CN105416605A - Vehicle-mounted unmanned aerial vehicle net bumping recovery device - Google Patents
Vehicle-mounted unmanned aerial vehicle net bumping recovery device Download PDFInfo
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- CN105416605A CN105416605A CN201510807581.4A CN201510807581A CN105416605A CN 105416605 A CN105416605 A CN 105416605A CN 201510807581 A CN201510807581 A CN 201510807581A CN 105416605 A CN105416605 A CN 105416605A
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
- B64F1/00—Ground or aircraft-carrier-deck installations
- B64F1/02—Ground or aircraft-carrier-deck installations for arresting aircraft, e.g. nets or cables
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U70/00—Launching, take-off or landing arrangements
- B64U70/30—Launching, take-off or landing arrangements for capturing UAVs in flight by ground or sea-based arresting gear, e.g. by a cable or a net
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Abstract
本发明属于无人机技术领域,涉及一种车载无人机撞网回收装置,包括立柱、连杆式同步机构、阻尼机构、支臂、回收网、摆杆和车辆平台;2个支臂对称的、倾斜的固定在车辆平台上,立柱竖直方向上垂直向下的固定在支臂的顶端,每根立柱的顶端固定1个连杆式同步机构;连杆式同步机构由机构主杆和通过转轴固定在机构主杆两端的第一摆臂与第二摆臂构成,第一摆臂与第二摆臂通过连杆连接在一起;第一摆臂和第二摆臂的顶端分别连接1根摆杆,回收网固定在4根摆杆的端头。无人机机头从车头向车尾方冲向回收网6的网面,无人机的机翼对回收网6产生拉力并带动摆杆7运动,将力传递给立柱1,最后由立柱1连接的阻尼机构3完成吸能,将无人机安全回收。
The invention belongs to the technical field of unmanned aerial vehicles, and relates to a vehicle-mounted unmanned aerial vehicle collision net recovery device, including a column, a connecting rod type synchronous mechanism, a damping mechanism, a support arm, a recovery net, a swing rod and a vehicle platform; the two support arms are symmetrical It is fixed on the vehicle platform obliquely, and the vertical column is fixed vertically downward on the top of the arm. The top of each column is fixed with a link-type synchronous mechanism; the link-type synchronous mechanism consists of the main rod of the mechanism and the The first swing arm and the second swing arm are fixed on the two ends of the main rod of the mechanism through the rotating shaft. The first swing arm and the second swing arm are connected together through the connecting rod; Root fork, recovery net is fixed on the end of 4 fork. The nose of the drone rushes to the mesh surface of the recovery net 6 from the front to the rear of the vehicle, and the wings of the drone generate tension on the recovery net 6 and drive the swing rod 7 to move, and transmit the force to the column 1, which is finally connected by the column 1. The damping mechanism 3 completes the energy absorption, and the drone is recovered safely.
Description
技术领域technical field
本发明属于无人机技术领域,涉及一种车载无人机撞网回收装置。The invention belongs to the technical field of unmanned aerial vehicles, and relates to a vehicle-mounted unmanned aerial vehicle collision net recovery device.
背景技术Background technique
现有无人机系统着陆方式一般采用滑跑着陆或者机腹擦地着陆,采用滑跑方式着落要求无人机安装有起落架,起落架结构重量较大,大大减小了无人机的有效载荷量;而且滑跑着陆需要较长且平坦的跑道,在地形复杂的山区或者舰船上的使用受到很大的限制。采用机腹擦地着陆方式在接地时无人机受到的冲击载荷较大,特别是着陆姿态出现偏差或者地面较硬时,很可能造成无人机机体结构的破坏,大大减短了无人机的使用寿命。The landing method of the existing UAV system generally adopts sliding landing or belly wipe landing, and the landing of the UAV requires the UAV to be equipped with a landing gear. The weight of the landing gear structure greatly reduces the effective use of the UAV. Load capacity; and the taxiing landing requires a long and flat runway, and its use in complex terrain mountains or ships is greatly restricted. The UAV is subjected to a large impact load when it touches the ground with the belly wipe landing method, especially when the landing attitude deviates or the ground is hard, it is likely to cause damage to the UAV body structure, which greatly shortens the UAV. service life.
发明内容Contents of the invention
本发明要解决的技术问题是提供一种飞行器在回收过程中所受冲击载荷较小以及对场地回收要求不高的无人机回收装置。The technical problem to be solved by the present invention is to provide an unmanned aerial vehicle recovery device that is subjected to less impact load during the recovery process and has low requirements for site recovery.
