CN218578020U - A miniature flapping wing device capable of controlling both wings separately - Google Patents
A miniature flapping wing device capable of controlling both wings separately Download PDFInfo
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- CN218578020U CN218578020U CN202220784770.XU CN202220784770U CN218578020U CN 218578020 U CN218578020 U CN 218578020U CN 202220784770 U CN202220784770 U CN 202220784770U CN 218578020 U CN218578020 U CN 218578020U
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Abstract
Description
技术领域technical field
本实用新型涉及微型扑翼飞行器领域,具体来说,是一种可实现双翼分别控制的微型扑翼装置。The utility model relates to the field of miniature flapping-wing aircraft, in particular to a miniature flapping-wing device capable of separately controlling two wings.
背景技术Background technique
微型扑翼飞行器有相对于固定翼飞行器特有的重量轻、体积小、机动性强、飞行效率高、反侦察能力强等特点,使其无论在军事方面还是民用领域都有广泛的应用前景,微型扑翼飞行器适于在较小的空间内飞行,完成观测、侦察、通讯、辅助救援等任务。尽管微型扑翼飞行器模仿昆虫和鸟类翅膀运动,但尺寸明显大于昆虫或鸟类,受技术发展的限制,微型扑翼飞行器也不能像鸟类和昆虫一样完成较为复杂的飞行运动。Compared with fixed-wing aircraft, miniature flapping-wing aircraft has the characteristics of light weight, small size, strong maneuverability, high flight efficiency, and strong anti-reconnaissance capabilities, making it have a wide range of application prospects in both military and civilian fields. The flapping-wing aircraft is suitable for flying in a small space to complete tasks such as observation, reconnaissance, communication, and auxiliary rescue. Although micro-orthopting-wing aircraft imitate the wing movements of insects and birds, their size is significantly larger than that of insects or birds. Due to the limitation of technological development, micro-orthoping-wing aircraft cannot complete more complex flight movements like birds and insects.
现有微型扑翼飞行器大多采用一个驱动电机驱动一对或多对翅膀,实现翅膀的同时拍动,此种驱动方式易于操控,较容易获得较高的精度,在一般的飞行环境中也可顺利飞行。Most of the existing micro-flapping-wing aircraft use a drive motor to drive one or more pairs of wings to achieve simultaneous flapping of the wings. This driving method is easy to control, and it is easier to obtain higher precision. It can also be used smoothly in the general flying environment. flight.
但在较为复杂的飞行环境中,微型扑翼飞行器顺利飞行较为困难,若能实现对两个翅膀的分别控制,则在复杂的飞行环境中能实现更好的飞行。However, in a relatively complex flight environment, it is difficult for a micro-orthopting-wing aircraft to fly smoothly. If the two wings can be controlled separately, better flight can be achieved in a complex flight environment.
实用新型内容Utility model content
本实用新型针对现有的微型扑翼飞行器在扑动过程中无法实现对两个翅膀分别进行控制的技术问题,提出了一种可实现双翼分别控制的微型扑翼装置,通过对称布局的齿轮连杆机构使得两个翅膀的分别拍动,从而实现对两个翅膀的分别控制。The utility model aims at the technical problem that the existing miniature flapping-wing aircraft cannot control the two wings separately during the flapping process, and proposes a miniature flapping-wing device that can realize the separate control of the two wings. The rod mechanism makes the two wings flap separately, thereby realizing the separate control of the two wings.
