CN114923364A - Arrow projection mechanism with two degrees of freedom - Google Patents

Arrow projection mechanism with two degrees of freedom Download PDF

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CN114923364A
CN114923364A CN202210185794.8A CN202210185794A CN114923364A CN 114923364 A CN114923364 A CN 114923364A CN 202210185794 A CN202210185794 A CN 202210185794A CN 114923364 A CN114923364 A CN 114923364A
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limit
yaw
arrow
pitch
plate
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CN114923364B (en
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王伟
邹金洲
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Wuhan University WHU
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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41WEAPONS
    • F41BWEAPONS FOR PROJECTING MISSILES WITHOUT USE OF EXPLOSIVE OR COMBUSTIBLE PROPELLANT CHARGE; WEAPONS NOT OTHERWISE PROVIDED FOR
    • F41B4/00Friction-wheel operated launchers
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41WEAPONS
    • F41GWEAPON SIGHTS; AIMING
    • F41G5/00Elevating or traversing control systems for guns
    • F41G5/02Elevating or traversing control systems for guns using only mechanical means for remote control
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02EREDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E10/00Energy generation through renewable energy sources
    • Y02E10/70Wind energy
    • Y02E10/72Wind turbines with rotation axis in wind direction

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Abstract

本发明公开了一种两自由度的箭矢投射机构,包括两自由度云台、箭支限位机构和发射驱动机构,两自由度云台包括俯仰驱动模块和偏航驱动模块,箭支限位机构和发射驱动机构整体安装在两自由度云台上,俯仰驱动模块和偏航驱动模块分别使箭支限位机构和发射驱动机构完成俯仰运动偏航运动;箭支限位机构包括固定限位和活动限位,固定限位分别从上下左右四个方向对箭矢进行限位,活动限位防止箭的旋转;发射驱动机构包括发射部分和触发部分,触发部分可以带动发射部分做开合运动,合到最近时,发射部分接触箭杆,用摩擦力带动箭杆飞出。本发明实现在一定距离的空间范围的精准投递,误差控制于厘米级。其可以应用于众多需要较高精准度的非交接式投送场合。

Figure 202210185794

The invention discloses a two-degree-of-freedom arrow projection mechanism, comprising a two-degree-of-freedom head, an arrow limiter mechanism and a launch drive mechanism. The two-degree-of-freedom head includes a pitch drive module and a yaw drive module. The positioning mechanism and the launch drive mechanism are integrally installed on the two-degree-of-freedom head. The pitch drive module and the yaw drive module respectively enable the arrow limit mechanism and the launch drive mechanism to complete the pitch and yaw motion; the arrow limit mechanism includes a fixed limit. Position and movable limit, the fixed limit respectively limits the arrow from four directions of up, down, left and right, and the movable limit prevents the rotation of the arrow; the launch drive mechanism includes a launch part and a trigger part, and the trigger part can drive the launch part to open and close Movement, when it closes to the nearest point, the launching part contacts the arrow shaft and drives the arrow shaft to fly out with friction. The present invention realizes accurate delivery within a certain distance space range, and the error is controlled at the centimeter level. It can be applied to many non-handover delivery occasions that require high precision.

Figure 202210185794

Description

一种两自由度的箭矢投射机构A two-degree-of-freedom arrow projection mechanism

技术领域technical field

本发明涉及机器人技术领域,具体来讲是一种实现精准箭矢投射的机构。The invention relates to the technical field of robots, in particular to a mechanism for realizing precise arrow projection.

背景技术Background technique

目前,国内外的机器人产业发展迅速,机器人技术在例如医学、工农业生产乃至军事领域都得到了较为广泛的应用。在很多工况中,都有涉及物品的准确递送,例如 水上救生设备的投递,高层火灾救援物资的投送。目前在生产和民用上鲜有物品精准 投掷的解决方案。如果能够通过机械来实现物体的投递,将在众多场合在精度、可靠 性上实现保障。At present, the robot industry at home and abroad is developing rapidly, and robot technology has been widely used in fields such as medicine, industrial and agricultural production and even military. In many working conditions, there is an accurate delivery of items, such as the delivery of water life-saving equipment, and the delivery of high-rise fire relief materials. At present, there are few solutions for accurate throwing of items in production and civilian use. If the delivery of objects can be realized by machinery, the accuracy and reliability will be guaranteed in many occasions.

申请号为CN202110657724.3,名称为“箭矢抛射机器人及抛射方法”的专利中, 采用了一种电机驱动摆壁抛射的箭矢投射方式,其结构简单但是所占空间巨大,并且 由于摆臂长,驱动的力效不高。较长的摆臂会放大控制误差,从而降低投射的精度The application number is CN202110657724.3, and the patent titled "Arrow Projection Robot and Projection Method" adopts a motor-driven swing wall projection method of arrow projection, which has a simple structure but occupies a huge space, and because of the swing arm Long, the driving force is not high. Longer swing arms magnify control errors and reduce projection accuracy

除此之外,申请号为CN201210040804.5,名称为“一种吹箭”的专利中,气动发 射是其动力方式,其主要的缺点表现在气动无法实现较大载荷的高速发射,同时要求 不能太大的发射质量,发射的精度直接受气源稳定性的影响。In addition, in the patent with the application number of CN201210040804.5 and the title of "A Blowing Arrow", aerodynamic launch is its power method. If the emission mass is too large, the accuracy of emission is directly affected by the stability of the gas source.

发明内容SUMMARY OF THE INVENTION

本发明主要是解决现有技术所存在的技术问题。发明为一种两自由度的箭矢发射机构,本发明实现在一定距离的空间范围的精准投递,误差控制于厘米级。其可以应 用于众多需要较高精准度的非交接式投送场合。The present invention mainly solves the technical problems existing in the prior art. The invention is a two-degree-of-freedom arrow launching mechanism. The invention realizes precise delivery within a space range of a certain distance, and the error is controlled at the centimeter level. It can be applied to many non-handover delivery occasions that require high precision.

为了解决上述技术问题,本发明提供了如下的技术方案:In order to solve the above-mentioned technical problems, the present invention provides the following technical solutions:

一种两自由度的箭矢投射机构,其特征在于:包括两自由度云台、箭支限位机构和发射驱动机构,其中,A two-degree-of-freedom arrow projection mechanism, characterized in that it comprises a two-degree-of-freedom head, an arrow limiter mechanism and a launch drive mechanism, wherein,

所述两自由度云台包括俯仰驱动模块和偏航驱动模块,所述箭支限位机构和发射驱动机构整体安装在所述两自由度云台上,俯仰驱动模块和偏航驱动模块分别使所述 箭支限位机构和发射驱动机构完成俯仰运动和偏航运动;The two-degree-of-freedom cloud platform includes a pitch drive module and a yaw drive module, the arrow limit mechanism and the launch drive mechanism are integrally installed on the two-degree-of-freedom cloud platform, and the pitch drive module and the yaw drive module are respectively used. The arrow limit mechanism and the launch drive mechanism complete the pitch motion and the yaw motion;

所述箭支限位机构包括固定限位和活动限位,所述固定限位分别从上下左右四个方向对箭矢进行限位,活动限位防止箭的旋转;The arrow limit mechanism includes a fixed limit and a movable limit, the fixed limit respectively limits the arrow from four directions of up, down, left and right, and the movable limit prevents the rotation of the arrow;

所述发射驱动机构包括发射部分和触发部分,触发部分可以带动发射部分做开合运动,合到最近时,发射部分接触箭杆,用摩擦力带动箭杆飞出。The launch driving mechanism includes a launch part and a trigger part, the trigger part can drive the launch part to open and close, and when it is closed to the nearest point, the launch part contacts the arrow shaft and drives the arrow shaft to fly out with frictional force.

进一步地,所述俯仰驱动模块和偏航驱动模块公用相同的驱动模块,所述驱动模块包括无刷伺服电机、电机座、第一压片联轴器、输出轴承、齿轮输出轴,其中所述 无刷伺服电机固定安装在所述电机座上通过第一压片联轴器依次连接输出轴承和齿轮 输出轴,所述齿轮输出轴的端部设有齿轮。Further, the pitch drive module and the yaw drive module share the same drive module, and the drive module includes a brushless servo motor, a motor base, a first press coupling, an output bearing, and a gear output shaft, wherein the The brushless servo motor is fixedly installed on the motor base and is sequentially connected to the output bearing and the gear output shaft through a first sheet-pressing coupling, and the end of the gear output shaft is provided with a gear.

