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一种中型固定翼无人机机身结构
InventionActive
4Claims · 2 independent
§ Ⅰ
Dossier Overview
Applicant
株洲西康尼克新材料有限公司
Inventor
姜永正; 周宇峰; 马俊飞; 杨大炼
IPC Classification
B64U 20/70 (2023.01)B64U 20/60 (2023.01)B64U 10/25 (2023.01)
本发明涉及无人飞行器装配领域，具体涉及一种中型固定翼无人机机身结构，包括前机头、中机身和后机尾，中机身骨架为由桁架和框构成的笼式结构，前机头与中机身盘式对接。任务载荷安装在前机头，动力系统安装在后机尾，机翼通过锁销机构安装在中机身后半部，起落架安装在起落架安装框上。本发明在满足强度和重量要求的同时，保证了较低的制造成本，主要部件安装的便捷性。
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