The invention discloses an aircraft nose cone. The aircraft nose cone comprises a cone section, a first connecting part, a second connecting part and a movable part. The plurality of cone sections are connected in sequence to form a nose cone; a plurality of first connecting parts and a plurality of second connecting parts are arranged on every two adjacent cone sections at intervals in the circumferential direction of the cone sections, and the first connecting parts and the second connecting parts are in one-to-one correspondence; one end of the movable part is hinged with the first connecting part, and the other end of the movable part is connected with the second connecting part through a universal joint; wherein the movable part is suitable for deforming to drive the two adjacent cone sections to move relatively so as to drive the nose cone to deform. According to the aircraft nose cone, under the condition that the structure is simplified, the deformation stability and flexibility of the nose cone can be guaranteed, and any-angle deformation of the nose cone is achieved.
本发明公开了一种飞行器头锥,飞行器头锥包括锥节、第一连接部、第二连接部和活动部。锥节设置有多个,多个锥节顺序连接以形成头锥;相邻的两个锥节上分别设置有第一连接部和第二连接部,第一连接部与第二连接部构造为在锥节周向上间隔设置且一一对应的多个;活动部的一端与第一连接部铰链连接,活动部的另一端与第二连接部通过万向节连接;其中活动部适于形变以驱动相邻的两个锥节相对移动以驱动头锥变形。本发明的飞行器头锥能够在结构精简的情况下保证头锥变形的稳定性和灵活性,实现头锥任意角度变形。
Aircraft nose cone
飞行器头锥
2025-03-28
Patent
Electronic Resource
Chinese
IPC: | B64C AEROPLANES , Flugzeuge |
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