进一步地,所述俯仰驱动模块包括侧板、肋板、驱动模块、俯仰支撑轴和俯仰从 动齿轮,其中,两侧板底部固定连接在偏航驱动模块上,肋板通过侧肋连接件连接在 两侧板之间,驱动模块的齿轮输出轴从肋板中穿出与俯仰从动齿轮上的齿轮啮合,俯 仰从动齿轮顶部设有俯仰支撑板,所述俯仰从动齿轮与所述侧板通过俯仰回转轴铰 接,所述俯仰从动齿轮中间设有弧形槽,俯仰限位钉设置在所述弧形槽中并和所述侧 板固定连接。Further, the pitch drive module includes a side plate, a rib plate, a drive module, a pitch support shaft and a pitch driven gear, wherein the bottoms of the two side plates are fixedly connected to the yaw drive module, and the rib plates are connected by side rib connectors. Between the two side plates, the gear output shaft of the drive module protrudes from the rib plate and meshes with the gear on the pitch driven gear. A pitch support plate is provided on the top of the pitch driven gear, and the pitch driven gear is connected to the side. The plate is hinged through the pitching rotary shaft, the pitch driven gear is provided with an arc-shaped groove in the middle, and the pitch-limiting pin is arranged in the arc-shaped groove and is fixedly connected with the side plate.

进一步地,所述俯仰回转轴包括贯穿所述侧板和俯仰支撑板的俯仰紧定螺栓,俯仰滚针轴承设置在侧板和俯仰支撑板之间,所述侧板和俯仰支撑板两侧分别设有俯仰 支撑挡边轴承,所述俯仰紧定螺栓的另一端通过俯仰紧定螺母紧固连接。Further, the pitching rotation axis includes pitching fixing bolts penetrating the side plate and the pitching support plate, the pitching needle bearing is arranged between the side plate and the pitching support plate, and the two sides of the side plate and the pitching support plate are respectively A pitching support rib bearing is provided, and the other end of the pitching fixing bolt is fastened and connected by a pitching fixing nut.

进一步地,所述偏航驱动模块包括基座,驱动支撑板,驱动模块,偏航轴承总 成,偏航从动齿圈,偏航支撑板,偏航支撑铝管;其中,所述偏航轴承总成包括偏航 轴承、偏航轴承内环和偏航轴承外环,驱动模块固定连接在所述驱动支撑板上方,偏 航轴承内环安装在所述驱动支撑板下方,基座,驱动支撑板,偏航轴承内环固定连 接,组成部分相对大地固定,驱动模块的齿轮输出轴与偏航从动齿圈啮合传动,偏航 轴承外环将轴承扣于偏航支撑板上,两个偏航支撑板将偏航从动齿圈夹于中间,偏航 支撑板、偏航从动齿圈、偏航轴承外环和偏航支撑铝管相对固定。Further, the yaw drive module includes a base, a drive support plate, a drive module, a yaw bearing assembly, a yaw driven ring gear, a yaw support plate, and a yaw support aluminum tube; wherein, the yaw The bearing assembly includes a yaw bearing, an inner ring of the yaw bearing and an outer ring of the yaw bearing, the drive module is fixedly connected above the drive support plate, the inner ring of the yaw bearing is installed under the drive support plate, the base, the drive The support plate, the inner ring of the yaw bearing is fixedly connected, the components are relatively fixed, the gear output shaft of the drive module is meshed with the yaw driven ring gear, and the outer ring of the yaw bearing buckles the bearing on the yaw support plate, two The yaw support plate sandwiches the yaw driven ring gear, and the yaw support plate, the yaw driven ring gear, the yaw bearing outer ring and the yaw support aluminum tube are relatively fixed.

进一步地,所述箭支限位机构和所述发射驱动机构整体通过固定连接件安装在所述两自由度云台上,所述固定连接件包括基准碳纤维板、前侧铝管,后侧铝管和上侧 连接板,其中前侧铝管固定连接在基准碳纤维板前端左右两侧,后侧铝管固定连接在 基准碳纤维板后端左右两侧并向后悬挑,所述上侧连接板固定在所述前侧铝管的上表 面,其中前侧铝管外侧与俯仰支撑板固定连接。Further, the arrow limit mechanism and the launch drive mechanism are integrally mounted on the two-degree-of-freedom pan/tilt through a fixed connector, and the fixed connector includes a reference carbon fiber board, a front aluminum tube, and a rear aluminum tube. The tube and the upper connecting plate, wherein the front aluminum tube is fixedly connected to the left and right sides of the front end of the reference carbon fiber board, and the rear aluminum tube is fixedly connected to the left and right sides of the rear end of the reference carbon fiber board and cantilevered rearward. The upper connecting plate It is fixed on the upper surface of the front aluminum tube, wherein the outer side of the front aluminum tube is fixedly connected with the pitch support plate.

进一步地,所述旋转限位为尾部限位,所述尾部限位通过尾部的分羽器实现;所述固定限位包括左右限位,下限位、头部限位和上限位;所述固定限位包括左右限 位,下限位、头部限位和尾部限位,其中左右限位包括分别分布在所述上侧连接板两 端和后限位连接板上的圆头钉固定座以及固定在所述圆头钉固定座内的左右限位圆头 钉,所述后限位连接板35固定在后侧铝管上;所述下限位包括通过下限位板固定座固 定在所述基准碳纤维板上的下限位板以及设置在后侧铝管之间的下限位圆头钉,其中 下限位圆头钉通国下限位钉固定座固定在后侧支撑板上方,其中后侧支撑板固定连接 在两后侧铝管之间;所述头部限位包括头部限位支撑块、头部限位支撑和头部限位轴 承,所述头部限位支撑块固定连接在基准碳纤维板上,头部限位支撑固接在头部限位 支撑块上,头部限位轴承固定在所述头部限位支撑上,两侧的头部限位轴承分别设置 在箭支头部两侧,所述上限位包括固定在所述上侧连接板上的旋转下压气缸固定座, 旋转下压气缸固定连接在所述旋转下压气缸固定座上,所述旋转下压气缸固定座前端 连接弯钩扣子,旋转下压气缸带动所述弯钩扣子转动对箭支进行上限位。Further, the rotation limit is a tail limit, and the tail limit is realized by a feather divider at the tail; the fixed limit includes a left and right limit, a lower limit, a head limit and an upper limit; the fixed limit The limit includes left and right limit, lower limit, head limit and tail limit, wherein the left and right limit includes the round head nail fixing seat and the fixed seat respectively distributed on the two ends of the upper connecting plate and the rear limit connecting plate The left and right limit round head nails in the round head nail fixing seat, the rear limit connecting plate 35 is fixed on the aluminum tube on the rear side; the lower limit includes being fixed on the reference carbon fiber through the lower limit plate fixing seat The lower limit plate on the plate and the lower limit round head nails arranged between the aluminum tubes on the rear side, wherein the lower limit round head nails are connected to the lower limit nail fixing seat above the rear side support plate, wherein the rear side support plate is fixedly connected Between the two rear aluminum tubes; the head limit includes a head limit support block, a head limit support and a head limit bearing, and the head limit support block is fixedly connected to the reference carbon fiber board , the head limit support is fixed on the head limit support block, the head limit bearing is fixed on the head limit support, and the head limit bearings on both sides are respectively arranged on both sides of the arrow head , the upper limit includes a rotary pressing cylinder fixing seat fixed on the upper connecting plate, the rotary pressing cylinder is fixedly connected to the rotary pressing cylinder fixing seat, and the front end of the rotary pressing cylinder fixing seat is connected The hook button is rotated and the pressing cylinder drives the hook button to rotate to upper limit the arrow.

进一步地,所述上侧连接板和基准碳纤维板之间依次设有气缸尾部长夹块和气缸尾部短夹块和直线气缸,分羽器固定连接在直线气缸气缸杆上。Further, a cylinder tail long clamp block, a cylinder tail short clamp block and a linear cylinder are sequentially arranged between the upper connecting plate and the reference carbon fiber board, and the feather separator is fixedly connected to the cylinder rod of the linear cylinder.

