Stabilized tilt rotor aircraft
OwnerGeorge Philip Tharisayiinventor
Life of this patent
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Abstract
The purpose of this invention is to design and construct Stabilized Tilt Rotor Aircraft (STRA). Stabilized Tilt Rotor Aircraft is a subsonic aircraft with tilt rotors assisted by tilting louvers and tail rotors powered by the battery charged by the rotor engines. During take off and landing when operational speeds are below stall, stability is provided by the tilting rotors, the tilting louvers and the battery powered tail rotors.
Claims10
A Stabilized Tilt Rotor Aircraft (STRA), comprising of a fuselage, a main wing, a horizontal tail, a vertical tail, a cockpit, front and back landing gears, a rudder, pair of elevators, pair of ailerons, two tilt rotors mounted on the main wing, one rotor to the left and the second rotor to the right of the fuselage of the aircraft, each tilt rotor having variable pitch and having one set of upper louvers consisting of one or more louvers parallel to the fuselage and each tilt rotor having one set of lower louvers consisting of one or more louvers parallel to main wing.
Dependencies are inferred from the claim text.