Aircraft with wing and cabin section heat insulation structure

• Main Authors: LIU QING, HU SHANGANG, ZOU TIANPING, WANG BOZHE, HU CHI, TAN YOUDE, WANG QIAOYUN
• Format: Patent
• Language: Chinese; English
• Published: 21.01.2022
• Subjects: AEROPLANES; AIRCRAFT; AVIATION; COSMONAUTICS; HELICOPTERS; PERFORMING OPERATIONS; TRANSPORTING

The invention discloses an aircraft with wing and cabin section heat insulation structures, and relates to the technical field of high-speed aircraft heat protection, the aircraft comprises a cabin section, and a cabin section mounting hole is formed in the cabin section; wings, wherein wing joint devices are arranged on the wing, and the wings are mounted on the cabin section through the wing joint devices; and a thermal protection assembly which comprises a cabin thermal protection assembly arranged between the end face of the wing joint device and the mounting hole, and a wing thermal protection assembly arranged between the side face of the wing joint device and the side wall of the mounting hole. According to the aircraft, the applicant arranges the heat-proof structure which completely covers the connecting part of the wing and the cabin section at the connecting part of the wing and the cabin section, so that the heat transfer efficiency of the high-temperature wing is effectively reduced, and a system