A deflector for upwardly re-directing the normally horizontal exhaust blast emitted from the exhaust nozzle of a reaction propulsive engine comprising: a supporting frame including a plurality of rigid laterally spaced side standards, each standard including an upright front member and an inclined rear member, said members being rigidly secured together near their upper ends; a plurality of elongated, spaced, superposed, horizontally disposed jet blast deflecting vanes bridging the respective spaces between said inclined rear members, all of said vanes having a concave upper surface and arranged with their forward edges at a lower elevation than their respective rear edges; and means rigidly securing the opposite ends of each vane between and to respectively adjacent inclined rear members.
U.S. Patent Specifications
Aircraft Engineering and Aerospace Technology ; 30 , 8 ; 250
01.08.1958
1 pages
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
Emerald Group Publishing | 1960
Emerald Group Publishing | 1956
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