FIELD: transport.
SUBSTANCE: version of every hybrid aircraft consists of fuselage, turboprop and wings. First version incorporates bearing devices arranged on both sides of fuselage and consisting of aircraft transverse wing root with engine fan ahead of front edge at fuselage nose and wings arranged there behind, several wings at top or bottom side, along fuselage. Second version incorporates top and bottom pairs of cantilever straight wings with spacing between pairs for gas-air flow from engine nozzles. Turboprop et engine incorporates shaped confuser and diffuser sections of propfan ring inner surface. Wing versions feature availability of bearing section and airfoil section. Methods comprises using said aircraft and engine.
EFFECT: higher safety, lower costs.
13 cl, 8 dwg
Title |
Year |
Author |
Number |
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|
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