CN110871900A - Space-saving high-waterproof airport - Google Patents

Space-saving high-waterproof airport Download PDF

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Publication number
CN110871900A
CN110871900A CN201811003563.0A CN201811003563A CN110871900A CN 110871900 A CN110871900 A CN 110871900A CN 201811003563 A CN201811003563 A CN 201811003563A CN 110871900 A CN110871900 A CN 110871900A
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waterproof
day window
space
saving high
airport
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赵士磊
王涛
马双义
王波
梁雪松
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Yifei Intelligent Control (tianjin) Technology Co Ltd
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Yifei Intelligent Control (tianjin) Technology Co Ltd
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    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64FGROUND 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
    • B64F1/00Ground or aircraft-carrier-deck installations
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64FGROUND 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
    • B64F1/00Ground or aircraft-carrier-deck installations
    • B64F1/02Ground or aircraft-carrier-deck installations for arresting aircraft, e.g. nets or cables

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Power-Operated Mechanisms For Wings (AREA)

Abstract

The invention discloses a space-saving high-waterproof airport, which comprises an airframe body, a parking apron, an adjusting mechanism and a waterproof mechanism, wherein an inlet and an outlet are formed at the top of the airframe body; the adjusting mechanism comprises a righting mechanism used for adjusting the relative central positioning of the parked unmanned aerial vehicle, the righting mechanism comprises two push plates which are arranged on the upper surface of the parking platform and positioned on the front side and the rear side of the parking area and driven to move forwards and backwards in opposite directions, and two push blocks which are arranged on the upper surface of the parking platform and positioned on the left side and the right side of the parking area and driven to move leftwards and rightwards in opposite directions; waterproof mechanism includes that bilateral symmetry sets up and receives the drive closure to carry out the first day window form and the second day window form that protect commodity circulation unmanned aerial vehicle to and sealing mechanism, have that the mechanism is simple, area is little and can be used for commodity circulation unmanned aerial vehicle to resist external environment's main function.

Description

空间节约型高防水机场Space-saving high-waterproof airport

技术领域technical field

本发明属于无人机技术领域,具体涉及一种空间节约型高防水机场。The invention belongs to the technical field of unmanned aerial vehicles, and in particular relates to a space-saving high-waterproof airport.

背景技术Background technique

目前,物流无人机在户外作业过程中会遇到风雨或者其他恶劣天气的状况,这往往给物 流无人机在运输过程中造成很大的损坏,甚至会出现坠机的危险,所以针对这种情况为物流 无人机设计一款提供物流无人机运输过程中遮风挡雨的装置是非常有必要的,但是,由于物 流无人机停落时体积比较庞大,其停放到遮风挡雨的装置内不仅需要很大的空间,而且对无 人机和该装置的尺寸和高度要求比较高,由于在户外环境内,机场设计不仅需要满足物流无 人机停放要求,又需要设计成一定的规格要求,方便搬运,为了能够减少机场的占地面积和 缩小自身的体积以及能够做好完全的保护好物流无人机免受外部环境的干扰,这给物流无人 机降落的机场提出了更高的要求,随着物流无人机的快速发展,解决这一问题也是迫在眉睫。At present, logistics drones will encounter wind, rain or other bad weather conditions during outdoor operations, which often cause great damage to logistics drones during transportation, and even the danger of crashing. In this case, it is very necessary for the logistics drone to design a device that provides shelter from the wind and rain during the transportation of the logistics drone. However, due to the large size of the logistics drone when it is parked, it is parked in a sheltered place. Not only does the device need a lot of space, but also the size and height of the drone and the device are relatively high. Because in the outdoor environment, the airport design not only needs to meet the parking requirements of logistics drones, but also needs to be designed to certain specifications. Requirements, easy handling, in order to reduce the footprint of the airport and reduce its own volume, and to fully protect the logistics drone from the interference of the external environment, which puts forward higher requirements for the airport where the logistics drones land. With the rapid development of logistics drones, it is urgent to solve this problem.

