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Single surface independent aircraft control

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64C-003/44   
미국특허분류(USC) 244/219 ; 244/036 ; 244/130 ; 244/045R
출원번호 US-0311072 (1999-05-13)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Anderson
인용정보 피인용 횟수 : 32  인용 특허 : 15
초록
▼

In accordance with the present invention, there is provided an aerodynamic control device for integrated use with an aircraft having an inboard lifting member. The inboard lifting member having a leading edge, a pair of opposing distal edges and a trailing edge. The control device is provided with a movable outboard member which extends substantially about the leading, distal and trailing edges of the inboard lifting member and is spaced apart therefrom. The outboard member is provided with a leading edge portion, a pair of opposing distal edge portions,...

대표
청구항
▼

[ What is claimed is:] [1.]1. An aerodynamic control device for integrated use with an aircraft having an inboard lifting member having a leading edge, a pair of opposing distal edges and a trailing edge, the aerodynamic control device comprising:a movable outboard member extending substantially about the leading, distal and trailing edges of the inboard lifting member and spaced apart therefrom, the outboard member having a leading edge portion, a pair of opposing distal edge portions, and a trailing edge portion, the leading, trailing and distal edge p...

이 특허에 인용된 특허 (15)

  1. Gerhardt Heinz A. (Redondo Beach CA). Aircraft outboard control. USP1992105156358.
  2. Grow Harlow B. (Pacific Palisades CA). Aircraft wing with internal flow control propulsion. USP1977054026500.
  3. Greenhalgh Samuel (Doylestown PA). Aircraft with single surface membranous airfoils. USP1987054667898.
  4. Frost Richard C. (Fort Worth TX) Gomez Eduardo W. (Fort Worth TX) McAnally Robert W. (Fort Worth TX). Airfoil variable cambering device and method. USP1981014247066.
  5. Vass Gabor I. (118-10221 133A Street Surrey ; B.C. CAX V3T 5J8). Circular wing aircraft. USP1996045503351.
  6. Moppert Joseph C.. Control surface continuous seal. USP1998115839698.
  7. Eppler Richard (Leibnizstrasse 84 7000 Stuttgart 1 DEX). Device to support rudders and trailing edge flaps of aircraft and watercraft. USP1980104230295.
  8. Diller Joseph B. ; Miller ; Jr. Nicholas F.. Elastomeric transition for aircraft control surface. USP1998085794893.
  9. Kim Kyusik (5026 Rhoads Ave. Santa Barbara CA 93111). Induction lift aircraft. USP1987034651953.
  10. Thompson Harold L. (Okmulgee OK). Land, water and air craft. USP1989094865275.
  11. Rao Dhanvada M. (Yorktown VA). Lift augmentation for highly swept wing aircraft. USP1993105255881.
  12. Gerhardt Heinz A. (Redondo Beach CA). Supersonic natural laminar flow wing. USP1996075538201.
  13. Cole James B. (Mercer Island WA). Variable camber airfoil. USP1976113994451.
  14. Zapel Edwin J. (Box 433 Maple Valley WA 98038). Variable camber leading edge for airfoil. USP1979104171787.
  15. Ango Alvino J. (1252 Elliott St. Madison Heights MI 48071). Variable lift advancing wing aircraft. USP1979094166595.