为了解决上述技术问题,本发明的技术方案如下:In order to solve the problems of the technologies described above, the technical solution of the present invention is as follows:
一种车载无人机撞网回收装置,包括2根立柱、2个连杆式同步机构、2个阻尼机构、2个支臂、回收网、4根摆杆和车辆平台;A vehicle-mounted unmanned aerial vehicle collision net recovery device, including 2 columns, 2 link-type synchronous mechanisms, 2 damping mechanisms, 2 support arms, recovery nets, 4 swing bars and a vehicle platform;
2个支臂对称的、倾斜的固定在车辆平台上,立柱竖直方向上垂直向下的固定在支臂的顶端,每根立柱的顶端固定1个连杆式同步机构;The two support arms are symmetrically and obliquely fixed on the vehicle platform, and the vertical column is fixed vertically downward on the top of the support arm, and a link type synchronization mechanism is fixed on the top of each column;
连杆式同步机构由机构主杆和通过转轴固定在机构主杆两端的第一摆臂与第二摆臂构成,第一摆臂与第二摆臂通过连杆连接在一起;The link-type synchronous mechanism is composed of a main rod of the mechanism and a first swing arm and a second swing arm fixed at both ends of the main rod of the mechanism through a rotating shaft, and the first swing arm and the second swing arm are connected together through a connecting rod;
第一摆臂和第二摆臂的顶端分别连接1根摆杆,回收网固定在4根摆杆的端头;The tops of the first swing arm and the second swing arm are respectively connected to one swing rod, and the recovery net is fixed at the ends of the four swing rods;
所述阻尼机构为串并联可自适应式阻尼机构,由第一阻尼器和阻尼器并联串接在一起组成,阻尼器的一端连有弹簧。The damping mechanism is a series-parallel adaptive damping mechanism, which is composed of a first damper and a damper connected in parallel and in series, and a spring is connected to one end of the damper.
进一步,所述车载无人机撞网回收装置还包括固定在车辆平台上的起竖装置,所述起竖装置由液压系统和升举臂构成,液压系统连接并驱动升举臂,2个支臂对称、倾斜地固定在所述升举臂的两端。Further, the vehicle-mounted unmanned aerial vehicle crash net recovery device also includes an erecting device fixed on the vehicle platform, the erecting device is composed of a hydraulic system and a lifting arm, the hydraulic system is connected and drives the lifting arm, and the two support Arms are fixed symmetrically and obliquely at both ends of the lifting arm.
优选地,为方便运输,所述支臂由2根半支臂组装而成,一根半支臂的内插销插入到另一根半支臂的内部后,通过螺栓将两根半支臂锁定。Preferably, for the convenience of transportation, the support arm is assembled by two half-arms, and after the inner pin of one half-arm is inserted into the other half-arm, the two half-arms are locked by bolts .
进一步,第一摆臂的端点通过连杆第二摆臂的中部。Further, the end point of the first swing arm passes through the middle of the second swing arm of the connecting rod.
本发明的有益效果如下:The beneficial effects of the present invention are as follows:
连杆式同步机构:利用机构主杆端头与第一摆臂和第二摆臂转轴之间的不同距离,设计达到两摆臂(第一摆臂和第二摆臂)在一定范围内的几何运动基本同步。Link-type synchronous mechanism: Utilizing the different distances between the end of the main rod of the mechanism and the shafts of the first swing arm and the second swing arm, the design achieves that the two swing arms (the first swing arm and the second swing arm) are within a certain range. Geometric motion is basically synchronous.
阻尼机构:将第二阻尼器与弹簧串联后整体与第一阻尼器并联。使阻尼机构在吸收冲击力的过程中,先由第一阻尼器吸收能量,多余能量转化为弹簧的弹性势能后再缓慢释放。达到阻尼力在撞网前后的稳定释放,降低无人机回收损坏风险。Damping mechanism: After the second damper is connected in series with the spring, the whole is connected in parallel with the first damper. In the process of absorbing the impact force of the damping mechanism, the first damper first absorbs the energy, and the excess energy is converted into the elastic potential energy of the spring and then released slowly. Achieve stable release of damping force before and after hitting the net, reducing the risk of drone recovery damage.
