专利名称：SHORT TAKE-OFF AIRCRAFT发明人：Cazals Olivier,Koch Alexander申请号：US12178711申请日：20080724
公开号：US20090026308A1公开日：20090129
摘要：An aircraft capable of making short takeoffs and landings includes essentially afuselage, a wing secured to the fuselage, a front horizontal stabilizer secured to thefuselage on the front end of the fuselage and at least two jet engines for propulsion.According to the architecture proposed, the propulsion engines are arranged side byside above the fuselage in a rear part of the fuselage with a width at least equal to thewidth of the propulsion group, a fuselage flap device is arranged in the back of thefuselage so that the fuselage flaps adopt at least a position in which the flaps areconsiderably in a horizontal plane and take at least a high-lift position in which the flapsare turned downward in such a way that the blast created by the jet engines is channeledtowards the top surface of the fuselage flaps to induce a blowing effect.
申请人：Cazals Olivier,Koch Alexander
地址：Daux FR,Eppstein DE
国籍：FR,DE
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