本实用新型解决上述问题所采用的技术方案如下:The technical solution adopted by the utility model to solve the above problems is as follows:
一种可实现双翼分别控制的微型扑翼装置,包括机架13、翅膀8以及拍动驱动机构100,拍动驱动机构100左右对称分布安装于机架13的两侧;A miniature flapping wing device capable of separately controlling two wings, comprising a
拍动驱动机构100包括动力齿轮1、传动齿轮2、摇杆3、连杆4、传动齿轮限位环5、连杆限位环6、摇臂支撑杆7、摇臂9、摇臂限位环10、牵引钩11、滑块12和牵引钩限位环14,传动齿轮2上制有摇杆3,连杆4、摇臂9上分别制有滑道,The
拍动驱动机构100上的动力齿轮1与外置电机的输出轴连接,动力齿轮1与传动齿轮2啮合传动,传动齿轮2和连杆4通过分别通过传动齿轮限位环5、连杆限位环6安装在机架13上,摇杆3、滑块12能够分别在连杆4不同的滑道内自由滑动,牵引钩11通过限位环14安装在滑块12上,牵引钩11能够自由转动,摇臂9通过销与牵引钩11相连接,并由摇臂支撑杆7支撑,在摇臂支撑杆7上方有限位环10限制摇臂9上下摆动,使摇臂9只能在固定的水平面内摆动,摇臂9与翅膀8固定连接;通过动力齿轮1与传动齿轮2啮合将电机输出的高转速进行减速,传动齿轮2通过摇杆3带动连杆4做往复运动,并使得滑块12在滑道内移动,但始终在同一水平面内带动摇臂9转动,从而实现由摇臂9带动翅膀8的拍动。The power gear 1 on the
进一步,机架13上制有第一套杆131和第二套杆132。Further, a first set of
有益效果Beneficial effect
1、一种双翼可分别控制的微型扑翼装置采用左右对称布局,实现两个翅膀分别拍动,可实现较为复杂的运动。1. A miniature flapping device with two wings that can be controlled separately adopts a left-right symmetrical layout to realize flapping of two wings separately, which can realize relatively complex movements.
2、一种双翼可分别控制的微型扑翼装置驱动机构为齿轮连杆结构,结构简单,质量轻,可靠性高。2. A miniature flapping wing device whose two wings can be controlled separately. The driving mechanism is a gear connecting rod structure, which is simple in structure, light in weight and high in reliability.
附图说明Description of drawings
图1为一种双翼可分别控制的微型扑翼装置的整体示意图。Fig. 1 is an overall schematic diagram of a miniature flapping wing device whose wings can be controlled separately.
图2为一种双翼可分别控制的微型扑翼装置的扑动驱动机构100结构示意图。FIG. 2 is a structural schematic diagram of a
图3为一种双翼可分别控制的微型扑翼装置的机架13机构示意图。Fig. 3 is a schematic diagram of the mechanism of the
图4为一种双翼可分别控制的微型扑翼装置的连杆4结构示意图。Fig. 4 is a structural schematic diagram of the connecting
图5为一种双翼可分别控制的微型扑翼装置的摇臂9结构示意图。Fig. 5 is a structural schematic diagram of the
图6为一种双翼可分别控制的微型扑翼装置的限位环5结构示意图。Fig. 6 is a structural schematic diagram of the
图7为一种双翼可分别控制的微型扑翼装置的滑块12结构示意图。Fig. 7 is a structural schematic diagram of the
附图标记记录如下:1-动力齿轮、2-传动齿轮、3-摇杆、4-连杆、5-传动齿轮限位环、6-连杆限位环、7-摇臂支撑杆、8-翅膀、9-摇臂、10-摇臂限位环、11-牵引钩、12-滑块、13-机架、14-牵引钩限位环,41-上滑道、42-下滑道、131-第一套杆、132-第二套杆、20-外置电机,The reference signs are recorded as follows: 1-power gear, 2-transmission gear, 3-rocker, 4-connecting rod, 5-transmission gear limit ring, 6-link limit ring, 7-rocker arm support rod, 8- -wings, 9-rocker arm, 10-rocker arm limit ring, 11-traction hook, 12-slider, 13-frame, 14-traction hook limit ring, 41-upper slide, 42-down slide, 131-the first set of rods, 132-the second set of rods, 20-external motor,
100-拍动驱动机构。100 - beat drive mechanism.
