The present embodiment relates to an aircraft (100) having an aircraft structure, the aircraft comprising a radar radome opening kinematics (200) and a radar radome housing (112), the radar radome housing (112) being adapted to enclose a device (115) in a nose region (110) of the aircraft (100) in a closed position. The radome opening kinematics (200) may move the radome housing (112) between a closed position and an open position, and vice versa. The radome opening kinematics 200 may include a guide rail (210) attached to the radome housing (112) and at least three rollers (230) attached to the aircraft structure (103), where a first roller (230a) and a second roller (230b) are disposed on opposite sides of the guide rail (210), and where the second roller (230b) and a third roller (230c) are disposed on the same side of the guide rail (210).
本实施方式涉及一种具有飞行器结构的飞行器(100),该飞行器包括雷达天线罩盖打开运动学件(200)和雷达天线罩盖壳体(112),该雷达天线罩盖壳体(112)适于在闭合位置将设备(115)封闭在飞行器(100)的机头区域(110)中。雷达天线罩盖打开运动学件(200)可以使雷达天线罩盖壳体(112)在闭合位置与打开位置之间运动,反之亦然。雷达天线罩盖打开运动学件200可包括附接至雷达天线罩盖壳体(112)的导向导轨(210)以及附接至飞行器结构(103)的至少三个滚轮(230),其中第一滚轮(230a)和第二滚轮(230b)设置在导向导轨(210)的相对两侧,并且其中第二滚轮(230b)和第三滚轮(230c)设置在导向导轨(210)的同一侧。
Radar radome housing and opening kinematics
雷达天线罩盖壳体和打开运动学件
2022-05-06
Patent
Electronic Resource
Chinese