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특허 상세정보

Supersonic natural laminar flow wing

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64C-003/10   
미국특허분류(USC) 244/204 ; 244/36 ; 244/45 ; R
출원번호 US-0167602 (1993-12-14)
발명자 / 주소
출원인 / 주소
인용정보 피인용 횟수 : 16  인용 특허 : 0
초록

A reverse delta aerodynamic wing has a basic reverse delta wing portion bounded by a leading edge and by a pair of trailing edges extending from respective ends of said leading edge toward a trailing apex point and respective span-wise wing extensions in a natural laminar boundary layer wing region extending chordwise from said leading edge by a fraction of the chordlength of said wing and extending span-wise from opposing sides of said wing. Laminar flow control in other regions of the wing employs fuel stored in the wing as a coolant.

대표
청구항

A reverse delta aerodynamic wing, comprising: a basic reverse delta wing portion bounded by a leading edge and by a pair of trailing edges extending inwardly from respective ends of said leading edge toward a trailing apex point and meeting at a point; and respective span-wise wing extensions extending chordwise from said leading edge by a fraction of the chordlength of said wing and extending span-wise from opposing sides of said reverse delta wing portion; wherein a forward portion of said wing experiences two-dimensional flow consistent with achieving...

이 특허를 인용한 특허 피인용횟수: 16

  1. Zhu, Xiaoyi. Aircraft generating a lift from an interior thereof. USP2014128910903.
  2. Arata,Allen A.; Graham,David H.. Aircraft with articulated leading edge of fuselage and wings. USP2007047204454.
  3. Arata,Allen A.. Aircraft with rotatable leading edge of fuselage and wings. USP2007077246770.
  4. Gerhardt Heinz A. ; Seho Kenneth ; Nolan Joan ; Mrdeza Matthew N.. Aircraft with variable forward-sweep wing. USP1999115984231.
  5. Praisner,Thomas J.; Clark,John P.. Boundary layer transition model. USP2006127150427.
  6. Kosheleff, Patrick Andrew. Compression-lift aircraft. USP2014038672259.
  7. Nastasi Richard F. ; Soeder Walter S.. Delta-shaped aircraft with variable camber fuselage and wing. USP2000106129308.
  8. Lugg, Richard H.. Hypersonic aircraft. USP20190310232937.
  9. Bowcutt, Kevin G.. Hypersonic waverider variable leading edge flaps. USP2003106634594.
  10. Arata Allen A.. Single surface independent aircraft control. USP2001056227498.
  11. Arata Allen A.. Single surface multi axis aircraft control. USP2000056068219.
  12. Rouleau, Bruce S.; Graham, David H.; Reynolds, Ross S.; Wainfan, Barnaby S.. Supersonic aircraft. USP200303D471854.
  13. Lugg, Richard H.. Supersonic aircraft with shockwave canceling aerodynamic configuration. USP2013068453961.
  14. Malmuth, Norman; Fedorov, Alexander. Surface plasma discharge for controlling leading edge contamination and crossflow instabilities for laminar flow. USP2004106805325.
  15. Miller ; Jr. John A. ; Losey ; deceased William A. ; Losey ; executor by Marion E.. Universal fluid-dynamic body for aircraft and watercraft. USP1998035730391.
  16. Fedorov Alexander V.,RUX ; Malmuth Norman D.. Use of absorbing walls for laminar flow control. USP1999035884871.