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특허 상세정보

Morphing wing leading edge

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64C-021/10   
미국특허분류(USC) 244/200; 244/214; 244/219
출원번호 US-0417201 (2012-03-09)
등록번호 US-8925870 (2015-01-06)
발명자 / 주소
출원인 / 주소
인용정보 피인용 횟수 : 6  인용 특허 : 33
초록

A wing may include a flexible leading edge skin segment having segment ends positioned adjacent to upper and lower leading edge wing skins to form a skin assembly. The upper leading edge wing skin may be positioned between the leading edge skin segment and an upper main wing skin. The lower leading edge wing skin may be positioned between the leading edge skin segment and a lower main wing skin. The wing may include a deployment device configured to flex the upper and lower leading edge wing skins thereby causing the leading edge skin segment to exhibit ...

대표
청구항

1. A wing having a morphing leading edge, comprising: a flexible leading edge skin segment having segment ends positioned adjacent to upper and lower leading edge wing skins to form a skin assembly, the upper leading edge wing skin being positioned between the leading edge skin segment and an upper main wing skin, the lower leading edge wing skin being positioned between the leading edge skin segment and a lower main wing skin; anda deployment device configured to cause the upper and lower leading edge wing skin to move between an undeployed position and...

이 특허에 인용된 특허 (33)

  1. Matsushima Yosuke,JPX ; Iino Yasuhiro,JPX ; Toyosawa Shinichi,JPX ; Kimura Takeshi,JPX ; Fukahori Yoshihide,JPX ; Noda Akeshi,JPX. Air bag. USP1999035879767.
  2. Rowarth Ralph (South Cave GB2). Aircraft wing drooping leading edge device. USP1980044200253.
  3. Strong John R. (King County WA). Composite leaf spring. USP1984084468014.
  4. Hamilton, Brian K.; Hassan, Ahmed; Birchette, Terrence S.; Murrill, Robert R.. Composite material for geometric morphing wing. USP2010097798443.
  5. McAnally Robert W. (Fort Worth TX). Continuous force actuator. USP1982094349169.
  6. Statkus Frank D. (Woodinville WA). Continuous skin, variable camber airfoil edge actuating mechanism. USP1982094351502.
  7. Pierce ; Donald. Flexible aerofoils. USP1978094113210.
  8. Martin, Frank J.. Insert cylinder cabinet cam lock. USP2010057716958.
  9. Clifford-Jones John B. (Hatfield GB2). Leading edge arrangements for aircraft wings. USP1986044585192.
  10. Beyer, Kevin W.; Fox, Stephen J.; Lacy, Douglas S.; Sakurai, Seiya. Method and apparatus for controlling airflow with a leading edge device having a flexible flow surface. USP2004096796534.
  11. Vos, Roelof; Barrett, Ronald M.. Method and apparatus for pressure adaptive morphing structure. USP2013028366057.
  12. Etling, Keith A.. Morphing control surface transition. USP2013018342447.
  13. Shatz Solomon (P.O. Box 523 Cupertino CA 94015). Movable sheet for laminar flow and deicing. USP1997015590854.
  14. Hemmelgarn, Christopher Douglas; Pelley, Bryan Michael; Cable, Kristin Marie; Kirby, Brandon Charles. Passive adaptive structures. USP2014038678324.
  15. Wood, Jeffrey H.; Dunne, James P.. Shape changing airfoil system. USP2012098256719.
  16. Lutke, Kevin R.; Kutzmann, Aaron J.. System and method for pneumatically actuating a control surface of an airfoil. USP2011108042772.
  17. Sakurai Seiya (Seattle WA). Three-position variable camber Krueger leading edge flap. USP1992105158252.
  18. Dean Roy D. (Seattle WA). Three-position variable camber flap. USP1981044262868.
  19. Zimmer Herbert (Friedrichshafen DEX). Transverse force-connected body with variable profiling, particularly an airplane wing. USP1981024252287.
  20. Brown Stephen T. (Bellevue WA) Statkus Frank D. (Woodinville WA). Variable camber aircraft wing tip. USP1984024429844.
  21. Cole James B. (Mercer Island WA). Variable camber airfoil. USP1976113994451.
  22. Cole James B. (Mercer Island WA). Variable camber airfoil. USP1976033941334.
  23. Cole James B. (Mercer Island WA). Variable camber airfoil. USP1976113994452.
  24. Cole James B. (Mercer Island WA). Variable camber flap. USP1979064159089.
  25. McKinney Maurice E. (Bellevue WA). Variable camber leading edge airfoil system. USP1977084040579.
  26. Cole James B. (Mercer Island WA). Variable camber leading edge assembly for an airfoil. USP1987114706913.
  27. Zapel Edwin J. (Box 433 Maple Valley WA 98038). Variable camber leading edge for airfoil. USP1979104171787.
  28. Seiya Sakurai ; Stephen John Fox. Variable camber leading edge for an airfoil. USP2002046375126.
  29. McKinney Maurice E. (Bellevue WA) Rudolph Peter K. C. (Seattle WA). Variable camber leading edge mechanism with Krueger flap. USP1984014427168.
  30. Cole, James B.. Variable-camber airfoil. USP1985114553722.
  31. Obermeyer,Henry K.. Water control gate and actuator therefore. USP2006107114879.
  32. Cole James B. (Mercer Island WA). Wind edge movable airfoil having variable camber. USP1987034650140.
  33. Brown Robert B. (Kent WA). Wing leading edge slat. USP1982114360176.