固定翼飛行器

專利類型

發明

專利國別 (專利申請國家)

中華民國

專利申請案號

105125435

專利證號

I 605978

專利獲證名稱

固定翼飛行器

專利所屬機關 (申請機關)

元智大學

獲證日期

2017/11/21

技術說明

一種固定翼飛行器，其包括一翼身融合機體、一飛行組件及一控制模組。翼身融合機體包括一機身部及兩個由所述機身部兩相反側延伸的翼部。飛行組件具有一固定部、由固定部呈放射狀延伸的多個支撐臂、多個旋翼以及多個驅動單元。飛行組件通過固定部裝設於翼身融合機體前端。每一個支撐臂的長度小於每一個所述翼部的長度。多個旋翼分別設置於多個支撐臂的末端，每一個旋翼與對應的驅動單元連接，並由對應的驅動單元驅動旋轉。控制模組設置於機身部內，並電性連接於飛行組件，以控制每一驅動單元驅動對應的旋翼的旋轉速度。 A fixed-wing aircraft is provided in the instant disclosure. The fixed-wing aircraft includes a blended wing body, a fly assembly, and a control module. The blended wing body includes a main portion and a couple of wing portions respectively extending from two opposite sides of the main portion. The fly assembly includes a fixing portion, a plurality of supporting arms extending radially outwards from the fixing portion, a plurality of propellers, and a plurality of driving units. The fly assembly is fixed on the front side of the blend wing body through the fixing portion. Each supporting arm has a length less than that of the wing portion. The propellers are respectively configured to the ends of the supporting arms and driven by the corresponding driving unit. The control module configured in the main portion is electrically connected to the fly assembly to control the driving units to drive the propellers.

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