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High performance amphibious airplane

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64C-035/00    B64C-035/02   
미국특허분류(USC) 244/106 ; 244/105 ; 244/101 ; 114/272
출원번호 US-0785470 (1985-10-08)
발명자 / 주소
인용정보 피인용 횟수 : 24  인용 특허 : 1
초록
▼

An amphibious executive or business airplane, also having military application, possesses sponsons integrated with the airplane fuselage. The trailing end of the sponsons end in a sharp edge, thus eliminating the need for a hull or float step or venting. A channel is formed by the sponsons and the underside of the fuselage, which channel has a constant cross-section and produces a surface lift effect facilitating take-off and landing. A pair of keels beginning substantially aft of the center of gravity of the airplane provide directional stability on the...

대표
청구항
▼

In an amphibious aircraft, having a fuselage with a water-contacting hull, wings, tail assembly, and at least one engine, the improvement wherein said fuselage hull includes sponsons integral therewith extending outwardly on either side of the fuselage, wherein the underside of the combination fuselage and sponsons includes a substantially constant cross section inverted channel, the fuselage further including twin keels extending fore to aft on the underside of said hull, the inner surfaces of said twin keels being substantially extensions of the walls ...

이 특허에 인용된 특허 (1)

  1. Stark Terry R. (Newport NC). Boat construction and method. USP1985014495884.

이 특허를 인용한 특허 피인용횟수: 24

  1. James R. Lohse ; James G. Hutton. Amphibious aircraft. USP2002046367737.
  2. Lohse James R. ; Hutton James G.. Amphibious aircraft. USP2000096113028.
  3. Gioia G. Leonard. Amphibious aircraft with aerodynamic/hydrodynamic sponsons. USP2001096290174.
  4. Kreuzer, Peter; Schaber, Sven; Goldhahn, Iris. Arrangement of aerodynamic auxiliary surfaces for an aircraft. USP2015059038950.
  5. Boetto,Steven C.. Float retractable landing gear. USP2007037188804.
  6. Conners, Timothy R.; Henne, Preston A.; Howe, Donald C.. Isentropic compression inlet for supersonic aircraft. USP2016119482155.
  7. Conners, Timothy R.; Howe, Donald C.; Henne, Preston A.. Isentropic compression inlet for supersonic aircraft. USP2012128333076.
  8. Henne, Preston A.; Conners, Timothy R.; Howe, Donald C.. Isentropic compression inlet for supersonic aircraft. USP2012128327645.
  9. Henne, Preston A.; Conners, Timothy R.; Howe, Donald C.. Isentropic compression inlet for supersonic aircraft. USP2012108286434.
  10. Saiz, Manuel Munoz. Lifting arrangement for aircraft fuselages. USP2005106957792.
  11. Conners, Timothy R.. Low shock strength inlet. USP2013038393158.
  12. Conners, Timothy R.. Low shock strength inlet. USP2015059027583.
  13. Conners, Timothy R.. Low shock strength propulsion system. USP2014068739514.
  14. Conners, Timothy R.. Low shock strength propulsion system. USP2014078783039.
  15. Sarh, Branko; File, David J.. Morphing aircraft with telescopic lifting and control surfaces. USP2010097789343.
  16. Herzberger, Erick; Clavreul, Jean-Francois. Motorised airplane with mixed hydrodynamic and aerodynamic structure for take-off and landing on water, ground or snow. USP2011108038095.
  17. Gevers David E.. Multi-purpose aircraft. USP2000086098927.
  18. Gevers David E.. Multi-purpose aircraft. USP1998125850990.
  19. Henne, Preston A.; Conners, Timothy R.; Howe, Donald C.. Supersonic aircraft jet engine installation. USP2016059334801.
  20. Henne, Preston A.; Howe, Donald C.; Wolz, Robert R.; Hancock, Jr., Jimmy L.. Supersonic aircraft with spike for controlling and reducing sonic boom. USP2004036698684.
  21. Henne, Preston A.; Howe, Donald C.; Wolz, Robert R.; Hancock, Jr., Jimmy L.. Supersonic aircraft with spike for controlling and reducing sonic boom. USP2014078789789.
  22. Knowles, Gareth; Bird, Ross W.. Telescopic wing system. USP2004126834835.
  23. Milde, Jr., Karl F.. VTOL personal aircraft. USP2005056892979.
  24. Karkow, Jon; Hawkins, Kirk; Gionta, Matthew; Strand, Steen. Wingtip and sponson interaction on an amphibious aircraft. USP2012058177162.

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