Duct means for aircraft
作者： Ivan Ray British Aerospace P.L.C. Yates
DOI:
关键词: Aerospace engineering 、 Engineering 、 Fluid pressure 、 Duct (flow)
摘要: 57 A duct 11 for an aircraft comprises a flexible panel member 18 which is normally held in non-fluid conducting condition adjacent the surface of body by biass tension means 12, 13, so as to define substantially continuous surface. On introduction fluid pressure between and body, inflated overcome expand relatively large cross-sectional area, upstanding from surrounding regions.
lens.org 参考文章(10)
John R Clifton, Auxiliary fuel cell ,(1953)
Brennan William M, Nelson Bud D, Retraction system for double pod air cushion landing gear system ,(1973)
Charles L. Holland, George B. Nicoloff, Inflatable air inlet duct ,(1977)
Dan J. Rundell, James E. Johnson, Onofre T. M. Castells, Auxiliary lift propulsion system with oversized front fan ,(1977)
Walter R. Burhans, James L. Ciccarello, Charles H. Stumpf, Aircraft collapsible fuel tank ,(1978)
A. Rhodes, C.M. British Aerospace Plc. Garside, Fuel storage means ,(1986)
Eggington Wilfred James, Earl Thomas Desmond, Aircraft with ground effect type landing gear ,(1965)
Lee Shao-Tang, Aircraft with inflatable landing gear ,(1965)
Hermann Dipl-Ing Bruno, Hagen Dr Hermann, Fluggeraet mit Strahltriebwerk und Nachbrennkammer ,(1960)
Marmier Lionnel-Pierre-Alexa D, Appareil permettant de vider instantanément l'essence du réservoir d'un avion en cas d'incendie ,(1927)