摘要：【中文】本发明涉及一种舰载小型固定翼无人机起飞姿态调整装置，包括传感器A、传感器B、横滚姿态调整装置、能源供给装置和控制器，通过传感器A、传感器B测量的角度及角速度信息传送给控制器，控制器与横滚姿态调整装置能够将小型固定翼无人机在舰载环境下起飞时横滚角度和角速度控制在一定范围内，减小起控后小型固定翼无人机控制难度，提高小型固定翼无人机在舰载环境下起飞的安全性，避免坠机事故发生。 【EN】The invention relates to a take-off attitude adjusting device of a ship-borne small-sized fixed-wing unmanned aerial vehicle, which comprises a sensor A, a sensor B, a roll attitude adjusting device, an energy supply device and a controller, wherein angle and angular speed information measured by the sensor A and the sensor B is transmitted to the controller, and the controller and the roll attitude adjusting device can control the roll angle and the angular speed of the small-sized fixed-wing unmanned aerial vehicle in a certain range when the small-sized fixed-wing unmanned aerial vehicle takes off in a ship-borne environment, so that the control difficulty of the small-sized fixed-wing unmanned aerial vehicle after being started and controlled is reduced, the take-off safety of the small-sized fixed-wing unmanned aerial vehicle in the ship-borne environment is.

摘要：【中文】本发明涉及一种弹射式无人机用的螺旋桨折叠机构,包括桨叶、桨叶铰链、桨榖、轴套、连杆、推力轴承、离合器，本发明利用弹簧弹力自动打开螺旋桨，同时利用螺旋桨离合器及其联动装置在螺旋桨折叠时断开发动机与螺旋桨的连接、在螺旋桨打开后通过联动装置带动螺旋桨离合器闭合从而连接发动机为无人机提供推力的机构。 【EN】The invention relates to a propeller folding mechanism for an ejection type unmanned aerial vehicle, which comprises a propeller blade, a propeller blade hinge, a propeller hub, a shaft sleeve, a connecting rod, a thrust bearing and a clutch.

摘要：【中文】本发明涉及一种筒式无人机，包括机身、上机翼、下机翼、V型尾翼、动力总成、可折叠螺旋桨组件，通过过上机翼、下机翼布局及V型尾翼的布置，能适应多种气候及恶劣条件，具有巡航状态气动特性好的特点；同时通过各机翼的折叠设置，在机身底部、顶部及尾部切平来放置对应的机翼，使得其筒装状态占用空间小、重量轻，既可由单兵背负携带，也可集群发射，操作简单。 【EN】The invention relates to a barrel type unmanned aerial vehicle, which comprises a vehicle body, an upper wing, a lower wing, a V-shaped empennage, a power assembly and a foldable propeller assembly, wherein the vehicle body can adapt to various climates and severe conditions by the arrangement of the upper wing and the lower wing and the arrangement of the V-shaped empennage, and has the characteristic of good pneumatic characteristic in a cruising state; meanwhile, the corresponding wings are flatly arranged at the bottom, the top and the tail of the body through the folding arrangement of the wings, so that the barrel-mounted aircraft has small occupied space and light weight, can be carried by a single soldier on the back, can be launched in a cluster, and is simple to operate.

摘要：【中文】本发明涉及一种筒射无人机机翼折叠展开机构，包括上接头、下接头、固定组件、轴承、弹性件、锁定机构、驱动机构，通过弹性件实现机翼的展开与折叠，并通过锁定机构与锁定槽的配合，能实现机翼的展开折叠锁定，提高了飞行的安全性，并通过驱动机构实现机翼折叠与展开的自动控制，机构简单可靠，成本低。 【EN】The invention relates to a wing folding and unfolding mechanism of a tube-shot unmanned aerial vehicle, which comprises an upper joint, a lower joint, a fixing assembly, a bearing, an elastic piece, a locking mechanism and a driving mechanism, wherein the wing is unfolded and folded through the elastic piece, the wing can be unfolded, folded and locked through the matching of the locking mechanism and a locking groove, the safety of flight is improved, the automatic control of the folding and unfolding of the wing is realized through the driving mechanism, and the mechanism is simple and reliable and has low cost.