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특허 상세정보

Aircraft structure to improve directional stability

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64C-003/00   
미국특허분류(USC) 24/404.5R ; 24/401.3 ; 24/403.5R
출원번호 US-0042278 (1998-03-13)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Felsman, Bradley, Vaden, Gunter & Dillon, L.L.P.Bradley
인용정보 피인용 횟수 : 34  인용 특허 : 15
초록

An aircraft structure has an arrangement of aircraft components that provide inherent directional stability for a flight vehicle throughout an angle-of-attack range, even at very high angles-of-attack where conventional means of stabilization are ineffective. Components attached to an aircraft fuselage include a wing, horizontal stabilizers and vertical stabilizers. The wing is mounted forward of the horizontal stabilizers and is carried high on the fuselage. The horizontal stabilizer is mounted toward the rear of the aircraft and is attached near the bo...

대표
청구항

[ What is claimed is:] [1.] An aircraft structure to improve directional stability comprising:a fuselage;a wing mounted to said fuselage;a horizontal stabilizer mounted to a bottom of said fuselage, rearward of and at a lower level than said wing, said horizontal stabilizer having trailing edges on opposite side of said fuselage, each trailing edge having an outboard junction with a tip of said horizontal stabilizer and an inboard junction with said fuselage, wherein said horizontal stabilizer sweeps backward;a forwardly sweeping right directional stabil...

이 특허에 인용된 특허 (15)

  1. Cabrol, Lucien. Aircraft providing with a lift structure incorporating multiple superposed wings. USP1985094541593.
  2. Adkins Gordon V. (Wimborne GBX) McDonald John R. (Wimborne GBX) Sivertsen Olav N. (Isswich GBX). Aircraft with paired aerofoils. USP1989084856736.
  3. Wolkovitch Julian (28603 Trailriders Dr. Rancho Palos Verdes CA 90274). Airplane with braced wings and pivoting propulsion devices. USP1991095046684.
  4. Zimmer ; Herbert. Airplane with two superposed wings. USP1978054090681.
  5. Bullard Gary M. (Rte. #1 ; Box 177 Accomac VA 23301). Combination automobile and airplane. USP1989114881701.
  6. Hall Eric B. (135 ; Spring Grove Crescent Hounslow Middlesex TW3 4DA GB2). Compound wing aircraft. USP1982064336913.
  7. Pruszenski ; Jr. Anthony (No. 3 ; 44th St. Plum Island MA 01951). Ground-air-water craft. USP1990024899954.
  8. Wolkovitch Julian (2109 Prestonwood Dr. Arlington TX 76012). Joined wing aircraft. USP1982124365773.
  9. Wolkovitch Julian (28603 Trailriders Drive Rancho Palos Verdes CA 90274). Joined wing aircraft. USP1976033942747.
  10. Frediani Aldo,ITX. Large dimension aircraft. USP1999055899409.
  11. Eger Vladimir S. (ulitsa Valtera Ulbrikhta ; 14 ; kv.115 Moscow RUX). Light-duty box-wing aeroplane. USP1996045503352.
  12. Wenzel Harold A. (Phoeniz AZ). Multi-winged lifting body aircraft. USP1979034146199.
  13. Geraci Alexander (5221 N. Lind Ave. Chicago IL 60630) DeLouise Joseph (6 E. Monroe St. Chicago IL 60606). Short coupled airplane with variable wing lift. USP1976103985317.
  14. Ratony Alexander (3264 Royal Ave. Simi Valley CA 93065). Staggered channel wing-type aircraft. USP1977104053125.
  15. Ratony Alexander (Simi Valley CA). Staggered channel wing-type aircraft. USP1976093981460.

