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특허 상세정보

Fluid stream deflecting members for aircraft bodies or the like

특허상세정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64C-023/00   
미국특허분류(USC) 244/199 ; 114/272 ; 244/91 ; 244/130
출원번호 US-0805438 (1977-06-10)
우선권정보 GB-0024943 (1976-06-16); GB-0008666 (1977-03-01)
발명자 / 주소
출원인 / 주소
인용정보 피인용 횟수 : 52  인용 특허 : 0
초록

Devices to reduce the drag experienced by aircraft and other travelling bodies, comprising sail-like members mounted on the body surface. These members project into the local stream that forms close to the surface during motion, and tend to divert that local stream back into the free stream direction and in so doing to experience useful thrust. The members are cambered and the camber varies from root to tip to allow for change in the local stream direction as distance from the surface increases. Special sails for use on surfaces subject to some complex f...

대표
청구항

A device to reduce the drag experienced by bodies in motion within and relative to masses of fluid, comprising: a body intended for motion within and relative to a mass of fluid and presenting a body surface; a member of cambered aerofoil cross-section having a given length mounted upon said surface so that the span of said member projects outward from said surface into the space where a local stream of fluid will form in use, whereby in Such use said member will tend to divert said local stream back into the free stream and in so doing experience useful...

이 특허를 인용한 특허 피인용횟수: 52

  1. Guida, Nicholas R.. Active winglet. USP2017099764825.
  2. Wyrembek,Susanne; May,Peter; Muthreich,Klaus. Aerodynamic component for controlling a landing guide path of an aircraft. USP2006077070148.
  3. Goodson Kenneth W. (Rte. 4 ; Box 389 Mt. Olive NC 28365). Airfoil. USP1987064671473.
  4. Waitzman Simon V. (57 Montague St. Brooklyn Heights NY 11201). Airplane airframe. USP1986074598885.
  5. Bodard, Guillaume; Henry, Cyprien; Jodet, Norman; Vuillemin, Alexandre Alfred Gaston. Attachment pylon for a turbine engine. USP2018049938901.
  6. Spranger Guenter (Wagnerstrasse 2 DE-2000 Hamburg 76 DEX). Blade-like profiled device for acting on a gaseous or liquid fluid flow. USP1991035002001.
  7. Guida, Nicholas R.. Controllable airflow modification device periodic load control. USP2017029567066.
  8. McLean, James D.. Efficient wing tip devices and methods for incorporating such devices into existing wing designs. USP2005056886778.
  9. Whitham Kent G. (Inyokern CA). Fin attachment. USP1986024568041.
  10. Schweiger, Johannes. Fluid dynamically effective surface for minimizing induced resistance. USP2009107597285.
  11. Spillman John J. (Bedford GB2). Fluid stream deflecting members for aircraft bodies or the like. USP1981064272043.
  12. Stuhr, Victor K.. Integrated wingtip extensions for jet transport aircraft and other types of aircraft. USP2013108544800.
  13. Conners, Timothy R.; Henne, Preston A.; Howe, Donald C.. Isentropic compression inlet for supersonic aircraft. USP2016119482155.
  14. Conners, Timothy R.; Howe, Donald C.; Henne, Preston A.. Isentropic compression inlet for supersonic aircraft. USP2012128333076.
  15. Henne, Preston A.; Conners, Timothy R.; Howe, Donald C.. Isentropic compression inlet for supersonic aircraft. USP2012128327645.
  16. Henne, Preston A.; Conners, Timothy R.; Howe, Donald C.. Isentropic compression inlet for supersonic aircraft. USP2012108286434.
  17. Conners, Timothy R.. Low shock strength inlet. USP2013038393158.
  18. Conners, Timothy R.. Low shock strength inlet. USP2015059027583.
  19. Conners, Timothy R.. Low shock strength propulsion system. USP2014068739514.