发明内容SUMMARY OF THE INVENTION

本发明的目的在于克服现有技术的不足,提供一种空间节约型高防水机场,该空间节约 型高防水机场具有机构简单,占地面积小且能够用于物流无人机抵御外界环境的主要功能优 点。The purpose of the present invention is to overcome the deficiencies of the prior art, and to provide a space-saving high-waterproof airport, the space-saving high-waterproof airport has the main features of simple structure, small footprint, and can be used for logistics drones to resist the external environment. Functional advantages.

本发明是通过以下技术方案实现的:The present invention is achieved through the following technical solutions:

一种空间节约型高防水机场,包括顶部形成有进出口的机舱体、受驱动可升降地设置在 所述的架体内部且中心形成有停机位的停机坪台,用以调整降落在所述的停机坪台上的无人 机位置的调整机构、以及设置在所述的进出口的防水机构;A space-saving high-waterproof airport, comprising a nacelle body with an inlet and outlet formed on the top, an apron platform that is driven and can be raised and lowered inside the frame body, and a parking space is formed in the center, for adjusting the landing on the The adjustment mechanism for the position of the drone on the apron platform, and the waterproof mechanism set at the entrance and exit;

所述的调整机构包括用于调整使停落的无人机相对居中定位的正位机构,所述的正位机 构包括两个设置在所述的停机坪台上表面且位于停机区前后两侧受驱动前后相向运动的推 板,以及两个设置在停机坪台上表面且位于停机区左右两侧受驱动沿左右相向运动的推块;The adjustment mechanism includes an upright mechanism for adjusting the relative centering of the parked UAV, and the upright mechanism includes two arranged on the upper surface of the parking pad platform and located on the front and rear sides of the parking area. A push plate that is driven to move in opposite directions in the front and rear, and two push blocks that are arranged on the upper surface of the apron platform and located on the left and right sides of the parking area and are driven to move in opposite directions along the left and right sides;

所述的防水机构包括左右对称设置且受驱动闭合对所述的物流无人机进行防护的第一天 窗体和第二天窗体,以及用于对闭合状态的所述的第一天窗体和第二天窗体密封的密封机构。The waterproof mechanism includes a first-day window and a second-day window that are symmetrically arranged and driven to close to protect the logistics drone, and the first skylight that is used for the closed state. The body and the next day the form is sealed by the sealing mechanism.

在上述技术方案中,所述的正位机构还包括均设置所述的停机坪台上在两个第一丝杠驱 动机构和两个第二丝杠驱动机构,两个所述的第一丝杠驱动机构用于驱动所述的推板,两个 所述的第二丝杠驱动机构用于驱动所述的推块。In the above technical solution, the positioning mechanism further includes two first screw driving mechanisms and two second screw driving mechanisms, both of which are arranged on the parking platform, and the two first screw driving mechanisms The rod driving mechanism is used for driving the push plate, and the two second screw driving mechanisms are used for driving the push block.

在上述技术方案中,驱动所述的停机坪台上下动作的升降机构包括两个丝杠升降机构, 所述的两个丝杠升降机构的丝杠分别竖直地安装在所述的停机坪台的左侧中心位置和右侧中 心位置,所述的丝杠升降机构的螺母与所述的停机坪台固定连接。In the above technical solution, the lifting mechanism that drives the landing pad platform to move up and down includes two lead screw lifting mechanisms, and the lead screws of the two lead screw lifting mechanisms are respectively vertically installed on the landing pad platform. the left center position and the right center position, the nut of the lead screw lifting mechanism is fixedly connected with the apron platform.

在上述技术方案中,所述的升降机构还包括导向模组,所述的导向模组包括四个分别固 定在所述的停机坪台的四个角的导向杆,停机坪台的四个角分别设置有与四个所述的导向杆 相对应的导向孔,所述的导向孔内插装有导向套。In the above technical solution, the lifting mechanism further includes a guide module, and the guide module includes four guide rods respectively fixed on the four corners of the apron platform, and the four corners of the apron platform Guide holes corresponding to the four guide rods are respectively provided, and guide sleeves are inserted into the guide holes.

