The invention belongs to the technical field of aviation, and discloses an aircraft fuselage elevated electronic array surface configuration device which comprises an in-cabin assembly, an out-cabin assembly and a ship-shaped assembly, the in-cabin assembly is arranged in a fuselage skin of an aircraft, the in-cabin assembly transmits structural force above to a floor cross beam and the bottom of the aircraft, and the ship-shaped assembly is connected with the in-cabin assembly. The upper portion of the in-cabin assembly is connected with the out-cabin assembly, the out-cabin assembly is of a cuboid structure in course layout, and the front end and the rear end of the out-cabin assembly are provided with a front edge and a rear edge. The upper end of the outboard assembly is connected with the ship-shaped assembly, the ship-shaped assembly is integrally ship-shaped and is symmetrical front, back, left and right, and electronic array planes are arranged in the front, back, left, right and top of the ship-shaped assembly; and electronic array planes are also arranged in the left side and the right side of the outboard assembly. The electronic array plane is installed at the high position outside the fuselage, the electronic array plane is lifted, and the problem that the electronic array plane is blocked by aircraft structures such as fuselage, wings and empennages is solved.
本发明属于航空技术领域,公开了一种飞机机身高架电子阵面构型装置,包括舱内组合件、舱外组合件和船型组合件,在飞机的机身蒙皮内布置舱内组合件,舱内组合件将上方的结构力传递给飞机的地板横梁与飞机底部,舱内组合件上方连接舱外组合件,舱外组合件为航向布局的长方体结构,舱外组合件的前端和后端设有前缘和后缘;舱外组合件的上端连接船型组合件,船型组合件整体为船型,前后左右对称,船型组合件的前后左右和顶部内均设有电子阵面;舱外组合件的左右两侧内也设有电子阵面。本发明通过将电子阵面安装于机身之外高处,将电子阵面高举,减小机身机翼尾翼等飞机结构对电子阵面遮挡等问题。
Aircraft fuselage elevated electronic array surface configuration device
一种飞机机身高架电子阵面构型装置
2024-02-06
Patent
Electronic Resource
Chinese
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
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