起竖装置:使用液压系统(包含泵站,电机,油箱)和升举臂实现撞网回收装置的快速起竖和放倒,使回收装置能快速展开使用,方便无人机回收阵地的快速布置。Erection device: use the hydraulic system (including pump station, motor, fuel tank) and lifting arm to realize the rapid erection and downturn of the impact net recovery device, so that the recovery device can be quickly deployed and used, and it is convenient for the rapid deployment of the UAV recovery position .
支臂:使用转轴形式采用三段折叠使支臂能快速展开及回收。在转轴对接区使用内接插销增强强度。使得支臂不但安装与回收速度快,而且整体强抗弯度高,满足撞网回收装置的需求。Support arm: The use of a rotating shaft adopts three-stage folding so that the support arm can be quickly unfolded and recovered. Inner pins are used in the shaft docking area for added strength. The support arm not only has fast installation and recovery speed, but also has a high overall bending resistance, which meets the needs of the impact net recovery device.
整体便于长途运输的设计模式,可以使整套装置使用一个车辆平台就完全收纳,不但展开迅速方便,也可以快速收纳及长途运输。The overall design mode is convenient for long-distance transportation, so that the whole set of equipment can be completely stored on a vehicle platform, which is not only fast and convenient to unfold, but also can be quickly stored and long-distance transportation.
附图说明Description of drawings
图1为本发明车载无人机撞网回收装置的结构示意图;Fig. 1 is the structural representation of vehicle-mounted unmanned aerial vehicle collision net recovery device of the present invention;
图2为本发明起竖装置的结构示意图;Fig. 2 is the structural representation of erecting device of the present invention;
图3为本发明支臂由2根半支臂组装处的局部示意图;Fig. 3 is the local schematic diagram of the place where the support arm of the present invention is assembled by 2 half support arms;
图4为本发明连杆式同步机构和阻尼机构连接处的局部示意图;Fig. 4 is a partial schematic diagram of the connection between the link type synchronous mechanism and the damping mechanism of the present invention;
图5为本发明车载无人机撞网回收装置的长途运输状态示意图。Fig. 5 is a schematic diagram of the long-distance transportation state of the vehicle-mounted UAV collision net recovery device of the present invention.
具体实施方案specific implementation plan
下面结合附图对本发明做进一步描述。The present invention will be further described below in conjunction with the accompanying drawings.
一种车载无人机撞网回收装置,如图1所示,包括2根立柱1、2个连杆式同步机构2、2个阻尼机构3、起竖装置4、2个支臂5、回收网6、4根摆杆7和车辆平台8;A vehicle-mounted unmanned aerial vehicle collision net recovery device, as shown in Figure 1, includes 2 upright columns 1, 2 link type synchronous mechanisms 2, 2 damping mechanisms 3, erecting devices 4, 2 support arms 5, recovery Net 6, 4 fork bars 7 and vehicle platform 8;
如图3所示,所述支臂5由2根半支臂组装而成,一根半支臂的内插销9插入到另一根半支臂的内部后,通过螺栓将两根半支臂锁定。As shown in Figure 3, the support arm 5 is assembled by two half-arms. After the inner pin 9 of one half-arm is inserted into the inside of the other half-arm, the two half-arms are connected by bolts. locking.