在上述技术方案中,所述的机舱体包括支撑骨架和外护板,所述的支撑骨架由多根型材 杆搭建组成。In the above technical solution, the nacelle body includes a support frame and an outer guard plate, and the support frame is constructed by a plurality of profile bars.

在上述技术方案中,所述的密封机构包括设置在所述的第一天窗体的前侧边上且向前延 伸的对接唇边、设置在所述的第二天窗体上前侧边上且向前延伸的对接薄边,以及与所述的 第一天窗体或第二天窗体的前侧边固定连接的密封条,所述的对接薄边可匹配地深入所述的 对接唇边内侧并实现密封,所述的密封条于朝向对接薄边侧形成有导水槽。In the above technical solution, the sealing mechanism includes a butt lip disposed on the front side of the first day window and extending forward, and a front side edge disposed on the second day window. The butting thin edge extending upward and forward, and the sealing strip fixedly connected with the front side edge of the first-day window or the second-day window, the butting thin edge can be matched and penetrate into the butting The inner side of the lip is sealed, and the sealing strip is formed with a water guide groove on the side facing the butted thin edge.

在上述技术方案中,所述的第一天窗体和所述的第二天窗体均由多面体架构的骨架和搭 建在所述的骨架上的盖板组成,其中,所述的骨架设置有中心向上鼓起的坡面以用于将停落 在所述的第一天窗体和所述的第二天窗体上的水从其外沿位置滑落。In the above technical solution, the first day window and the second day window are both composed of a skeleton of a polyhedron structure and a cover plate built on the skeleton, wherein the skeleton is provided with The upwardly bulging slope in the center is used to slide the water parked on the first-day window and the second-day window from its outer edge position.

在上述技术方案中,所述的第一天窗体和第二天窗体的侧面盖板上均设置有骨架筋板, 所述的骨架筋板与驱动机构传动连接。In the above technical solution, the side cover plates of the first-day window and the second-day window are provided with skeleton rib plates, and the skeleton rib plates are drive-connected with the driving mechanism.

在上述技术方案中,所述的驱动机构为单侧滚珠双向丝杠以实现第一天窗体和第二天窗 体同步异向动作。In the above technical solution, the drive mechanism is a single-sided ball bidirectional screw to realize the synchronous and anisotropic movements of the first-day window and the second-day window.

在上述技术方案中,所述的密封条通过侧连接边固定设置于所述的对接唇边的内侧,所 述的对接薄边的前端部与密封条的侧连接边相顶持。In the above technical solution, the sealing strip is fixedly arranged on the inner side of the butting lip through the side connecting edge, and the front end of the butting thin edge is held against the side connecting edge of the sealing strip.

本发明的优点和有益效果为:The advantages and beneficial effects of the present invention are:

本发明的一种空间节约型高防水机场通过调整机构、防水机构以及机舱体配合使用对物 流无人机进行控制,通过调整机构不仅能够使物流无人机体积达到最小体积,还能够方便的 将物流无人机收纳到机舱体内,减少了机场的占地面积以节约了物流无人机以及机场的空间 占用面积,而且还方便防水机构对物流无人机进行保护,以用于防御外界环境。The space-saving high-waterproof airport of the present invention controls the logistics drone through the coordinated use of the adjustment mechanism, the waterproof mechanism and the cabin body. The logistics drone is stored in the cabin, which reduces the footprint of the airport to save the space occupied by the logistics drone and the airport, and also facilitates the waterproofing mechanism to protect the logistics drone for defense against the external environment.

附图说明Description of drawings

图1是本发明的一种空间节约型高防水机场的结构示意图。FIG. 1 is a schematic structural diagram of a space-saving high-waterproof airport of the present invention.

图2是本发明的一种空间节约型高防水机场的正位机构的结构示意图。FIG. 2 is a schematic structural diagram of a positioning mechanism of a space-saving high-waterproof airport of the present invention.

图3是本发明的一种空间节约型高防水机场的防水机构的结构示意图。3 is a schematic structural diagram of a waterproof mechanism of a space-saving high-waterproof airport of the present invention.

