The invention belongs to the technical field of aviation, and discloses an array plane conformal with an aircraft skin, the array plane comprises a rectification wave-transparent cover and an annular electronic array plane, the rectification wave-transparent cover and the annular electronic array plane are both of a semicircular annular structure, the rectification wave-transparent cover is a cover body with rectification and wave-transparent functions, and the annular electronic array plane is of a rectangular structure. The annular electronic array planes are electronic array planes composed of composite materials and integrated electronic elements, the two annular electronic array planes are folded to form the electronic array plane with the 360-degree radiation angle of the airplane, and the two rectification wave-transparent covers are folded outside the two annular electronic array planes. An air inlet and an air outlet are formed in the front end and the rear end of the rectification wave-transparent cover in the course of an airplane respectively, an air cooling air inlet cover and an air cooling exhaust port cover are arranged outside the air inlet and the air outlet respectively, and the air cooling air inlet cover and the air cooling exhaust port cover are opened in the mode that the outer sides are ejected out to be opened and then slide along one side of a cover body of the rectification wave-transparent cover. An air cooling channel is arranged between the rectification wave-transparent cover and the annular electronic array plane. An electronic array plane structure platform is omitted, and the external size is reduced.

    本发明属于航空技术领域,公开了一种与飞机蒙皮共形的阵面,包括整流透波罩和环形电子阵面,整流透波罩和环形电子阵面均为半圆的环形结构,整流透波罩为具有整流和透波功能的罩体,环形电子阵面为复合材料和集成电子元件组成的电子阵面,两个环形电子阵面合拢组成飞机的360°辐射角度的电子阵面,两个整流透波罩合拢在两个环形电子阵面的外部;整流透波罩在飞机航向的前端和后端分别设有进气口和出气口,进气口和出气口外分别设有风冷进气口盖和风冷排气口盖,风冷进气口盖和风冷排气口盖为外侧顶出打开再沿整流透波罩的罩体一侧滑动的打开方式,整流透波罩与环形电子阵面之间具有风冷通道。本发明取消了电子阵面结构平台,降低外部尺寸。


    Access

    Download


    Export, share and cite



    Title :

    Array plane conformal with aircraft skin and aircraft


    Additional title:

    一种与飞机蒙皮共形的阵面及飞机


    Contributors:
    FANG JIN (author) / XIE RUIPENG (author) / WU YANPING (author) / REN KAIXUN (author)

    Publication date :

    2024-03-05


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / H01Q Antennen , ANTENNAS, i.e. RADIO AERIALS / H05K PRINTED CIRCUITS , Gedruckte Schaltungen



    Engine conformal jet aircraft

    ZHANG YAN / CHENG XIANGYU | European Patent Office | 2023

    Free access

    AIRCRAFT PLUG-PLANE AIRCRAFT

    PANFILOV ALEKSANDR ALEKSANDROVICH | European Patent Office | 2018

    Free access

    Outer surface conformal system of fixed-wing aircraft and aircraft

    ZHANG GONG | European Patent Office | 2024

    Free access

    LIFTING PLANE OF AIRCRAFT AND AIRCRAFT

    GONZALEZ GOZALBO ALFONSO | European Patent Office | 2021

    Free access

    CONFORMAL SURFACE HEAT EXCHANGER FOR AIRCRAFT

    CAMPBELL KEITH ALAN / STORAGE MICHAEL RALPH / MCQUEEN DENNIS ALAN et al. | European Patent Office | 2016

    Free access