The invention relates to a rear single-channel fan
composite wing aircraft with double-channel fan composite auxiliary wings, which is composed of a rear single-channel fan
composite wing aircraft, achannel fan thrust self-powering composite auxiliary wing and a manned cabin installed on both sides of the rear single-channel fan
composite wing aircraft. A aft-single-channel fan-type composite-wing aircraft comprise a body, a composite lift wing fixedly arrange on both sides of that body, and a
propeller; Wherein, the
airframe is arranged as a
deck platform; The compound lift wing has built-inself-enclosed duct fan and wing hinge on the outside of the compound lift wing. A self-enclosed ducted fan is arranged in the ducted fan thrust self-powered composite auxiliary wing, and one or bothsides of the ducted fan thrust self-powered composite auxiliary wing are provided with an electro-hydraulic
air interface and a wing hinge, which are movably connected with the composite lifting wingthrough the wing hinge, and the manned cabin is installed below the body. The invention not only has the characteristics of short take-off and landing distance, high flying speed, high wing structuralstrength,
energy storage capability of the wing, low flying
energy consumption, long air stagnation time and the like, but also has the functions of a large-area composite lifting wing, which can play the role of a
glider in an emergency situation, greatly improves the safety of an aircraft, and guarantees the safety of personnel and materials.