  20. Conners, Timothy R.. Low shock strength propulsion system. USP2014078783039.
  21. Wyrembek,Susanne; May,Peter; Muthreich,Klaus. Method and device for steepening a landing approach of an aircraft. USP2008017316371.
  22. Guida, Nicholas R.. Multiple controllable airflow modification devices. USP2015109162755.
  23. Guida, Nicholas R.. Multiple controllable airflow modification devices. USP2018059969487.
  24. Henderson Michael L. (Seattle WA) Owen Ralph B. (Issaquah WA). Nacelle/wing assembly with vortex control device. USP1987084685643.
  25. Roman, Dino L.; Vassberg, John C.; Friedman, Douglas M.; Malachowski, Adam P.; Vegter, Christopher A.. Performance-enhancing winglet system and method. USP2015018936219.
  26. Gratzer, Louis B.. Split blended winglet. USP20190410252793.
  27. Gratzer, Louis B.. Split blended winglet. USP20180610005546.
  28. Gratzer, Louis B.. Split blended winglet. USP2016049302766.
  29. Gratzer, Louis B.. Split blended winglet. USP2015028944386.
  30. Gratzer, Louis B.. Split blended winglet. USP20181010106247.
  31. Gratzer, Louis B.. Split spiroid. USP2017029580170.
  32. Gratzer, Louis B.. Split spiroid. USP2015059038963.
  33. Gratzer, Louis B.. Split spiroid. USP2016099434470.
  34. Roman, Dino L.; Vassberg, John C.; Friedman, Douglas M.; Malachowski, Adam P.; Vegter, Christopher A.. Split winglet system. USP2017059637226.
  35. Wolfgang Brix DE. Subsonic aircraft with backswept wings and movable wing tip winglets. USP2002026345790.
  36. Henne, Preston A.; Conners, Timothy R.; Howe, Donald C.. Supersonic aircraft jet engine installation. USP2016059334801.
  37. Henne, Preston A.; Howe, Donald C.; Wolz, Robert R.; Hancock, Jr., Jimmy L.. Supersonic aircraft with spike for controlling and reducing sonic boom. USP2004036698684.
  38. Henne, Preston A.; Howe, Donald C.; Wolz, Robert R.; Hancock, Jr., Jimmy L.. Supersonic aircraft with spike for controlling and reducing sonic boom. USP2014078789789.
  39. Bussom, Richard; McVeigh, Michael A.; Narducci, Robert P.; Zientek, Thomas A.. System and method for improved rotor tip performance. USP2010077757992.
  40. Bussom,Richard; McVeigh,Michael A.; Narducci,Robert P.; Zientek,Thomas A.. System and method for improved rotor tip performance. USP2007097264200.
  41. Archer John D. (Coopersdal ; Komatiepoort District Transvaal ZAX). Utilization of wind energy. USP1984014428711.
  42. Santos Jonathan (2902 Tapered La. Bowie MD 20715). Wing tip airfoils. USP1986064595160.
  43. Wright, Christopher; Chu, James K.; Himisch, Jan. Wing tip device. USP2015119193445.
  44. Wright, Christopher; Chu, James K.; Himisch, Jan. Wing tip device. USP2015129199727.
  45. Wright, Christopher; Chu, James K.; Himisch, Jan. Wing tip device. USP2015059033282.
  46. Zaman, AbuMuhammed A.. Wing tip device for an aircraft wing. USP2016129511850.
  47. Gratzer, Louis B.. Wing tip with optimum loading. USP2016079381999.
  48. Roman, Dino L.; Vassberg, John C.; Friedman, Douglas M.; Malachowski, Adam P.; Vegter, Christopher A.. Winglet system. USP2016059346537.
  49. Roman, Dino L.; Vassberg, John C.; Friedman, Douglas M.; Malachowski, Adam P.; Vegter, Christopher A.. Winglet system and method. USP2015129216817.
  50. Roman, Dino L.; Vassberg, John C.; Friedman, Douglas M.; Malachowski, Adam P.; Vegter, Christopher A.. Winglet system having upper and lower winglet. USP2016109463871.
  51. Malachowski, Adam P.; Chaney, Stephen R.; Ebner, Norman K.; LeDoux, Stephen T.. Winglets with recessed surfaces, and associated systems and methods. USP2012038128035.
  52. Patterson ; Jr. James C. (Newport News VA). Wingtip vortex turbine. USP1990044917332.