进一步地,所述发射部分包括橡胶胎皮、轮毂、发射驱动电机、上层安装板,中 层安装板、下层安装板、第一滑轨,第一滑块,上下连接件,所述胎皮套在轮毂上, 轮毂套在发射驱动电机的电机转子上,电机安装在安装板上,上层安装板,中层安装 板、下层安装板依次固定连接,下层安装板下侧安装有第一滑块,所述第一滑轨固定 安装在所述基准碳纤维板上,所述第上下连接件固定连接在下层安装板迪安位于两侧 第一滑块之间,所述上下连接件向下设置于基准碳纤维板中的凹槽中与触发部分连 接,触发部分带动所述第一滑块沿所述第一滑轨滑动用于开合运动的导向。Further, the launching part includes a rubber tire skin, a wheel hub, a launching drive motor, an upper-layer mounting plate, a middle-layer mounting plate, a lower-layer mounting plate, a first sliding rail, a first sliding block, an upper and lower connecting piece, and the tire skin is sleeved on the upper and lower layers. On the hub, the hub is sleeved on the motor rotor of the launch drive motor, the motor is mounted on the mounting plate, the upper mounting plate, the middle mounting plate, and the lower mounting plate are fixedly connected in sequence, and the lower side of the lower mounting plate is installed with a first slider. The first slide rail is fixedly installed on the reference carbon fiber board, the first upper and lower connecting pieces are fixedly connected to the lower mounting board, and Dean is located between the first sliders on both sides, and the upper and lower connecting pieces are set downward on the reference carbon fiber board The groove in the middle is connected with the triggering part, and the triggering part drives the first sliding block to slide along the first sliding rail for guiding the opening and closing movement.

进一步地,所述触发部分包括曲轴前段,曲轴中段和曲轴后段;所述曲轴前段和曲轴后段通过中段上的孔固定连接;所述曲轴前段通过曲轴前段支撑轴承安装在前端 固定座上,前端固定座与基准碳纤维板固定连接,曲轴后段通过第二压片联轴器与曲 轴电机的电机轴连接,曲轴电机通过曲轴电机座与基准碳纤维板连接,两曲柄两侧各 安装曲柄承力轴承,另一端安装滚针轴承,两曲柄分别安装在曲轴前段和曲轴中段、 曲轴中段和曲轴后段之间,所述曲柄的另外一端通过轴承与滑动座子连接,带动滑动 座子做开合运动,所述滑动座子下侧安装第二滑块,第二滑块下侧设有第二滑轨,第 二滑轨和第二滑块起导向作用。Further, the triggering part includes a front section of the crankshaft, a middle section of the crankshaft and a rear section of the crankshaft; the front section of the crankshaft and the rear section of the crankshaft are fixedly connected through a hole on the middle section; the front section of the crankshaft is mounted on the front end fixing seat through a support bearing of the front section of the crankshaft, The front end fixing seat is fixedly connected with the reference carbon fiber board, the rear section of the crankshaft is connected with the motor shaft of the crankshaft motor through the second pressing coupling, the crankshaft motor is connected with the reference carbon fiber board through the crankshaft motor seat, and the crank bearing capacity is installed on each side of the two cranks Bearing, the other end is installed with a needle roller bearing, and the two cranks are respectively installed between the front section of the crankshaft and the middle section of the crankshaft, the middle section of the crankshaft and the rear section of the crankshaft. The other end of the crank is connected with the sliding seat through the bearing, which drives the sliding seat to open and close A second sliding block is installed on the lower side of the sliding seat, and a second sliding rail is arranged on the lower side of the second sliding block, and the second sliding rail and the second sliding block play a guiding role.

与现有技术相比,本发明有益效果如下:Compared with the prior art, the beneficial effects of the present invention are as follows:

1.结构为功能服务,曲轴可以放大4倍偏心距,在一定的张夹距离下,可以做到 较小的体积。轻量化程度高,整体重量不超过2kg,可以适应众多的工作场景。同 时,轻量化设计减小了惯量,云台的灵活性大大提高,适应更多要求迅速动作的场 景。机构设计紧凑,驱动系统集中,有利于电气系统配置。1. The structure serves the function, the crankshaft can be enlarged by 4 times the eccentric distance, and under a certain clamping distance, a smaller volume can be achieved. The light weight is high, and the overall weight does not exceed 2kg, which can adapt to many work scenarios. At the same time, the lightweight design reduces the inertia, and the flexibility of the gimbal is greatly improved, adapting to more scenes that require rapid movements. The mechanism design is compact and the drive system is centralized, which is beneficial to the configuration of the electrical system.

2.机构采取了除发射正方向以外的所有自由度限制。一方面可以做到发射对象在机构上绝佳的稳定性,另一方面为发射精度提供了保障。2. The mechanism adopts all degrees of freedom constraints except the forward direction of launch. On the one hand, it can achieve the excellent stability of the launch object in the mechanism, and on the other hand, it provides a guarantee for the launch accuracy.

3.驱动方式为摩擦速度控制,得益于现阶段,伺服电机闭环控制技术的发展,可以做到较高精度的转速控制。同时触发方式采用了连杆机构的死点,保证了夹紧的精 度,降低了触发驱动力的要求。机构发射精度表现优秀。机构的投射距离大于15m, 误差小于5cm。3. The driving method is friction speed control. Thanks to the development of servo motor closed-loop control technology at this stage, high-precision speed control can be achieved. At the same time, the trigger method adopts the dead point of the linkage mechanism, which ensures the clamping accuracy and reduces the requirement of triggering driving force. The mechanism launch accuracy is excellent. The projection distance of the mechanism is greater than 15m, and the error is less than 5cm.

附图说明Description of drawings

附图1为本发明的等轴测图。Figure 1 is an isometric view of the present invention.

附图2为本发明的两自由度云台等轴测图。FIG. 2 is an isometric view of a two-degree-of-freedom pan/tilt head of the present invention.

附图3为本发明的驱动模块爆炸视图。FIG. 3 is an exploded view of the drive module of the present invention.

附图4为本发明的偏航部分轴测图。Figure 4 is an axonometric view of the yaw part of the present invention.

附图5为本发明的偏航部分爆炸视图。Figure 5 is an exploded view of the yaw part of the present invention.

附图6为本发明的俯仰部分轴测图。Figure 6 is an axonometric view of the pitch part of the present invention.

附图7为本发明的俯仰部分转轴爆炸视图。FIG. 7 is an exploded view of the rotating shaft of the pitch part of the present invention.

附图8为本发明的限位示意图。FIG. 8 is a schematic diagram of the limit position of the present invention.

附图9为本发明的箭支限位等轴测图。Figure 9 is an isometric view of the arrow limit position of the present invention.

附图10为本发明箭支限位爆炸视图。FIG. 10 is an exploded view of the arrow position limit of the present invention.

附图11为本发明发射驱动的发射部分等轴测图。Figure 11 is an isometric view of the launch part of the launch drive of the present invention.

附图12为本发摩擦发射滑台爆炸视图。Figure 12 is an exploded view of the friction launch slide of the present invention.

附图13为本发射驱动的触发部分等轴测图。Figure 13 is an isometric view of the trigger portion of the firing drive.

附图14为本发射驱动的触发部分爆炸视图。Figure 14 is an exploded view of the trigger part of the launch drive.

附图15中(a)、(b)、(c)、(d)为曲轴动作示意图。(a), (b), (c), (d) of FIG. 15 are schematic diagrams of crankshaft movements.

附图16中(e)、(f)、(g)、(h)为发射动作示意图。(e), (f), (g), and (h) in FIG. 16 are schematic diagrams of the launching action.

附图中:In the attached picture:

