan E.. Wing employing leading edge flaps and winglets to achieve improved aerodynamic performance. USP2009017475848.
  22. Quayle,Brian; Morgenstern,John M.; Arslan,Alan E.. Wing gull integration nacelle clearance, compact landing gear stowage, and sonic boom reduction. USP2007057216830.