公开(公告)号：US20140008487A1

公开(公告)日：2014-01-09

申请号：US13710323

申请日：2012-12-10

Applicant: Singapore Technologies Aerospace LTD

Inventor： Yong Wee Liu ,  Hian Beng Kek

IPC: B64C3/56

CPC classification number: B64C3/56 ,  B64C39/024 ,  B64C2201/102

Abstract: Disclosed herein is a collapsible wing assembly of an unmanned aerial vehicle (UAV) and a method of locking and unlocking the collapsible wing assembly of an unmanned aerial vehicle (UAV). The collapsible wing assembly comprising a centre wing adapted to be attached to the fuselage; and a pair of outboard wings, wherein each of the outboard edges of the centre wing comprises a first attachment structure, and each of the inboard edges of the outboard wings comprises a second attachment structure, wherein the first attachment structure is operable to engage with the second attachment structure and displace the second attachment structure to a captive position towards the trailing edge of the centre wing.

Abstract translation: 本文公开了一种无人飞行器（UAV）的可折叠翼组件以及锁定和解锁无人机（UAV）的可折叠翼组件的方法。 可折叠翼组件包括适于附接到机身的中心翼; 以及一对外侧翼，其中所述中心翼的所述外侧边缘中的每一个包括第一附接结构，并且所述外侧翼的每个内侧边缘包括第二附接结构，其中所述第一附接结构可操作以与 第二附接结构，并且使第二附接结构朝向中心翼的后缘移动到捕获位置。

公开(公告)号：US09150301B2

公开(公告)日：2015-10-06

申请号：US13710323

申请日：2012-12-10

Applicant: SINGAPORE TECHNOLOGIES AEROSPACE LTD

Inventor： Yong Wee Liu ,  Hian Beng Kek

IPC: B64C3/56 ,  B64C39/02

CPC classification number: B64C3/56 ,  B64C39/024 ,  B64C2201/102

Abstract: Disclosed herein is a collapsible wing assembly of an unmanned aerial vehicle (UAV) and a method of locking and unlocking the collapsible wing assembly of an unmanned aerial vehicle (UAV). The collapsible wing assembly comprising a center wing adapted to be attached to the fuselage; and a pair of outboard wings, wherein each of the outboard edges of the center wing comprises a first attachment structure, and each of the inboard edges of the outboard wings comprises a second attachment structure, wherein the first attachment structure is operable to engage with the second attachment structure and displace the second attachment structure to a captive position towards the trailing edge of the center wing.

Abstract translation: 本文公开了一种无人飞行器（UAV）的可折叠翼组件以及锁定和解锁无人机（UAV）的可折叠翼组件的方法。 可折叠翼组件包括适于附接到机身的中心翼; 以及一对外侧翼，其中所述中心翼的所述外侧边缘中的每一个包括第一附接结构，并且所述外侧翼的每个内侧边缘包括第二附接结构，其中所述第一附接结构可操作以与 第二附接结构，并且使第二附接结构朝着中心翼的后缘移动到捕获位置。