Wing box and aircraft

• Main Authors: FENG XIAO, DU BAIYU, CHEN YUANQIANG, ZHANG ZEPENG, YUAN LAOHU, WU BIAO, ZHANG DEYUAN
• Format: Patent
• Language: Chinese; English
• Published: 15.06.2021
• Subjects: AIRCRAFT; AVIATION; COSMONAUTICS; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING ORREPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLYADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFTCOMPONENTS, NOT OTHERWISE PROVIDED FOR; PERFORMING OPERATIONS; TRANSPORTING

The invention provides a wing box and an aircraft, the wing box comprises a wing box body, a first positioning plate, a second positioning plate, a wing displacement control mechanism, a sweep angle control mechanism and a dihedral angle control mechanism, the first positioning plate and the second positioning plate are arranged in the wing box body; and the sweep angle control mechanism and the dihedral angle control mechanism are arranged on the wing displacement control mechanism, and the wing displacement control mechanism is arranged between the first positioning plate and the second positioning plate. The aircraft comprises the wing box. The problems that according to scaling verification, an aircraft flies unstably on the edge of an envelope, and the number of parameter types of a free wing aircraft is small are solved. 本申请提供一种翼盒及飞行器，包括：翼盒本体，第一定位板，第二定位板，机翼位移操纵机构，掠角操纵机构以及反角操纵机构，所述第一定位板与所述第二定位板设置在所述翼盒本体内部，所述掠角操纵机构与所述反角操纵机构设置在所述机翼位移操纵机构上，所述机翼位移操纵机构设置在所述第一定位板与所述第二定位板之间，一种飞行器，包括上述所述的翼盒，以解决缩比验证飞行器飞行在包线的边缘飞行不