具体实施方式Detailed ways
以下结合附图对本实用新型的原理和特征进行描述,所举实例只用于解释本实用新型,并非用于限定本实用新型的范围。The principles and features of the present utility model are described below in conjunction with the accompanying drawings, and the examples given are only used to explain the utility model, and are not used to limit the scope of the utility model.
如图1-7所示,一种可实现双翼可分别控制的微型扑翼装置,包括机架13、2个翅膀8以及2套拍动驱动机构100。As shown in FIGS. 1-7 , a miniature flapping wing device capable of separately controlling both wings includes a
拍动驱动机构100包括动力齿轮1、传动齿轮2、摇杆3、连杆4、传动齿轮限位环5、连杆限位环6、摇臂支撑杆7、摇臂9、摇臂限位环10、牵引钩11、滑块12、牵引钩限位环14,传动齿轮2上制有摇杆3,连杆4上制有上滑道41和下滑道42,摇臂9上制有滑道,2套所述拍动驱动机构100左右对称分布安装于机架13的两侧。The
拍动驱动机构100上的动力齿轮1与外置电机20的输出轴连接,外置电机20通过电机套固定在机架13上,动力齿轮1与传动齿轮2啮合传动,传动齿轮2和连杆4通过分别通过传动齿轮限位环5、连杆限位环6套装在机架13的第一套杆131和第二套杆132上,摇杆3、滑块12能够分别在连杆4的下滑道42和上滑道41内自由滑动,牵引钩11通过限位环14安装在滑块12上,牵引钩11能够自由转动,摇臂9通过销与牵引钩11相连接,并由摇臂支撑杆7支撑,在摇臂支撑杆7上方有限位环10限制摇臂9上下摆动,使摇臂9只能在固定的水平面内摆动,摇臂9与翅膀8固定连接,通过动力齿轮1与传动齿轮2啮合将外置电机20输出的高转速进行减速,使得传动齿轮2上的摇杆3做圆周运动,带动连杆4做往复运动,滑块12在上滑道41内移动,但始终在同一水平面内带动摇臂9转动,从而实现由摇臂9带动翅膀8的拍动。The power gear 1 on the
一种双翼可分别控制的微型扑翼装置通过如下的方式实现动作:A miniature flapping wing device whose wings can be controlled separately realizes the action in the following way:
动力扑动时,需要连接外置电机20进行驱动,外置电机20输出轴固定安装有动力齿轮1,动力齿轮1与传动齿轮2啮合,传动齿轮2将外置电机20输出的高转速减为适合扑翼拍动的速度,摇杆3在连杆4的下滑道42内并做圆周运动,并通过摇杆3与传动齿轮2连接实现摇杆4的摆动,滑块12与牵引钩11通过牵引钩限位环14连接,牵引钩11通过销与摇臂9连接,摇臂9上方有摇臂限位环10限制所摆动的平面,连杆4做往复运动时带动滑块12和牵引钩11前后摆动,同时带动摇臂9做往复运动,从而实现摇臂9带动翅膀8拍动,两个动力齿轮1、两个传动齿轮2、两个连杆4、两个摇臂支撑杆7、两个滑块12及两个摇臂9左右对称分布,由此实现对两个翅膀拍动的分别控制。When the power flutters, it is necessary to connect the
本例的双翼可分别控制的微型扑翼装置通过两套齿轮连杆机构来实现对两个翅膀的分别控制,结构简单,易于控制。In this example, the micro-flapping wing device that can control the two wings separately realizes the separate control of the two wings through two sets of gear linkage mechanisms, and has a simple structure and is easy to control.
以上所述仅为本实用新型的较佳实施例,并不用以限制本实用新型,凡在本实用新型的精神和原则之内,所作的任何修改、等同替换、改进等,均应包含在本实用新型的保护范围之内。The above descriptions are only preferred embodiments of the present utility model, and are not intended to limit the present utility model. Any modifications, equivalent replacements, improvements, etc. made within the spirit and principles of the present utility model shall be included in this utility model. within the scope of protection of utility models.
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