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특허 상세정보

Transonic flow shockwave position stabilizer

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64C-003/28   
미국특허분류(USC) 244/035.A; 244/214; 244/130; 244/045.R
출원번호 US-0963887 (2001-09-26)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Lewis, John D.
인용정보 피인용 횟수 : 8  인용 특허 : 11
초록

A stabilizer suitable for stabilizing a shock formed during transonic velocity is presented. The stabilizer comprises an inboard end, an outboard end that forms an airfoil, which is positioned opposite the inboard end and, an upper surface that extends between the inboard end and the outboard end. A lower surface also extends between the inboard end and the outboard end and is positioned to oppose the upper surface. A leading edge between the upper surface and lower surface forms the stabilizer nose. A trailing edge positioned opposite the leading edge f...

대표
청구항

A stabilizer suitable for stabilizing a shock formed during transonic velocity is presented. The stabilizer comprises an inboard end, an outboard end that forms an airfoil, which is positioned opposite the inboard end and, an upper surface that extends between the inboard end and the outboard end. A lower surface also extends between the inboard end and the outboard end and is positioned to oppose the upper surface. A leading edge between the upper surface and lower surface forms the stabilizer nose. A trailing edge positioned opposite the leading edge f...

이 특허에 인용된 특허 (11)

  1. Gerhardt Heinz A. ; Seho Kenneth ; Nolan Joan ; Mrdeza Matthew N.. Aircraft with variable forward-sweep wing. USP1999115984231.
  2. Herrick Larry L. ; Bays-Muchmore C. Byram ; Hoffman Michael S. ; LeGrand Louis L. ; Ogg Steven S. ; Paul ; Jr. Bernard P. ; Visser Kenneth D. ; Wells Stephen L.. Blunt-leading-edge raked wingtips. USP2000076089502.
  3. Savill Anthony M. (Cambridge GB2). Control of fluid flow. USP1996085542630.
  4. Hollowell Steven J. ; Robinson Michael R.. Extremely short takeoff and landing of aircraft using multi-axis thrust vectoring. USP1999115984229.
  5. Fujino Michimasa,JPX ; Kawamura Yuichi,JPX. Flow separator reducer. USP2000106126118.
  6. Sirovich Lawrence ; Levich Eugene,ILX ; Bronicki Lucien Y.,ILX. Method and apparatus for controlling turbulence in boundary layer and other wall-bounded fluid flow fields. USP1998085797414.
  7. Finch Thomas (San Antonio TX). Modifications to jet aircraft having aft fuselage-mounted nacelles overlapping the wing assemblies. USP1982014311289.
  8. Vanderhoeven Antonius J. (Bellevue WA). Shock inducing pod for causing flow separation. USP1987024643376.
  9. Mihora Dennis J. (Santa Barbara CA) Cannon Walter E. (San Jose CA). Shock wave stabilization apparatus and method. USP1997125692709.
  10. Neal Ronald D. (Wichita KS) Ross Richard (Sedgwick KS) Hein Joseph N. (Wichita KS). Wing and reduced airspeed system for jet aircraft. USP1977094050651.
  11. Hinkleman Michael J.. Wing leading edge flap and method therefor. USP1999075927656.