According to the side wing synchronous separation structure, the wings on the two sides can be synchronously separated from the fuselage body, and a stable flight track is achieved. Wing removing springs are arranged between the wings on the two sides and the fuselage; the rotary screw rod is driven by a driving motor, a transmission gear is axially and vertically arranged above the rotary screw rod and is arranged on the periphery of a transmission drum, an axial stroke groove is formed in the transmission drum, a wing fixing column is arranged in the transmission drum, a stroke clamping shaft is arranged on the wing fixing column and slides in the stroke groove, and the wing fixing column and the stroke clamping shaft are connected through a connecting rod. The rotating roller is further provided with an open groove corresponding to the stroke clamping shaft and used for sliding of the stroke clamping shaft. The rotating screw drives the transmission gear, the transmission gear drives the transmission roller to rotate, pressurization fixing or wing disengaging control is achieved, and when the stroke clamping shaft moves to the position corresponding to the opening groove, the wings are synchronously disengaged through the springs arranged between the wings and the fuselage. Meanwhile, the wings on the two sides are mounted or separated, and the flight attitude control is extremely stable and reliable.
本发明提供一种可同步将两侧机翼脱离机身本体的、实现飞行轨道稳定的侧翼同步分离结构。两侧的机翼与机身之间设有脱翼弹簧;还包括有旋转螺杆,旋转螺杆由驱动电机驱动,旋转螺杆上方轴向垂直设置有传动齿轮并设于一传动滚筒外周,传动滚筒中设有轴向行程凹槽,所述传动滚筒中设有机翼固定柱,机翼固定柱上设有行程卡轴,行程卡轴滑动于所述行程凹槽中,转动滚筒上还设有与行程卡轴相对应的开口槽,用于行程卡轴的滑动;旋转螺杆驱动传动齿轮,传动齿轮带动传动滚筒旋转,实现加压固定或脱翼控制,行程卡轴行到与开口槽对应位置时,由机翼与机身之间设置的弹簧同步脱翼。同时实现两侧机翼的安装或脱离,飞行姿态控制极其稳定可靠。
Side wing synchronous separation structure
侧翼同步分离结构
2023-07-07
Patent
Electronic Resource
Chinese
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