이 특허를 인용한 특허 피인용횟수: 32

  1. Good,Mark S.; Huynh,Neal V.; Jones,Kelly T.; Sakurai,Selya. Actuation device positioning systems and associated methods, including aircraft spoiler droop systems. USP2007127309043.
  2. Perez Sanchez,Juan. Adjustment mechanism for a variable-shape wing. USP2006097108231.
  3. Voogt, Nicolaas. Aerospace vehicle fairing systems and associated methods. USP2010057721999.
  4. Voogt,Nicolaas. Aerospace vehicle fairing systems and associated methods. USP2007117300021.
  5. Sakurai,Seiya; Finnila,James E.; Stephenson,Martin F.. Aerospace vehicle flow body systems and associated methods. USP2009037500641.
  6. Konings,Christopher A.. Aerospace vehicle leading edge slat devices and corresponding methods. USP2008017322547.
  7. Jones,Kelly T.. Aircraft control surface drive system and associated methods. USP2009037506842.
  8. Rampton,Scott N.; Amorosi,Stephen R.. Aircraft leading edge apparatuses and corresponding methods. USP2007097270305.
  9. Lacy,Douglas S.; Wyatt,Greg H.. Aircraft leading edge device systems and corresponding sizing methods. USP2008047357358.
  10. Lacy, Douglas S.; Beyer, Kevin W.; Brown, Stephen T.; Dees, Paul W.; Huynh, Neal V.; Kordel, Jan A.; Prow, Clayton A.; Sakurai, Seiya. Aircraft trailing edge devices, including devices with non-parallel motion paths, and associated methods. USP2010067744040.
  11. Lacy,Douglas S.; Beyer,Kevin W.; Brown,Stephen T.; Dees,Paul W.; Huynh,Neal V.; Kordel,Jan A.; Prow,Clayton A.; Sakurai,Seiya. Aircraft trailing edge devices, including devices with non-parallel motion paths, and associated methods. USP2009017475854.
  12. Good,Mark S.; Viigen,Paul M.; Gitnes,Seth E.; Thomas,Glynn Michael. Aircraft wing systems for providing differential motion to deployable lift devices. USP2009027494094.
  13. Arata,Allen A.; Graham,David H.. Aircraft with articulated leading edge of fuselage and wings. USP2007047204454.
  14. Arata,Allen A.. Aircraft with rotatable leading edge of fuselage and wings. USP2007077246770.
  15. Gosling, Harry George Dennis. Annular airborne vehicle. USP2013048408489.
  16. Gosling, Harry George Dennis. Annular airborne vehicle. USP2012128328131.
  17. Gosling, Harry George Dennis. Annular airborne vehicle. USP2012098262016.
  18. Birkenstock, David. Apparatus, system and method for drag reduction. USP2017099764823.
  19. Wheaton, James M.; Amorosi, Stephen R.. Leading edge flap apparatuses and associated methods. USP2010117828250.
  20. Wheaton,James M.; Amorosi,Stephen R.. Leading edge flap apparatuses and associated methods. USP2007097264206.
  21. Fox, Stephen J.; Sakurai, Seiya. Link mechanisms for gapped rigid krueger flaps, and associated systems and methods. USP2009087578484.
  22. Espagnan, Lionel; Hormiere, Arnaud; Guillaumel, Francois. Method for improving the performance of an aircraft. USP2012078210472.
  23. Etling, Keith A.. Morphing control surface transition. USP2013018342447.
  24. Sakurai,Seiya; Fox,Stephen J.; Beyer,Kevin W.; Lacy,Douglas S.; Johnson,Paul L.; Wells,Stephen L.; Noble,Jack S.; Meredith,Paul T.; Huynh,Neal V.; Christianson,Russell R.; Vijgen,Paul M.; Fitzpatrick. Multi-function trailing edge devices and associated methods. USP2007077243881.
  25. Rawdon, Blaine K.; Grip, Robert E.. Providing skins for aircraft fuselages. USP2012038128025.
  26. Manley, David J.; Grip, Robert E.. Shape-changing control surface. USP2013028382045.
  27. Huynh, Neal V.; Bleeg, Robert J.; Pepper, Ralph Scott; Standley, John A.; Bocksch, Brian L.. Systems and methods for controlling aircraft flaps and spoilers. USP2011027891611.
  28. Huynh,Neal V.; Bleeg,Robert J.; Pepper,Ralph Scott; Standley,John A.; Bocksch,Brian L.. Systems and methods for controlling aircraft flaps and spoilers. USP2008037338018.
  29. Good, Mark S.; Vijgen, Paul M.; Gitnes, Seth E.; Thomas, Glynn Michael. Systems and methods for providing differential motion to wing high lift device. USP2010067726610.
  30. Kordel, Jan A.; Sakurai, Seiya; Balzer, Michael A.; Dovey, John V.. Trailing edge device catchers and associated systems and methods. USP2010087766282.
  31. Speer,Thomas E.. Vehicle control systems and corresponding sizing methods. USP2008097424350.
  32. Law, Barnaby. Wing unit, in particular spar box, for forming aerodynamically active surfaces of an aircraft, in particular airfoils, horizontal tail units or rudder units of a plane. USP2009107607617.

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