1-无刷伺服电机,2-第一压片联轴器,3-电机座,4-齿轮输出轴,5-输出轴 承;6-驱动模块,7-驱动支撑板,8-偏航轴承外环,9-偏航支撑铝管,10-基座, 11-偏航轴承内环,12-偏航支撑板,13-偏航从动齿圈,14-偏航轴承;15-俯仰从 动齿轮,16-俯仰限位钉,17-齿轮,18-侧板,19-肋板,20-侧肋连接件,21-俯 仰支撑板,22-俯仰紧定螺栓,23-俯仰支撑挡边轴承,24-俯仰滚针轴承,25-俯 仰紧定螺母;26-前侧铝管,27-左右限位圆头钉,28-圆头钉固定座,29-弯钩扣 子,30-上侧连接板,31-旋转下压气缸固定座,32-旋转下压气缸,33-后侧铝 管,34-直线气缸,35-后限位连接板,36-下限位圆头钉,37-分羽器,38-下限位钉固定座,39-后侧支撑板,40-气缸头部固定座,41-气缸尾部短夹块,42-气缸 尾部长夹块,43-下限位板,44-下限位板固定座,45-头部限位支撑块,46-头部 限位支撑,47-头部限位轴承,48-基准碳纤维板;49-轮毂,50-橡胶胎皮,51-发 射驱动电机,52-上层安装板,53-中层安装板,54-下层安装板,55-上下连接 件,56-第一滑轨,57-第一滑块,58-滑动承力轴承,59-滑动座子,60-第二滑 块,61-第二滑轨,62-曲柄承力轴承,63-曲轴电机,64-曲轴电机座,65-第二压 片联轴器,66-曲轴后段,67-曲柄,68-滚针轴承,69-曲轴中段,70-曲轴前段, 71-曲轴前段支撑轴承,72-前端固定座。1-Brushless servo motor, 2-First press coupling, 3-Motor base, 4-Gear output shaft, 5-Output bearing; 6-Drive module, 7-Drive support plate, 8-Yaw bearing outside Ring, 9-Yaw support aluminum tube, 10-Base, 11-Yaw bearing inner ring, 12-Yaw support plate, 13-Yaw driven ring gear, 14-Yaw bearing; 15-Pitch driven Gear, 16-pitch limit pin, 17-gear, 18-side plate, 19-rib plate, 20-side rib connecting piece, 21-pitch support plate, 22-pitch set bolt, 23-pitch support rib bearing , 24- pitching needle roller bearing, 25- pitching set nut; 26- front aluminum tube, 27- left and right limit round head nails, 28- round head nail fixing seat, 29- hook button, 30- upper side connection Plate, 31- Rotating Down Pressing Cylinder Holder, 32- Rotating Down Pressing Cylinder, 33- Rear Aluminum Tube, 34- Linear Cylinder, 35- Rear Limit Connection Plate, 36- Lower Limit Round Head Nail, 37- Split Feather device, 38-lower limit pin fixing seat, 39-rear side support plate, 40-cylinder head fixing seat, 41-cylinder tail short clamp block, 42-cylinder tail long clamp block, 43-lower limit plate, 44-lower limit Position plate fixing seat, 45- head limit support block, 46- head limit support, 47- head limit bearing, 48- benchmark carbon fiber plate; 49- wheel hub, 50- rubber tire skin, 51- launch drive Motor, 52-upper mounting plate, 53-middle mounting plate, 54-lower mounting plate, 55-upper and lower connecting pieces, 56-first sliding rail, 57-first sliding block, 58-sliding bearing, 59-sliding Seat, 60-Second Slider, 61-Second Slide Rail, 62-Crank Bearing, 63-Crankshaft Motor, 64-Crankshaft Motor Seat, 65-Second Press Coupling, 66-Crankshaft Rear Section , 67-Crank, 68-Needle bearing, 69-Crankshaft middle, 70-Crankshaft front, 71-Crankshaft front support bearing, 72-Front fixed seat.

具体实施方式Detailed ways

为使本发明的目的、技术方案和优点更加清楚明了,下面结合具体实施方式并参照附图,对本发明进一步详细说明。应该理解,这些描述只是示例性的,而并非要限 制本发明的范围。此外,在以下说明中,省略了对公知结构和技术的描述,以避免不 必要地混淆本发明的概念。In order to make the objectives, technical solutions and advantages of the present invention clearer, the present invention will be further described in detail below with reference to the specific embodiments and the accompanying drawings. It should be understood that these descriptions are exemplary only, and are not intended to limit the scope of the invention. Also, in the following description, descriptions of well-known structures and techniques are omitted to avoid unnecessarily obscuring the concepts of the present invention.

请参阅图1-14,本发明提供一种技术方案:一种两自由度的箭矢投射机构,包括两自由度云台、箭支限位、发射驱动三部分。其中两自由度云台主要功能是提供投射 所需要的俯仰角和偏航角,并提供与基座10的连接孔位。箭支限位提供对箭杆初始位 置的限定,提供准确的目标空间姿态。发射驱动部分是投射的动力源,通过对箭杆夹 紧,产生足够的摩擦力将箭杆推出。Referring to Figures 1-14, the present invention provides a technical solution: a two-degree-of-freedom arrow projection mechanism, comprising three parts: a two-degree-of-freedom head, an arrow limiter, and a launch drive. Among them, the main function of the two-degree-of-freedom PTZ is to provide the pitch angle and yaw angle required for projection, and to provide the connection hole position with the base 10. The arrow limit provides the limitation of the initial position of the arrow shaft and provides accurate target space attitude. The launch driving part is the power source of the projection, by clamping the arrow shaft, enough friction force is generated to push the arrow shaft out.

如图2所示,两自由度云台包括俯仰驱动模块和偏航驱动模块,所述箭支限位机构和发射驱动机构整体安装在所述两自由度云台上,俯仰驱动模块和偏航驱动模块分 别使所述箭支限位机构和发射驱动机构完成俯仰运动和偏航运动。其中俯仰驱动模块 和偏航驱动模块公用相同的驱动模块6,如图3所示,所述驱动模块6包括无刷伺服 电机1、电机座3、第一压片联轴器2、输出轴承5、齿轮输出轴4,其中所述无刷伺 服电机1固定安装在所述电机座3上通过第一压片联轴器2依次连接输出轴承5和齿 轮输出轴4,所述齿轮输出轴4的端部设有齿轮17。如图6所示,俯仰驱动模块包括 侧板18、肋板19、驱动模块6、俯仰支撑轴和俯仰从动齿轮15,其中,两侧板18底 部固定连接在偏航驱动模块上,肋板19通过侧肋连接件20连接在两侧板18之间,驱 动模块6的齿轮输出轴4从肋板19中穿出与俯仰从动齿轮15上的齿轮啮合,俯仰从 动齿轮15顶部设有俯仰支撑板21,所述俯仰从动齿轮15与所述侧板18通过俯仰回 转轴铰接,所述俯仰从动齿轮15中间设有弧形槽,俯仰限位钉16设置在所述弧形槽 中。俯仰回转轴包括贯穿所述侧板18和俯仰支撑板21的俯仰紧定螺栓22,俯仰滚针 轴承24设置在侧板18和俯仰支撑板21之间,所述侧板18和俯仰支撑板21两侧分别 设有俯仰支撑挡边轴承23,所述俯仰紧定螺栓22的另一端通过俯仰紧定螺母25紧固 连接。驱动模块6安装在一侧的侧板18上,齿轮输出轴4的齿轮从外侧伸出,与俯仰 从动齿轮15啮合传动。俯仰限位钉16安装在同侧的侧板18上,用于限制铰链运动范 围。俯仰回转轴有左右两个,具体结构如图7所示,侧板18和俯仰支撑板21将俯仰 滚针轴承24夹于中间,两板外侧均安装承力轴承,然后通过紧定螺栓压紧连接。As shown in Figure 2, the two-degree-of-freedom head includes a pitch drive module and a yaw drive module. The arrow limiter mechanism and the launch drive mechanism are integrally installed on the two-DOF head, and the pitch drive module and the yaw drive module are integrally installed on the two-DOF head. The drive module enables the arrow limit mechanism and the launch drive mechanism to complete pitch motion and yaw motion respectively. The pitch drive module and the yaw drive module share the same drive module 6 . As shown in FIG. 3 , the drive module 6 includes a brushless servo motor 1 , a motor base 3 , a first press coupling 2 , and an output bearing 5 , Gear output shaft 4, wherein the brushless servo motor 1 is fixedly installed on the motor base 3 through the first press coupling 2 to connect the output bearing 5 and the gear output shaft 4 in turn, the gear output shaft 4 The ends are provided with gears 17 . As shown in FIG. 6 , the pitch drive module includes a side plate 18 , a rib plate 19 , a drive module 6 , a pitch support shaft and a pitch driven gear 15 , wherein the bottom of the two side plates 18 is fixedly connected to the yaw drive module, and the rib plate 19 is connected between the two side plates 18 through the side rib connecting piece 20. The gear output shaft 4 of the drive module 6 passes through the rib plate 19 and meshes with the gear on the pitch driven gear 15. The top of the pitch driven gear 15 is provided with The pitch support plate 21, the pitch driven gear 15 and the side plate 18 are hinged through the pitch rotation axis, the pitch driven gear 15 is provided with an arc groove in the middle, and the pitch limit pin 16 is arranged in the arc groove middle. The pitching rotation shaft includes pitching fixing bolts 22 penetrating the side plate 18 and pitching support plate 21 , and pitching needle bearing 24 is arranged between the side plate 18 and pitching support plate 21 , and the side plate 18 and pitching support plate 21 Both sides are respectively provided with pitch support rib bearings 23 , and the other end of the pitch tightening bolt 22 is fastened and connected by a pitch tightening nut 25 . The drive module 6 is mounted on the side plate 18 on one side, and the gear of the gear output shaft 4 protrudes from the outside to engage with the pitch driven gear 15 for transmission. The pitch limit pin 16 is installed on the side plate 18 on the same side to limit the range of motion of the hinge. The pitch rotation axis has two left and right. The specific structure is shown in Figure 7. The side plate 18 and the pitch support plate 21 sandwich the pitch needle roller bearing 24 in the middle. connect.