이 특허를 인용한 특허 피인용횟수: 34

  1. Mark A. Hreha ; Gerard Schkolnik. Adaptive method to control and optimize aircraft performance. USP2002016341247.
  2. Shepshelovich, Michael; Sletean, Mario; Steinbuch, Moshe; Levy, David Eli. Aircraft configuration for micro and mini UAV. USP2012028123160.
  3. McGinnis, John William. Aircraft stability and efficient control through induced drag reduction. USP2017019545993.
  4. Maris, John M.. Airfoil performance monitor. USP2013088514103.
  5. August, Henry. Arch wing and forward steering for an advanced air vehicle. USP2003126659396.
  6. Alford, Jr., Lionel D.; Clayman, Jr., Gary J.. Blended winglet. USP2010017644892.
  7. Fink, Axel; Blacha, Martin. Compound rotorcraft. USP20181110131424.
  8. Hernadi, Andras. Decagonal box-wing aircraft. USP201904D844538.
  9. Hernadi, Andras. Decagonal boxed-wing for aircraft. USP201903D843920.
  10. McGinnis, John William. Efficient control and stall prevention in advanced configuration aircraft. USP2014028657226.
  11. Suokas, Aki. Flying device and a wing construction for the same. USP2016049308984.
  12. Conners, Timothy R.; Henne, Preston A.; Howe, Donald C.. Isentropic compression inlet for supersonic aircraft. USP2016119482155.
  13. Conners, Timothy R.; Howe, Donald C.; Henne, Preston A.. Isentropic compression inlet for supersonic aircraft. USP2012128333076.
  14. Henne, Preston A.; Conners, Timothy R.; Howe, Donald C.. Isentropic compression inlet for supersonic aircraft. USP2012128327645.
  15. Henne, Preston A.; Conners, Timothy R.; Howe, Donald C.. Isentropic compression inlet for supersonic aircraft. USP2012108286434.
  16. Garreau, Oliver F.. Joined-wing tilt-wing aircraft. USP201503D724001.
  17. Houck, II, Ronald G.. Lifting foil. USP2013038387912.
  18. Houck, II,Ronald G.. Lifting foil. USP2006097100867.
  19. Bevirt, Joeben; Gibboney, Jeffrey K.; Craig, David D.; Peddie, Matthew. Lightweight vertical take-off and landing aircraft and flight control paradigm using thrust differentials. USP2014058733690.
  20. Conners, Timothy R.. Low shock strength inlet. USP2013038393158.
  21. Conners, Timothy R.. Low shock strength inlet. USP2015059027583.
  22. Conners, Timothy R.. Low shock strength propulsion system. USP2014068739514.
  23. Conners, Timothy R.. Low shock strength propulsion system. USP2014078783039.
  24. Wilding,Joseph Ray; Olcott,Dennis D.. Methods for manufacturing composite aircraft, parts and a family of composite aircraft. USP2009017478780.
  25. Wilding, Joseph Ray; Olcott, Dennis D.. Modular spar tunnel. USP2004116811120.
  26. Cacciaguerra, Bruno. Rotary-wing and fixed-wing aircraft. USP2014098820673.
  27. Henne, Preston A.; Conners, Timothy R.; Howe, Donald C.. Supersonic aircraft jet engine installation. USP2016059334801.
  28. Henne, Preston A.; Howe, Donald C.; Wolz, Robert R.; Hancock, Jr., Jimmy L.. Supersonic aircraft with spike for controlling and reducing sonic boom. USP2004036698684.
  29. Henne, Preston A.; Howe, Donald C.; Wolz, Robert R.; Hancock, Jr., Jimmy L.. Supersonic aircraft with spike for controlling and reducing sonic boom. USP2014078789789.
  30. Clark, Walter D.. System and method for controlling an aircraft. USP2003116641086.
  31. Cox,Beverly; Dews,Hampton; Nyroth,Nicholas. Unmanned airborne reconnaissance system. USP2006037014141.
  32. Cox,Beverly; Dews,Hampton; Nyroth,Nicholas. Unmanned airborne reconnaissance system. USP2007057210654.
  33. Cox, Beverly; Dews, Hampton; Nyroth, Nicholas. Unmanned biplane for airborne reconnaissance and surveillance having staggered and gapped wings. USP2003096626398.
  34. Churchman, Charles Gilpin. V/STOL biplane. USP2005126974106.