图4是本发明的一种空间节约型高防水机场的第二天窗体的结构示意图。4 is a schematic structural diagram of the second day window of a space-saving high-waterproof airport of the present invention.

图5是本发明的一种空间节约型高防水机场的第一天窗体的结构示意图。5 is a schematic structural diagram of a first-day window of a space-saving high-waterproof airport of the present invention.

图6是本发明的一种空间节约型高防水机场的导水槽这对接唇边的结构示意图。FIG. 6 is a schematic structural diagram of the abutment lip of a water guide trough of a space-saving high-waterproof airport of the present invention.

其中:in:

1:调整机构,1-1:正位机构,1-1-1:推板,1-1-2:推块,1-1-3:第一丝杠驱动机构,1-1-4:第二丝杠驱动机构,1-2:升降机构,1-2-1:丝杠升降机构,1-2-2:导向模组,1-2-2-1: 导向杆,1-2-2-2:导向孔,1-2-2-3:导向套,2:防水机构,2-1:第一天窗体,2-2:第二 天窗体,2-3:密封机构,2-3-1:对接唇边,2-3-2:对接薄边,2-3-4:导水槽,2-4:骨架 筋板,2-5:驱动机构,3:机舱体,4:停机坪台。1: Adjustment mechanism, 1-1: Positive position mechanism, 1-1-1: Push plate, 1-1-2: Push block, 1-1-3: First screw drive mechanism, 1-1-4: Second screw drive mechanism, 1-2: Lifting mechanism, 1-2-1: Screw lifting mechanism, 1-2-2: Guide module, 1-2-2-1: Guide rod, 1-2- 2-2: Guide hole, 1-2-2-3: Guide sleeve, 2: Waterproof mechanism, 2-1: First day window, 2-2: Second day window, 2-3: Sealing mechanism, 2-3-1: Butt lip, 2-3-2: Butt thin edge, 2-3-4: Water guide, 2-4: Skeleton ribs, 2-5: Drive mechanism, 3: Engine room body, 4 : Helipad platform.

对于本领域普通技术人员来讲,在不付出创造性劳动的前提下,可以根据以上附图获得 其他的相关附图。For those of ordinary skill in the art, other related drawings can be obtained from the above drawings without creative effort.

具体实施方式Detailed ways

为了使本技术领域的人员更好地理解本发明方案,下面结合附图1-6以及具体实施例进 一步说明本发明的技术方案。In order to make those skilled in the art better understand the solution of the present invention, the technical solution of the present invention is further described below in conjunction with the accompanying drawings 1-6 and specific embodiments.

实施例1Example 1

一种空间节约型高防水机场,包括顶部形成有进出口的架体、受驱动可升降地设置在所 述的架体内部且中心形成有停机位的停机坪台,用以调整包括调整降落在所述的停机坪台上 的无人机位置的调整机构1、以及设置在所述的进出口的防水机构2;A space-saving high-waterproof airport, comprising a frame body with an inlet and outlet formed on the top, an apron platform that is driven and can be raised and lowered inside the frame body, and a parking space is formed in the center, which is used for adjustment, including adjusting the landing at the The adjustment mechanism 1 for the position of the drone on the apron platform, and the waterproof mechanism 2 arranged at the entrance and exit;

调整机构1包括用于调整停落在机场上的物流无人机的位置的正位机构1-1、将物流无 人机放置在机舱体3内的升降机构1-2,以及用于缩小物流无人机体积的桨叶正位机构1-3;The adjustment mechanism 1 includes a positioning mechanism 1-1 for adjusting the position of the logistics drone parked on the airport, a lifting mechanism 1-2 for placing the logistics drone in the cabin body 3, and a reduction in logistics The blade positing mechanism 1-3 of the UAV volume;

