The utility model discloses a UAV including tripod, tripod, folding mechanism and gas supply system, which is composed of two side stand on each side of the arm rod, between the two side arm rod welding welding rod with a lower cross bar, in addition, the first hinge seat and a hinge seat third welded on each side arm in the side bar, the bottom supporting rod is welded with two second hinge seat, folding mechanism is respectively connected with the first hinge seat, second seat and third seat hinge hinge, gas supply system is connected with a foot frame, a folding mechanism is composed of a cylinder, a connecting rod, connecting rod and connecting rod two, three wheels, cylinder hinged with the first hinge seat is hinged. The piston rod of the cylinder and a connecting rod, a connecting rod and the other end of the hinge seat second is hinged with a piston rod two connecting rod side of the cylinder, the other end of the wheel center and hinge, link the 31 ends of the connecting rod two The other end is hinged with the third hinged seat, and the air supply system is composed of an air nozzle and a flexible air pipe, which is used for avoiding the abrasion of the foot landing of the unmanned vehicle gliding and landing.
【技术实现步骤摘要】
一种无人机脚架
本技术属于无人机
,具体地说,本技术涉及一种无人机脚架。
技术介绍
现有的遥控无人机脚架,都是骨架焊接件,多数是在脚架上设有弹簧或者橡胶减振装置,来缓冲着陆时地面的冲击,目前的弹簧或者橡胶减振装置,主要还是在垂直起降时有用,当无人机在滑行过程中着陆时,很容易造成脚架底部的磨损损伤,为了避免脚架的磨损,希望设计的无人机脚架,既能实现垂直降落,又能实现滑行降落。
技术实现思路
本技术提供一种无人机脚架,目的是用来避免无人机滑行降落脚架的磨损。为了实现上述目的,本技术采取的技术方案为:一种无人机脚架,包括脚架、折叠机构和供气系统,其中每一侧的脚架由两根侧臂杆组成,在两根侧臂杆之间上部焊接有横撑杆,下部焊接有底撑杆,另外在每根侧臂杆上焊接有第一铰座和第三铰座,在底撑杆下侧焊接有两个第二铰座,所述折叠机构分别与第一铰座、第二铰座和第三铰座铰接,所述供气系统与脚架连接。优选的,所述折叠机构由气缸、连杆一、连杆二、连杆三和轮子组成,所述气缸与第一铰座铰接,气缸的活塞杆与连杆一的一端铰接,连杆一的另外一端与第二铰座铰接,所述连杆二一端与气缸的活塞杆铰接,另外一端与轮子中心铰接,所述连杆三一端与连杆二中间铰接,另外一端与第三铰座铰接。优选的,所述供气系统由气嘴和柔性气管组成,所述气嘴与脚架相通连接,所述柔性气管一端与气缸相通连接,另外一端与侧臂杆相通连接。采用以上技术方案的有益效果是:该无人机脚架,包括脚架、折叠机构和供气系统,其中每一侧的脚架由两根侧臂杆组成,在两根侧臂杆之间上部焊接有横撑杆,下部焊接有底撑杆,另外在每根侧臂杆上焊接有第一铰座和第三铰座,在底 ...
【技术保护点】
一种无人机脚架,其特征在于:包括脚架、折叠机构和供气系统,其中每一侧的脚架由两根侧臂杆组成,在两根侧臂杆之间上部焊接有横撑杆,下部焊接有底撑杆,另外在每根侧臂杆上焊接有第一铰座和第三铰座,在底撑杆下侧焊接有两个第二铰座,所述折叠机构分别与第一铰座、第二铰座和第三铰座铰接,所述供气系统与脚架连接。
【技术特征摘要】
1.一种无人机脚架,其特征在于:包括脚架、折叠机构和供气系统,其中每一侧的脚架由两根侧臂杆组成,在两根侧臂杆之间上部焊接有横撑杆,下部焊接有底撑杆,另外在每根侧臂杆上焊接有第一铰座和第三铰座,在底撑杆下侧焊接有两个第二铰座,所述折叠机构分别与第一铰座、第二铰座和第三铰座铰接,所述供气系统与脚架连接。2.根据权利要求1所述的一种无人机脚架,其特征在于:所述折叠机构由气缸、连杆一、连杆二、连...
【专利技术属性】
技术研发人员:吴龙秋,王会恩,臧楠,
申请(专利权)人:芜湖元一航空科技有限公司,
类型:新型
国别省市:安徽,34
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