固定在车辆平台8上的起竖装置4如图2所示,由液压系统10和升举臂11构成,液压系统10连接并驱动升举臂11,2个支臂5对称、倾斜地固定在所述升举臂11的两端,也就是说2个支臂5通过起竖装置4对称的、倾斜的固定在车辆平台8上,立柱1竖直方向上垂直向下的固定在支臂5的顶端,每根立柱1的顶端固定1个连杆式同步机构2;The erecting device 4 fixed on the vehicle platform 8, as shown in Figure 2, is composed of a hydraulic system 10 and a lifting arm 11, the hydraulic system 10 is connected and drives the lifting arm 11, and the two support arms 5 are symmetrically and obliquely fixed on the The two ends of the lifting arm 11, that is to say, the two support arms 5 are symmetrically and obliquely fixed on the vehicle platform 8 through the erecting device 4, and the column 1 is vertically fixed on the support arm 5 vertically downward. The top of each column 1 is fixed with a link type synchronous mechanism 2;
如图4所示,连杆式同步机构2由机构主杆和通过转轴固定在机构主杆两端的第一摆臂12与第二摆臂13构成,第一摆臂12与第二摆臂13通过连杆14连接在一起,一般情况下,第一摆臂12的端点通过连杆14第二摆臂13的中部;As shown in Figure 4, the link type synchronous mechanism 2 is made up of the main rod of the mechanism and the first swing arm 12 and the second swing arm 13 fixed on the two ends of the main rod of the mechanism through the rotating shaft. The first swing arm 12 and the second swing arm 13 Connected together by a connecting rod 14, generally, the end point of the first swing arm 12 passes through the middle of the second swing arm 13 of the connecting rod 14;
第一摆臂12和第二摆臂13的顶端分别连接1根摆杆7,回收网6固定在4根摆杆7的端头;The tops of the first swing arm 12 and the second swing arm 13 are respectively connected to a swing rod 7, and the recovery net 6 is fixed on the ends of the four swing rods 7;
所述阻尼机构3为串并联可自适应式阻尼机构,由第一阻尼器15和第二阻尼器17并联串接在一起组成,第二阻尼器17的一端连有弹簧16。The damping mechanism 3 is a series-parallel adaptive damping mechanism, composed of a first damper 15 and a second damper 17 connected in parallel and in series, and a spring 16 is connected to one end of the second damper 17 .
本实施无人机撞网回收装置的长途转运状态如图5所示,将4根摆杆7拆下并固定在搭载车辆平台8的车顶安装架上。然后2个支臂5折叠完毕同样固定在车顶安装架上。将拆卸下来的立柱及其他机构分别放入车辆平台8后部的尾箱内即可。The long-distance transfer state of the UAV collision net recovery device is shown in Figure 5. The four swing rods 7 are removed and fixed on the roof mounting frame of the vehicle platform 8. Then 2 support arms 5 are folded and are fixed on the roof mounting frame equally. Put the dismantled column and other mechanisms into the tail box at the rear of the vehicle platform 8 and get final product.
本发明工作原理如:无人机机头从车头向车尾方冲向回收网6的网面,无人机的机翼对回收网6产生拉力并带动摆杆7运动,将力传递给立柱1,最后由立柱1连接的阻尼机构3完成吸能,将无人机安全回收。The working principle of the present invention is as follows: the head of the UAV rushes towards the mesh surface of the recycling net 6 from the front of the vehicle to the rear of the vehicle, and the wings of the UAV generate a pulling force on the recycling net 6 and drive the swing rod 7 to move, and transmit the force to the column 1 , and finally the damping mechanism 3 connected by the column 1 completes the energy absorption, and the UAV is recovered safely.
阻尼机构3吸能的原理如下:通过连杆(14)保证第一摆臂12与第二摆臂13在一定的角度范围内(一般10°到70°)对称运动。在撞网回收的缓冲过程中,先由第一阻尼器15全程吸能,多余的能量转化为弹簧16拉伸的弹性势能,再由弹簧16反馈给第二阻尼器17,达到回收过程中阻尼力的合理释放。The energy absorption principle of the damping mechanism 3 is as follows: the first swing arm 12 and the second swing arm 13 are guaranteed to move symmetrically within a certain angle range (generally 10° to 70°) through the connecting rod (14). In the buffering process of hitting the net and recovering, the first damper 15 absorbs energy throughout the entire process, and the excess energy is converted into elastic potential energy stretched by the spring 16, and then fed back to the second damper 17 by the spring 16 to achieve damping during the recovery process. Reasonable release of force.
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CN107014255A (en) * | 2017-05-24 | 2017-08-04 | 大鹏高科(武汉)智能装备有限公司 | A kind of method and apparatus for aiding in unmanned boat to capture unmanned plane |
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CN112607026A (en) * | 2020-12-30 | 2021-04-06 | 山东省科学院海洋仪器仪表研究所 | Automatic recovery and release device and method for multi-rotor unmanned aerial vehicle |
CN113120249A (en) * | 2021-05-06 | 2021-07-16 | 上海交通大学 | Marine unmanned aerial vehicle jack |
CN115367139A (en) * | 2022-08-05 | 2022-11-22 | 中国船舶重工集团公司第七一三研究所 | A folding recovery device for fixed-wing unmanned aerial vehicles that is conveniently arranged on the hull |
CN115367139B (en) * | 2022-08-05 | 2025-06-06 | 中国船舶重工集团公司第七一三研究所 | A foldable recovery device for fixed-wing UAV that is convenient for deployment on a ship hull |
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