如图4和5所示,偏航驱动模块包括基座10,驱动支撑板7,驱动模块6,偏航 轴承14,偏航从动齿圈13,偏航支撑板12,偏航支撑铝管9;其中,所述偏航轴承 14包括偏航轴承内环11和偏航轴承外环8,驱动模块6固定连接在所述驱动支撑板7 上方,偏航轴承内环11安装在所述驱动支撑板7下方,基座10、驱动支撑板7、偏航 轴承内环11固定连接,组成部分相对大地固定,驱动模块6的齿轮输出轴4与偏航从 动齿圈13啮合传动,偏航轴承外环8将轴承扣于偏航支撑板12上,两个偏航支撑板 12将偏航从动齿圈13夹于中间,偏航支撑板12、偏航从动齿圈13、偏航轴承外环8 和偏航支撑铝管9相对固定。As shown in Figures 4 and 5, the yaw drive module includes a base 10, a drive support plate 7, a drive module 6, a yaw bearing 14, a yaw driven ring gear 13, a yaw support plate 12, and a yaw support aluminum tube 9; wherein, the yaw bearing 14 includes a yaw bearing inner ring 11 and a yaw bearing outer ring 8, the drive module 6 is fixedly connected above the drive support plate 7, and the yaw bearing inner ring 11 is installed on the drive Below the support plate 7, the base 10, the drive support plate 7, and the yaw bearing inner ring 11 are fixedly connected, and the components are relatively fixed. The bearing outer ring 8 buckles the bearing on the yaw support plate 12, the two yaw support plates 12 sandwich the yaw driven ring gear 13, the yaw support plate 12, the yaw driven ring gear 13, the yaw driven ring gear 13, The bearing outer ring 8 and the yaw supporting aluminum tube 9 are relatively fixed.

箭支限位如图9所示,分为固定限位和活动限位,活动限位具有自由度,固定限 位相对于俯仰云台固定。固定限位包括左右限位,下限位、头部限位和上限位,旋转 限位为尾部限位;上限位包括固定在所述上侧连接板30上的旋转下压气缸32固定座 31,旋转下压气缸32固定连接在所述旋转下压气缸固定座31上,所述旋转下压气缸 固定座31前端连接弯钩扣子29,旋转下压气缸带动所述弯钩扣子29转动对箭支进行 上限位,其为独立自由度,可以开合;其中左右限位包括分别分布在所述上侧连接板 30两端和后限位连接板35上的圆头钉固定座28以及固定在所述圆头钉固定座28内 的左右限位圆头钉27,所述后限位连接板35固定在后侧铝管33上;所述下限位包括 通过下限位板固定座44固定在所述基准碳纤维板48上的下限位板43以及设置在后侧 铝管33之间的下限位圆头钉36,左右限位由左右各三个限位圆头钉组成,分别固定 在上侧连接板30和后限位连接板35上,分布于俯仰云台结构的前中后三个部分。其 中下限位圆头钉36通国下限位钉固定座38固定在后侧支撑板39上方,其中后侧支撑 板39通过气缸头部固定座40固定连接在两后侧铝管33之间;所述头部限位包括头部 限位支撑块45、头部限位支撑46和头部限位轴承47,所述头部限位支撑块45固定连 接在基准碳纤维板48上,头部限位支撑46固接在头部限位支撑块45上,头部限位轴 承47固定在所述头部限位支撑上,两侧的头部限位轴承47分别设置在箭支头部两侧,拖住箭头防止其沿轨道滑落,旋转限位为尾部限位,所述尾部限位通过尾部的分 羽器37实现。具体限位方式如图8,左右为圆头钉,上侧为弯钩扣子29,下侧为长 板,沿箭杆法平面的四个正方向均被结构限制。通过多方限位,箭支有且仅有向前运 动的自由度。在上述实施例中,圆头螺钉为点接触限位,保证较小的限位阻力。分羽 器37由左右直线气缸34驱动,直线气缸34通过夹块固定在基准碳纤维板48和上侧 连接板30之间。The arrow limit is shown in Figure 9, which is divided into fixed limit and movable limit. The movable limit has degrees of freedom, and the fixed limit is fixed relative to the tilt head. The fixed limit includes the left and right limit, the lower limit, the head limit and the upper limit, and the rotation limit is the tail limit; The rotary pressing cylinder 32 is fixedly connected to the rotary pressing cylinder fixing seat 31 , the front end of the rotary pressing cylinder fixing seat 31 is connected to the hook button 29 , and the rotary pressing cylinder drives the hook button 29 to rotate to the arrow support Carry out the upper limit, which is an independent degree of freedom and can be opened and closed; wherein the left and right limit includes the round head nail fixing seat 28 distributed on the two ends of the upper connecting plate 30 and the rear limit connecting plate 35 and fixed on the The left and right limit round head nails 27 in the round head nail fixing seat 28, the rear limit connecting plate 35 is fixed on the rear aluminum pipe 33; The lower limit plate 43 on the reference carbon fiber board 48 and the lower limit round head nails 36 arranged between the aluminum tubes 33 on the rear side are composed of three limit round head nails on the left and right, respectively fixed on the upper connecting plate. 30 and the rear limit connecting plate 35 are distributed in the front, middle and rear parts of the tilting head structure. The lower limit round head nail 36 is connected to the lower limit pin fixing seat 38 and is fixed above the rear support plate 39, wherein the rear support plate 39 is fixedly connected between the two rear aluminum pipes 33 through the cylinder head fixing seat 40; The head limit includes a head limit support block 45, a head limit support 46 and a head limit bearing 47. The head limit support block 45 is fixedly connected to the reference carbon fiber board 48, and the head limit The support 46 is fixed on the head limit support block 45, the head limit bearing 47 is fixed on the head limit support, and the head limit bearings 47 on both sides are respectively arranged on both sides of the arrow head. The arrow is dragged to prevent it from sliding down the track, and the rotation limit is the tail limit, which is realized by the feather divider 37 at the tail. The specific limiting method is shown in Figure 8, the left and right are round head nails, the upper side is the hook button 29, the lower side is the long plate, and the four positive directions along the normal plane of the arrow shaft are all limited by the structure. Through the multi-directional limit, the arrow has and only the freedom of forward movement. In the above-mentioned embodiment, the round head screw is a point contact limiter, which ensures a small limiter resistance. The feather separator 37 is driven by the left and right linear cylinders 34, and the linear cylinders 34 are fixed between the reference carbon fiber plate 48 and the upper connecting plate 30 through a clamping block.

上侧连接板30和基准碳纤维板48之间依次设有气缸尾部长夹块42和气缸尾部短夹块41和直线气缸34,分羽器37滑动连接在直线气缸34上。直线气缸34可以带动 分羽器37实现前后伸缩,摆正箭羽。Between the upper connecting plate 30 and the reference carbon fiber plate 48 are sequentially provided a cylinder tail long clamping block 42 , a cylinder tail short clamping block 41 and a linear cylinder 34 , and the feather separator 37 is slidably connected to the linear cylinder 34 . The linear cylinder 34 can drive the feather splitter 37 to expand and contract back and forth, and to straighten the feathers.

箭支限位机构和所述发射驱动机构整体通过固定连接件安装在所述两自由度云台 上,所述固定连接件包括基准碳纤维板48、前侧铝管26,后侧铝管33和上侧连接板 30,其中前侧铝管26固定连接在基准碳纤维板48前端左右两侧,后侧铝管33固定连 接在基准碳纤维板48后端左右两侧并向后悬挑,所述上侧连接板30固定在所述前侧 铝管26的上表面,其中前侧铝管26外侧与俯仰支撑板21固定连接。The arrow limiting mechanism and the launch drive mechanism are integrally mounted on the two-degree-of-freedom pan/tilt through a fixed connector, and the fixed connector includes a reference carbon fiber plate 48, a front aluminum tube 26, a rear aluminum tube 33 and The upper connecting plate 30, wherein the front aluminum tubes 26 are fixedly connected to the left and right sides of the front end of the reference carbon fiber board 48, and the rear aluminum tubes 33 are fixedly connected to the left and right sides of the rear end of the reference carbon fiber board 48 and cantilevered backwards. The side connecting plate 30 is fixed on the upper surface of the front aluminum tube 26 , wherein the outer side of the front aluminum tube 26 is fixedly connected to the pitch support plate 21 .