正位机构1-1包括两个设置在停机坪台4上表面且位于停机区前后两侧受驱动前后相向 运动的推板1-1-1,以及两个设置在停机坪台4上表面且位于停机区左右两侧受驱动沿左右 相向运动的推块1-1-2;The upright mechanism 1-1 includes two push plates 1-1-1 arranged on the upper surface of the apron platform 4 and located on the front and rear sides of the parking area and driven to move in opposite directions, and two push plates 1-1-1 arranged on the upper surface of the apron platform 4 and The push blocks 1-1-2 located on the left and right sides of the parking area are driven to move in opposite directions;

防水机构2设置在机场的上方,防水机构2包括左右对称设置且受驱动闭合对物流无人 机进行防护的第一天窗体2-1和第二天窗体2-2,以及用于对闭合状态的所述的第一天窗体 和第二天窗体密封的密封机构。The waterproof mechanism 2 is arranged above the airport. The waterproof mechanism 2 includes a first-day window 2-1 and a second-day window 2-2 that are symmetrically arranged and driven to close to protect the logistics drone, and In the closed state, the first day window and the second day window are sealed by the sealing mechanism.

其中,驱动所述的停机坪台上下动作的升降机构1-2包括两个丝杠升降机构1-2-1,两 个丝杠升降机构1-2-1的丝杠分别竖直地安装在停机坪台4的左侧中心位置和右侧中心位置, 丝杠升降机构1-2-1的螺母与停机坪台4固定连接以用于将物流无人机收纳到机舱体3内;Wherein, the lifting mechanism 1-2 that drives the landing pad platform to move up and down includes two lead screw lifting mechanisms 1-2-1, and the lead screws of the two lead screw lifting mechanisms 1-2-1 are respectively vertically installed on the The left center position and the right center position of the apron platform 4, the nut of the lead screw lifting mechanism 1-2-1 is fixedly connected to the apron platform 4 for accommodating the logistics drone into the nacelle body 3;

本发明的一种空间节约型高防水机场通过调整机构、防水机构以及机舱体3配合使用对 物流无人机进行控制,停机坪台可升起然后在对无人机进行居中定位后再回落机舱内部,能 够方便的将物流无人机收纳到机舱体内,减少了机场的占地面积以节约了物流无人机以及机 场的空间占用面积,而且还方便防水机构对物流无人机进行保护,以用于防御外界环境。A space-saving high-waterproof airport of the present invention controls the logistics drone through the coordinated use of the adjustment mechanism, the waterproof mechanism and the cabin body 3. The apron platform can be raised, and the drone can be centered and then lowered to the cabin. Internally, the logistics drone can be conveniently stored in the cabin, which reduces the area of the airport to save the space occupied by the logistics drone and the airport, and it is also convenient for the waterproof mechanism to protect the logistics drone. Used to defend against the external environment.

实施例2Example 2

以实施例1为基础,正位机构1-1还包括均设置在停机坪台4上的两个第一丝杠驱动机 构1-1-3和两个第二丝杠驱动机构1-1-4,两个第一丝杠驱动机构1-1-3用于驱动推板1-1-1, 两个第二丝杠驱动机构1-1-4用于驱动推块1-1-2,以使物流无人机设置在停机坪台4的中 心位置,方便将物流无人机收纳到机舱体3内。Based on Embodiment 1, the upright mechanism 1-1 further includes two first screw driving mechanisms 1-1-3 and two second screw driving mechanisms 1-1- 4. The two first screw drive mechanisms 1-1-3 are used to drive the push plate 1-1-1, the two second screw drive mechanisms 1-1-4 are used to drive the push block 1-1-2, In order to set the logistics drone at the center of the apron platform 4 , it is convenient to store the logistics drone in the cabin body 3 .

