Tandem powered power tilting aircraft - june 2002

摘要

An aircraft with a long body 1 which has a forward end 2 and an aft end 3 , which is able to achieve vertical take-off by means of a tiltable rotor and blade assembly 4 at the forward part of the aircraft and a tiltable turbojet 19 at the rear of the aircraft. The rotor and blade assembly is rotated by an engine assembly 8 , with the engine assembly, the rotor and blades all positioned on top a multi-directional tilt enabling joint 9 . The tubojet is fitted to a multi-directional tilt enabling joint 27 to allow control of lateral movement of the aircraft as well as providing vertical lift and forward propulsion during forward flight.