发射驱动部分如图11所示,分为发射部分和触发部分,发射部分位于基准碳纤维板48上侧,触发部分位于基准碳纤维板48下侧,他们通过上下连接件55连接。触发 部分可以带动发射部分做开合运动,合到最近时,发射部分接触箭杆,用摩擦力带动 箭杆飞出。其中发射部分结构如图12所示,包括橡胶胎皮50、轮毂49、发射驱动电 机51、上层安装板52,中层安装板53、下层安装板54、第一滑轨56,第一滑块57, 上下连接件55,所述胎皮套在轮毂49上,轮毂49套在发射驱动电机51的电机转子 上,电机安装在安装板上,上层安装板52,中层安装板53、下层安装板54依次固定 连接,下层安装板54下侧安装有第一滑块57,所述第一滑轨56固定安装在所述基准 碳纤维板48上,所述第上下连接件55固定连接在下层安装板54迪安位于两侧第一滑 块57之间,所述上下连接件55向下设置于基准碳纤维板48中的凹槽中与触发部分连 接,触发部分带动所述第一滑块57沿所述第一滑轨56滑动用于开合运动的导向。As shown in FIG. 11 , the launch driving part is divided into a launch part and a trigger part. The launch part is located on the upper side of the reference carbon fiber board 48 , and the trigger part is located on the lower side of the reference carbon fiber board 48 , and they are connected by the upper and lower connecting pieces 55 . The trigger part can drive the launch part to open and close, and when it is closed to the nearest point, the launch part contacts the arrow shaft and drives the arrow shaft to fly out with friction. The launch part structure is shown in Figure 12, including rubber tire skin 50, wheel hub 49, launch drive motor 51, upper mounting plate 52, middle mounting plate 53, lower mounting plate 54, first slide rail 56, first slider 57 , the upper and lower connectors 55, the tire skin is sleeved on the hub 49, the hub 49 is sleeved on the motor rotor of the launch drive motor 51, the motor is installed on the mounting plate, the upper mounting plate 52, the middle mounting plate 53, the lower mounting plate 54 The first sliding block 57 is installed on the lower side of the lower mounting plate 54, the first sliding rail 56 is fixedly installed on the reference carbon fiber board 48, and the first upper and lower connecting pieces 55 are fixedly connected to the lower mounting plate 54. Dean is located between the first sliders 57 on both sides, and the upper and lower connecting pieces 55 are downwardly arranged in the grooves in the reference carbon fiber board 48 to connect with the trigger part, and the trigger part drives the first slider 57 along the The first slide rail 56 slides to guide the opening and closing movement.

触发部分如图13所示,包括曲轴前段70,曲轴中段69和曲轴后段66;所述曲轴 前段70和曲轴后段66通过中段上的孔固定连接;所述曲轴前段70通过曲轴前段支撑 轴承71安装在前端固定座上,前端固定座与基准碳纤维板48固定连接,曲轴后段66 通过第二压片联轴器65与曲轴电机63的电机轴连接,曲轴电机63通过曲轴电机座 64与基准碳纤维板48连接,两曲柄67两侧各安装曲柄承力轴承62,另一端安装滚针 轴承68,两曲柄67分别安装在曲轴前段70和曲轴中段69、曲轴中段69和曲轴后段 66之间,所述曲柄67的另外一端通过滑动承力轴承58与滑动座子59连接,带动滑 动座子59做开合运动,所述滑动座子59下侧安装第二滑块60,第二滑块60下侧设 有第二滑轨61,第二滑轨61和第二滑块60起导向作用。As shown in Figure 13, the triggering part includes a crankshaft front section 70, a crankshaft middle section 69 and a crankshaft rear section 66; the crankshaft front section 70 and the crankshaft rear section 66 are fixedly connected through the holes on the middle section; the crankshaft front section 70 supports the bearing through the crankshaft front section 71 is installed on the front end fixing seat, the front end fixing seat is fixedly connected with the reference carbon fiber plate 48, the rear section 66 of the crankshaft is connected with the motor shaft of the crankshaft motor 63 through the second pressing coupling 65, and the crankshaft motor 63 is connected with the crankshaft motor seat 64 through the crankshaft motor. The reference carbon fiber plate 48 is connected, the crank bearing 62 is installed on both sides of the two cranks 67, and the needle roller bearing 68 is installed at the other end. During the time, the other end of the crank 67 is connected with the sliding seat 59 through the sliding bearing 58, and drives the sliding seat 59 to open and close. The second sliding block 60 is installed on the lower side of the sliding seat 59. The lower side of the block 60 is provided with a second sliding rail 61, and the second sliding rail 61 and the second sliding block 60 play a guiding role.

本发明中机器人可实现的动作和功能:Actions and functions that the robot can realize in the present invention:

(1)云台偏航电机带动偏航齿圈转动,使得偏航大轴承以上所有结构沿轴承中心旋转,发射轨道调整到任意偏航角;(1) The yaw motor of the gimbal drives the yaw ring gear to rotate, so that all the structures above the yaw large bearing rotate along the center of the bearing, and the launch track is adjusted to any yaw angle;

(2)云台俯仰电机带动俯仰齿轮转动,使得发射轨道沿俯仰转轴旋转,从而达到任意范围内的俯仰角度;(2) The gimbal pitch motor drives the pitch gear to rotate, so that the launch track rotates along the pitch axis, so as to achieve a pitch angle within any range;

(3)旋转下压气缸伸出,将箭锁定在机构上。(3) Rotate and press the cylinder to extend to lock the arrow on the mechanism.

(4)尾部分羽气缸伸出,锁定箭的旋转角。(4) The tail feather cylinder is extended to lock the rotation angle of the arrow.

(5)触发电机旋转180度,两驱动轮间距由最大变为最小,略小于箭的直径。(5) The trigger motor rotates 180 degrees, and the distance between the two driving wheels changes from the largest to the smallest, which is slightly smaller than the diameter of the arrow.

(6)驱动电机给驱动轮提供扭力,扭力通过摩擦转化为为向前的推力,之后向前射出。(6) The drive motor provides torque to the drive wheel, and the torque is converted into forward thrust through friction, and then shot forward.

为实现多样的抛物线轨迹,发射采取两自由度云台,动作(1)(2)能够实现以机构本 体为中心的一定范围内的任意方向矢量对准,配合发射驱动部分的不同出速度,可以实现实 现投射任意的抛物轨迹,实现一定范围内的任意点以任意角度落箭。准确的限位可以保证高 的发射精度。动作(3)(4)实现了对发射对象的5自由度限制,旋转下压为箭支装填提供 便利,除左右钉限位和上下板限位外,分羽机构即旋转限位不仅可以防止箭的旋转,还为发 射驱动提供方便,防止驱动部分与箭尾产生干涉。头托即前后限位保证统一的箭支前后位置, 从而保证驱动部分相同的作用时间,保证落点精度。动作(5)(6)为最终发射动作,如附 图16(e)和16(f)所示。发射动作的触发由曲轴实现,如附图15(a)和(b)、(c)和(d)所示。准备状态下曲轴位于零位,曲轴处于张开状态,如图15(a)所示,发射驱动电机51 和电机滑台处于距中心最远位置。发射需要触发时,发射触发电机沿如图如图15(b)方向 逆时针旋转,带动连杆内端沿着圆周运动,曲轴、连杆和滑动座子可以看作是曲柄滑块机构,滑块会产生与圆周运动沿导轨方向投影相同的运动,表现为向内运动,滑块座子带动上下连 接件做合运动,上下连接件带动发射驱动电机及其固定座做合运动。直到如图15(d)所示 的状态,曲轴旋转180度,连杆达到极限位置,并且进入机构死点,发射驱动电机合运动到 达最近点,与箭杆产生夹紧力,此时夹箭的反作用力无法传递给电机,保证了夹紧精度。单 边滑块模组的行程为曲轴偏心距的两倍,总张夹距离为其四倍。最小距离状态下,箭杆夹持 处于过盈状态。所有动作过程驱动电机一直处于旋转状态,当曲轴夹紧后,电机的扭矩即刻 通过摩擦转化为对箭向前的摩擦力,推动箭向前运动,完成发射过程。发射完成后,曲轴反 向运动180度,实现发射的逆过程回到初始状态。In order to realize various parabolic trajectories, the launch adopts a two-degree-of-freedom head. Actions (1) and (2) can achieve any direction vector alignment within a certain range centered on the body of the mechanism. Realize the realization of projecting any parabolic trajectory, and realize any point within a certain range to drop arrows at any angle. Accurate limit can ensure high transmission accuracy. Actions (3) and (4) realize the 5-DOF limitation on the launching object, and the rotation and pressing down facilitates the loading of arrows. The rotation of the arrow also provides convenience for the launch drive, preventing the drive part from interfering with the nock tail. The head rest is the front and rear limit to ensure a uniform front and rear position of the arrow, thereby ensuring the same action time of the driving part and ensuring the accuracy of the landing point. Actions (5) and (6) are the final firing actions, as shown in Figures 16(e) and 16(f). The firing action is triggered by the crankshaft, as shown in Figures 15(a) and (b), (c) and (d). In the ready state, the crankshaft is in the zero position, and the crankshaft is in the open state. As shown in Figure 15(a), the launch drive motor 51 and the motor slide table are in the farthest position from the center. When the launch needs to be triggered, the launch trigger motor rotates counterclockwise in the direction shown in Figure 15(b), and drives the inner end of the connecting rod to move in a circle. The crankshaft, connecting rod and sliding seat can be regarded as a crank-slider mechanism. The block will produce the same motion as the circular motion projected along the direction of the guide rail, which is shown as an inward movement. Until the state shown in Figure 15(d), the crankshaft rotates 180 degrees, the connecting rod reaches the limit position, and enters the dead center of the mechanism, the launch drive motor moves together to the closest point, and generates a clamping force with the arrow shaft. At this time, the arrow clamps The reaction force cannot be transmitted to the motor, which ensures the clamping accuracy. The stroke of the single-sided slider module is twice the eccentric distance of the crankshaft, and the total clamping distance is four times. In the minimum distance state, the shaft clamping is in an interference state. The drive motor is always in a rotating state during all actions. When the crankshaft is clamped, the torque of the motor is instantly converted into a frictional force against the arrow forward through friction, which pushes the arrow forward to complete the firing process. After the launch is completed, the crankshaft moves 180 degrees in the reverse direction to realize the reverse process of launching and return to the initial state.

