Stol/vtol free wing aircraft with articulated tail boom

Details Stol/vtol free wing aircraft with articulated tail boom Stol/vtol free wing aircraft with articulated tail boom

B - Operations, Transporting

64

C

B64C 29/02 (2006.01) B64C 3/38 (2006.01) B64C 29/00 (2006.01) B64C 39/02 (2006.01) B64C 39/04 (2006.01)

Patent

CA 2154160

A VTOL/STOL free wing aircraft includes a free wing having wings on opposite sides of a fuselage connected to one another respectively adjacent fixed wing inboard or center root sections fixedly attached to the fuselage for free rotation about a spanwise axis. Horizontal and vertical tail surfaces are located at the rear end of a boom assembly rotatably connected to the fuselage. A gearing or screw rod arrangement controlled by the pilot or remote control operator selectively relatively pivots the fuselage in relation to the tail boom assembly to enable the fuselage to assume a tilted or nose up configuration to enable VTOL/STOL flight.

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