具体实施方式如下:为了保证物流无人机的正位情况,停机坪台4上设置有用于保证物 流无人机正位情况的限位机构其包括两个分别设置在两个第一丝杠驱动机构1-1-3上的第一 位置传感器和两个分别设置在两个第二丝杠驱动机构1-1-4上的第二位置传感器,两个第一 位置传感器与两个第二位置传感器均与控制器通信连接,其中,两个第一位置传感器分别用 于对两个推板1-1-1的两端的起始位置进行限位该两个推板1-1-1在移动过程中能够对物流 无人机7推动实现前后正位,并将该限位信号传输到控制器,控制器根据接收到的该限位信 号对应停止第一丝杠驱动机构1-1-3的工作,两个推板1-1-1停止运动,然后控制器控制两 个第二丝杠驱动机构1-1-4的电机启动,两个第二位置传感器分别检测两个第二丝杠驱动机 构1-1-4的推块1-1-2的位置信号,该两个推块1-1-2在移动过程中能够对物流无人机7推 动实现左右正位,当该信号被触发时,控制器控制两个第二丝杠驱动机构1-1-4的电机停止 转动,两个推块1-1-2同时停止运动,其中,该两个第一丝杠驱动机构1-1-3和两个第二丝 杠驱动机构1-1-4均可采用滚珠丝杠驱动机构,其中,该控制器为PLC控制器。The specific implementation is as follows: in order to ensure the upright condition of the logistics drone, the parking apron 4 is provided with a limit mechanism for ensuring the upright condition of the logistics drone, which includes two respectively arranged on the two first lead screw drives The first position sensor on the mechanism 1-1-3 and the two second position sensors respectively provided on the two second screw drive mechanisms 1-1-4, the two first position sensors and the two second position sensors The sensors are all connected in communication with the controller, wherein the two first position sensors are respectively used to limit the starting positions of the two ends of the two push plates 1-1-1 when the two push plates 1-1-1 are moving During the process, the logistics drone 7 can be pushed to achieve front and rear alignment, and the limit signal can be transmitted to the controller, and the controller correspondingly stops the first screw drive mechanism 1-1-3 according to the received limit signal. Work, the two push plates 1-1-1 stop moving, then the controller controls the motors of the two second screw drive mechanisms 1-1-4 to start, and the two second position sensors detect the two second screw drives respectively. The position signal of the push block 1-1-2 of the mechanism 1-1-4, the two push blocks 1-1-2 can push the logistics drone 7 to achieve the left and right positive position during the moving process, when the signal is triggered When the controller controls the motors of the two second screw drive mechanisms 1-1-4 to stop rotating, and the two push blocks 1-1-2 stop moving at the same time, the two first screw drive mechanisms 1-1 Both -3 and the two second screw drive mechanisms 1-1-4 can adopt ball screw drive mechanisms, wherein the controller is a PLC controller.

优选地,两个推块1-1-2分别由两个第二丝杠驱动机构1-1-4驱动,当推板1-1-1完成 居中定位后,首先由一侧,如左侧的推块1-1-2推动物流无人机进行左右方向上的位置调整 直至触发到其对应的第二位置传感器,然后再驱动另一侧,即右侧的推块1-1-23-1动作,将 物流无人机驱动到左右中间位置。Preferably, the two push blocks 1-1-2 are respectively driven by the two second lead screw driving mechanisms 1-1-4. After the push plate 1-1-1 is centered, it is first driven by one side, such as the left side. The push block 1-1-2 pushes the logistics drone to adjust the position in the left and right directions until it triggers its corresponding second position sensor, and then drives the other side, that is, the push block 1-1-23- 1 action, drive the logistics drone to the left and right middle position.

实施例3Example 3

以实施例1为基础,升降机构1-2还包括导向模组1-2-2,导向模组1-2-2包括四个分 别固定在停机坪台4的四个角的导向杆1-2-2-1,停机坪台4的四个角分别设置有与四个导 向杆1-2-2-1相对应的导向孔1-2-2-2,导向孔1-2-2-2内插装有导向套1-2-2-3。机舱体3 由支撑骨架及外护板搭建而成,该支撑骨架由多根型材杆搭建组成,每一型材杆的抗拉强度 范围为80~100MPa以使其能够承受停机坪台、物流无人机等的重量。Based on Embodiment 1, the lifting mechanism 1-2 further includes a guide module 1-2-2, and the guide module 1-2-2 includes four guide rods 1- 2-2-1, the four corners of the apron platform 4 are respectively provided with guide holes 1-2-2-2 corresponding to the four guide rods 1-2-2-1, and the guide holes 1-2-2- 2 The guide sleeve 1-2-2-3 is inserted inside. The nacelle body 3 is constructed of a supporting frame and an outer guard plate. The supporting frame is composed of a plurality of profile rods. The tensile strength of each profile rod is in the range of 80-100MPa, so that it can withstand the apron platform, logistics unmanned the weight of the machine, etc.