以上是对本发明的较佳实施进行了具体说明,但本发明并不限于所述实施例,熟悉本领域的技术人员在不违背本发明精神的前提下还可做作出种种的等同变形或替 换,这些等同的变形或替换均包含在本申请权利要求所限定的范围内。The above is a specific description of the preferred implementation of the present invention, but the present invention is not limited to the described embodiments, and those skilled in the art can also make various equivalent deformations or replacements without departing from the spirit of the present invention, These equivalent modifications or substitutions are all included within the scope defined by the claims of the present application.

Claims (10)

1.一种两自由度的箭矢投射机构,其特征在于:包括两自由度云台、箭支限位机构和发射驱动机构,其中,1. an arrow projection mechanism of two degrees of freedom, is characterized in that: comprise two degrees of freedom platform, arrow limiter mechanism and launch drive mechanism, wherein, 所述两自由度云台包括俯仰驱动模块和偏航驱动模块,所述箭支限位机构和发射驱动机构整体安装在所述两自由度云台上,俯仰驱动模块和偏航驱动模块分别使所述箭支限位机构和发射驱动机构完成俯仰运动和偏航运动;The two-degree-of-freedom cloud platform includes a pitch drive module and a yaw drive module, the arrow limit mechanism and the launch drive mechanism are integrally installed on the two-degree-of-freedom cloud platform, and the pitch drive module and the yaw drive module are respectively used. The arrow limit mechanism and the launch drive mechanism complete the pitch motion and the yaw motion; 所述箭支限位机构包括固定限位和活动限位,所述固定限位分别从上下左右四个方向对箭矢进行限位,活动限位防止箭的旋转;The arrow limit mechanism includes a fixed limit and a movable limit, the fixed limit respectively limits the arrow from four directions of up, down, left and right, and the movable limit prevents the rotation of the arrow; 所述发射驱动机构包括发射部分和触发部分,触发部分可以带动发射部分做开合运动,合到最近时,发射部分接触箭杆,用摩擦力带动箭杆飞出。The launch driving mechanism includes a launch part and a trigger part, the trigger part can drive the launch part to open and close, and when it is closed to the nearest point, the launch part contacts the arrow shaft and drives the arrow shaft to fly out with frictional force. 2.根据权利要求1所述的一种两自由度的箭矢投射机构,其特征在于,所述俯仰驱动模块和偏航驱动模块公用相同的驱动模块,所述驱动模块包括无刷伺服电机、电机座、第一压片联轴器、输出轴承、齿轮输出轴,其中所述无刷伺服电机固定安装在所述电机座上通过第一压片联轴器依次连接输出轴承和齿轮输出轴,所述齿轮输出轴的端部设有齿轮。2. The arrow projection mechanism with two degrees of freedom according to claim 1, wherein the pitch drive module and the yaw drive module share the same drive module, and the drive module comprises a brushless servo motor, A motor seat, a first compression coupling, an output bearing, and a gear output shaft, wherein the brushless servo motor is fixedly mounted on the motor seat and is sequentially connected to the output bearing and the gear output shaft through the first compression coupling, The end of the gear output shaft is provided with a gear. 3.根据权利要求2所述的一种两自由度的箭矢投射机构,其特征在于,所述俯仰驱动模块包括侧板、肋板、驱动模块、俯仰支撑轴和俯仰从动齿轮,其中,两侧板底部固定连接在偏航驱动模块上,肋板通过侧肋连接件连接在两侧板之间,驱动模块的齿轮输出轴从肋板中穿出与俯仰从动齿轮上的齿轮啮合,俯仰从动齿轮顶部设有俯仰支撑板,所述俯仰从动齿轮与所述侧板通过俯仰回转轴铰接,所述俯仰从动齿轮中间设有弧形槽,俯仰限位钉设置在所述弧形槽中并和所述侧板固定连接。3. The arrow projection mechanism with two degrees of freedom according to claim 2, wherein the pitch drive module comprises a side plate, a rib plate, a drive module, a pitch support shaft and a pitch driven gear, wherein, The bottom of the two side plates is fixedly connected to the yaw drive module, the rib plate is connected between the two side plates through the side rib connecting piece, the gear output shaft of the drive module passes through the rib plate and meshes with the gear on the pitch driven gear, The top of the pitch driven gear is provided with a pitch support plate, the pitch driven gear and the side plate are hinged through a pitch rotation axis, an arc-shaped groove is arranged in the middle of the pitch driven gear, and a pitch limit pin is arranged on the arc in the groove and fixedly connected with the side plate. 4.根据权利要求3所述的一种两自由度的箭矢投射机构,其特征在于,所述俯仰回转轴包括贯穿所述侧板和俯仰支撑板的俯仰紧定螺栓,俯仰滚针轴承设置在侧板和俯仰支撑板之间,所述侧板和俯仰支撑板两侧分别设有俯仰支撑挡边轴承,所述俯仰紧定螺栓的另一端通过俯仰紧定螺母紧固连接。4 . The two-degree-of-freedom arrow projection mechanism according to claim 3 , wherein the pitch rotation axis comprises a pitch set bolt penetrating the side plate and the pitch support plate, and a pitch needle bearing is provided with a pitch needle bearing. 5 . Between the side plate and the pitch support plate, pitch support rib bearings are respectively provided on both sides of the side plate and the pitch support plate, and the other end of the pitch tightening bolt is fastened and connected by a pitch tightening nut. 5.根据权利要求1所述的一种两自由度的箭矢投射机构,其特征在于,所述偏航驱动模块包括基座,驱动支撑板,驱动模块,偏航轴承总成,偏航从动齿圈,偏航支撑板,偏航支撑铝管;其中,所述偏航轴承总成包括偏航轴承、偏航轴承内环和偏航轴承外环,驱动模块固定连接在所述驱动支撑板上方,偏航轴承内环安装在所述驱动支撑板下方,基座,驱动支撑板,偏航轴承内环固定连接,组成部分相对大地固定,驱动模块的齿轮输出轴与偏航从动齿圈啮合传动,偏航轴承外环将轴承扣于偏航支撑板上,两个偏航支撑板将偏航从动齿圈夹于中间,偏航支撑板、偏航从动齿圈、偏航轴承外环和偏航支撑铝管相对固定。5 . The arrow projection mechanism with two degrees of freedom according to claim 1 , wherein the yaw drive module comprises a base, a drive support plate, a drive module, a yaw bearing assembly, and a yaw slave 5 . A moving ring gear, a yaw support plate, and a yaw support aluminum tube; wherein, the yaw bearing assembly includes a yaw bearing, an inner ring of the yaw bearing and an outer ring of the yaw bearing, and the drive module is fixedly connected to the drive support Above the plate, the inner ring of the yaw bearing is installed under the drive support plate, the base, the drive support plate, and the inner ring of the yaw bearing are fixedly connected, and the components are relatively fixed, and the gear output shaft of the drive module is connected to the yaw driven gear. Ring meshing transmission, the outer ring of the yaw bearing buckles the bearing on the yaw support plate, the two yaw support plates sandwich the yaw driven ring gear, the yaw support plate, the yaw driven ring gear, the yaw driven ring gear The bearing outer ring and the yaw support aluminum tube are relatively fixed. 6.根据权利要求1所述的一种两自由度的箭矢投射机构,其特征在于,所述箭支限位机构和所述发射驱动机构整体通过固定连接件安装在所述两自由度云台上,所述固定连接件包括基准碳纤维板、前侧铝管,后侧铝管和上侧连接板,其中前侧铝管固定连接在基准碳纤维板前端左右两侧,后侧铝管固定连接在基准碳纤维板后端左右两侧并向后悬挑,所述上侧连接板固定在所述前侧铝管的上表面,其中前侧铝管外侧与俯仰支撑板固定连接。6 . The arrow projection mechanism with two degrees of freedom according to claim 1 , wherein the arrow limiting mechanism and the launch driving mechanism are integrally installed on the two-degree-of-freedom cloud through a fixed connector. 