A contra-rotating rotorcraft with fixed wings and a foldable tail
An aircraft and empennage technology, applied in the field of contra-rotating dual-rotor aircraft, can solve the problems of low load, short range, high fuel consumption, etc., and achieve the effect of large load, long range and heavy load
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[0062]The technical scheme of the present invention stipulates: along the aircraft of the present invention, from the nose to the tail is the longitudinal axis of the aircraft of the present invention. Along the aircraft of the present invention, from the left wing to the right wing is the horizontal axis of the aircraft of the present invention. Along the aircraft of the present invention, from the nose to the belly is the vertical axis of the aircraft of the present invention. The three axes are perpendicular to each other, and the intersection point of the three axes is the design center of gravity of the aircraft. Such as Figure 1 The power distribution system of the present invention is as Figure four shown. The engine transmits the torque to the main drive gear 18, the main drive gear 18, the drive gear 18 meshes with the differential gear 19, drives the differential main drive gear 19, and the differential main drive gear 19 is mounted on the differential case , t...
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