发明名称 SPIN RESISTANT AIRCRAFT CONFIGURATION
摘要 A configuration and system for rendering an aircraft spin resistant is disclosed. Resistance of the aircraft to spinning is accomplished by constraining a stall cell to a wing region (220) adjacent to the fuselage and distant from the wing tip (210). Wing features that facilitate this constraint include but are not limited to one or more cuffs (215), stall strips (320), vortex generators (630), wing twists (510-550), wing sweeps and horizontal stabilizers. Alone or in combination, aircraft configuration features embodied by the present invention render the aircraft spin resistant by constraining the stall cell, which allows control surfaces of the aircraft to remain operational to control the aircraft.
申请公布号 WO2014074182(A1) 申请公布日期 2014.05.15
申请号 WO2013US51355 申请日期 2013.07.19
申请人 ICON AIRCRAFT, INC.;GIONTA, MATTHEW;KARKOW, JON;RONCZ, JOHN;KOEHLER, DIETER;FOX, LEN;LEDNICER, DAVID 发明人 GIONTA, MATTHEW;KARKOW, JON;RONCZ, JOHN;KOEHLER, DIETER
分类号 B64C3/10;B64C23/06;B64C35/00 主分类号 B64C3/10
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