7 . On the stage, the fixed connectors include a reference carbon fiber board, a front aluminum tube, a rear aluminum tube and an upper connecting plate, wherein the front aluminum tube is fixedly connected to the left and right sides of the front end of the reference carbon fiber board, and the rear aluminum tube is fixedly connected. On the left and right sides of the rear end of the reference carbon fiber board and cantilevered rearward, the upper connecting plate is fixed on the upper surface of the front aluminum tube, wherein the outer side of the front aluminum tube is fixedly connected with the pitch support plate. 7.根据权利要求6所述的一种两自由度的箭矢投射机构,其特征在于,所述旋转限位为尾部限位,所述尾部限位通过尾部的分羽器实现;所述固定限位包括左右限位,下限位、头部限位和上限位,其中左右限位包括分别分布在所述上侧连接板两端和后限位连接板上的圆头钉固定座以及固定在所述圆头钉固定座内的左右限位圆头钉,所述后限位连接板固定在后侧铝管上;所述下限位包括通过下限位板固定座固定在所述基准碳纤维板上的下限位板以及设置在后侧铝管之间的下限位圆头钉,其中下限位圆头钉通国下限位钉固定座固定在后侧支撑板上方,其中后侧支撑板固定连接在两后侧铝管之间;所述头部限位包括头部限位支撑块、头部限位支撑和头部限位轴承,所述头部限位支撑块固定连接在基准碳纤维板上,头部限位支撑固接在头部限位支撑块上,头部限位轴承固定在所述头部限位支撑上,两侧的头部限位轴承分别设置在箭支头部两侧,所述上限位包括固定在所述上侧连接板上的旋转下压气缸固定座,旋转下压气缸固定连接在所述旋转下压气缸固定座上,所述旋转下压气缸固定座前端连接弯钩扣子,旋转下压气缸带动所述弯钩扣子转动对箭支进行上限位。7 . The arrow projection mechanism with two degrees of freedom according to claim 6 , wherein the rotation limit is a tail limit, and the tail limit is realized by a feather divider at the tail; the fixed The limit includes the left and right limit, the lower limit, the head limit and the upper limit, wherein the left and right limit includes the round head nail fixing seats distributed on the two ends of the upper connecting plate and the rear limit connecting plate respectively, and the The left and right limit round head nails in the round head nail fixing seat, the rear limit connecting plate is fixed on the rear aluminum pipe; the lower limit includes being fixed on the reference carbon fiber board through the lower limit plate fixing seat The lower limit plate and the lower limit round head nails arranged between the aluminum tubes on the rear side, wherein the lower limit round head nails pass through the country and the lower limit nail fixing seat is fixed above the rear side support plate, wherein the rear side support plate is fixedly connected to the two. Between the rear aluminum tubes; the head limit includes a head limit support block, a head limit support and a head limit bearing, the head limit support block is fixedly connected to the reference carbon fiber board, and the head limit The upper limit support is fixed on the head limit support block, the head limit bearing is fixed on the head limit support, and the head limit bearings on both sides are respectively arranged on both sides of the arrow head, so the head limit bearing is fixed on the head limit support. The upper limit includes a rotary pressing cylinder fixing seat fixed on the upper connecting plate, the rotary pressing cylinder is fixedly connected to the rotary pressing cylinder fixing seat, and the front end of the rotary pressing cylinder fixing seat is connected with a hook The button is rotated and the pressing cylinder drives the hook button to rotate to upper limit the arrow. 8.根据权利要求6所述的一种两自由度的箭矢投射机构,其特征在于,所述上侧连接板和基准碳纤维板之间依次设有气缸尾部长夹块和气缸尾部短夹块和直线气缸,分羽器固定连接在直线气缸气缸杆上。8 . The arrow projection mechanism with two degrees of freedom according to claim 6 , wherein a cylinder tail long clamp block and a cylinder tail short clamp block are sequentially arranged between the upper connecting plate and the reference carbon fiber plate. 9 . And the linear cylinder, the feather separator is fixedly connected to the cylinder rod of the linear cylinder. 9.根据权利要求1所述的一种两自由度的箭矢投射机构,其特征在于,所述发射部分包括橡胶胎皮、轮毂、发射驱动电机、上层安装板,中层安装板、下层安装板、第一滑轨,第一滑块,上下连接件,所述胎皮套在轮毂上,轮毂套在发射驱动电机的电机转子上,电机安装在安装板上,上层安装板,中层安装板、下层安装板依次固定连接,下层安装板下侧安装有第一滑块,所述第一滑轨固定安装在所述基准碳纤维板上,所述第上下连接件固定连接在下层安装板且位于两侧第一滑块之间,所述上下连接件向下设置于基准碳纤维板中的凹槽中与触发部分连接,触发部分带动所述第一滑块沿所述第一滑轨滑动用于开合运动的导向。9 . The arrow projection mechanism with two degrees of freedom according to claim 1 , wherein the launching part comprises a rubber tire skin, a wheel hub, a launching drive motor, an upper-layer mounting plate, a middle-layer mounting plate, and a lower-layer mounting plate. 10 . , The first slide rail, the first slider, the upper and lower connecting parts, the tire skin is sleeved on the hub, the hub is sleeved on the motor rotor of the launch drive motor, the motor is installed on the mounting plate, the upper mounting plate, the middle mounting plate, The lower mounting plate is fixedly connected in sequence, a first slider is installed on the lower side of the lower mounting plate, the first sliding rail is fixedly installed on the reference carbon fiber board, and the first upper and lower connecting pieces are fixedly connected to the lower mounting plate and are located on the two sides. Between the side first sliders, the upper and lower connecting pieces are downwardly arranged in the grooves in the reference carbon fiber board to be connected with the triggering part, and the triggering part drives the first slider to slide along the first slide rail for opening. combined movement orientation. 10.根据权利要求1所述的一种两自由度的箭矢投射机构,其特征在于,所述触发部分包括曲轴前段,曲轴中段和曲轴后段;所述曲轴前段和曲轴后段通过中段上的孔固定连接;所述曲轴前段通过曲轴前段支撑轴承安装在前端固定座上,前端固定座与基准碳纤维板固定连接,曲轴后段通过第二压片联轴器与曲轴电机的电机轴连接,曲轴电机通过曲轴电机座与基准碳纤维板连接,两曲柄两侧各安装曲柄承力轴承,另一端安装滚针轴承,两曲柄分别安装在曲轴前段和曲轴中段、曲轴中段和曲轴后段之间,所述曲柄的另外一端通过轴承与滑动座子连接,带动滑动座子做开合运动,所述滑动座子下侧安装第二滑块,第二滑块下侧设有第二滑轨,第二滑轨和第二滑块起导向作用。10. A two-degree-of-freedom arrow projection mechanism according to claim 1, wherein the trigger part comprises a crankshaft front section, a crankshaft middle section and a crankshaft rear section; the crankshaft front section and the crankshaft rear section pass through the middle section The front end of the crankshaft is fixedly connected to the front end of the crankshaft through the support bearing of the front end of the crankshaft. The crankshaft motor is connected with the reference carbon fiber board through the crankshaft motor seat. The crank bearing bearing is installed on both sides of the two cranks, and the needle roller bearing is installed on the other end. The other end of the crank is connected with the sliding seat through a bearing to drive the sliding seat to open and close. A second sliding block is installed on the lower side of the sliding seat, and a second sliding rail is arranged on the lower side of the second sliding block. The second sliding rail and the second sliding block play a guiding role.
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