| 摘要 |
VTOL amphibious aircraft comprising two fuselages spaced apart to enable the placement of single center wing and split ailerons, engine and rotor or fan such that they may be rotated from vertical flight to horizontal flight and back while center wing ailerons counter rotor torque. Out board wings remain fixed and the twin fuselages provide buoyant hulls to facilitate water landings. Standard aircraft components are employed such as a vertical tails and horizontal stabilizers. |
