Aerospace variant aircraft with wing folding function and launching system thereof

• Main Authors: ZHANG JUNWEI, JIN LU, HU ANJUN, QI YIFAN, XU JIEWEI, TIAN DAKE, SHI ZUWEI, SONG YUQUN, YANG XIHUA, ZHAO BINGFENG
• Format: Patent
• Language: Chinese; English
• Published: 05.08.2022
• Subjects: AIRCRAFT; AVIATION; COSMONAUTICS; PERFORMING OPERATIONS; TRANSPORTING; VEHICLES OR EQUIPMENT THEREFOR

The invention belongs to the technical field of aerospace aircrafts, and particularly relates to an aerospace variant aircraft with a wing folding function and a launching system of the aerospace variant aircraft. According to the technical scheme, the aerospace morphing aircraft with the wing folding function comprises a fuselage, inner wing sections, morphing wing sections, outer wing sections and a vertical tail wing, the vertical tail wing is fixedly installed at the upper end of the tail of the central axis of the fuselage, and the two inner wing sections are symmetrically arranged on the left side and the right side of the middle of the fuselage respectively; one end of the deformation wing section is fixedly connected with the inner wing section, and the other end of the deformation wing section is fixedly connected with the outer wing section; the outer wing section and the inner wing section are in a trapezoid shape after being projected in a plane, and the deformation wing section is in a rectangula