具体实施方式:丝杠升降机构1-2-1包括:电机、丝杠以及与丝杠啮合的丝杠螺母,该 丝杠竖直设置在机场的机舱体3内,该电机与丝杠轴接,该电机固装在支撑横梁架上,丝杠 的一端通过该电机安装在支撑横梁架上,丝杠的另一端穿过停机坪台4且安装在机场的上侧 面的内侧,丝杠螺母固装在停机坪台的下底面以用于带动停机坪台上下移动,该电机与控制 器通信连接。其中,在停机坪台4左右两端设置有用于固定升降模组和导向杆1-2-2-1的支 撑横梁架。机场的四脚均通过螺钉固装在底面上以用于避免停机坪台4升降过程中出现晃动 或倾斜的情况;DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS: The lead screw lifting mechanism 1-2-1 includes: a motor, a lead screw and a lead screw nut engaged with the lead screw, the lead screw is vertically arranged in the nacelle body 3 of the airport, and the motor is connected to the lead screw shaft. , the motor is fixed on the support beam frame, one end of the lead screw is installed on the support beam frame through the motor, the other end of the lead screw passes through the apron platform 4 and is installed on the inner side of the upper side of the airport, the lead screw nut is fixed It is installed on the lower bottom surface of the apron platform to drive the apron platform to move up and down, and the motor is connected with the controller in communication. Wherein, at the left and right ends of the apron platform 4, there are supporting beam frames for fixing the lifting module and the guide rod 1-2-2-1. The four feet of the airport are fixed on the bottom surface by screws to avoid shaking or tilting during the lift of the apron platform 4;

作为优选,导向套1-2-2-3插装在导向孔1-2-2-2内且与导向孔1-2-2-2固装,导向杆 1-2-2-1固装在支撑横梁架的四个角,将停机坪台4的四个脚均通过导向套1-2-2-3套装在 导向杆1-2-2-1上,控制器控制丝杠升降机构的电机转动带动停机坪台4上下移动,导向杆 1-2-2-1能够保证停机坪台4上下垂直移动避免停机坪台4上下移动过程中出现倾斜的情况。Preferably, the guide sleeve 1-2-2-3 is inserted in the guide hole 1-2-2-2 and fixedly installed with the guide hole 1-2-2-2, and the guide rod 1-2-2-1 is fixedly installed At the four corners of the supporting beam frame, set the four feet of the apron platform 4 on the guide rod 1-2-2-1 through the guide sleeve 1-2-2-3, and the controller controls the screw lifting mechanism. The rotation of the motor drives the apron platform 4 to move up and down, and the guide rods 1-2-2-1 can ensure the vertical movement of the apron platform 4 up and down to prevent the apron platform 4 from tilting during the up and down movement.

实施例4Example 4

防水机构2的密封机构2-3包括设置在第一天窗体2-1的前侧边上且向前延伸的对接唇 边2-3-1、设置在第二天窗体2-2上前侧边上且向前延伸的对接薄边2-3-2,以及与第一天窗 体2-1或第二天窗体2-2的前侧边固定连接的密封条2-3-3,对接薄边2-3-2可匹配地深入 对接唇边2-3-1内侧并实现密封,密封条2-3-3于朝向对接薄边2-3-2侧形成有导水槽2-3-4。The sealing mechanism 2-3 of the waterproof mechanism 2 includes a butt lip 2-3-1 provided on the front side of the window 2-1 on the first day and extending forward, and provided on the window 2-2 on the second day The butting thin edge 2-3-2 on the front side edge and extending forward, and the sealing strip 2-3- 3. The butting thin edge 2-3-2 can be matched to the inner side of the butting lip 2-3-1 to achieve sealing. The sealing strip 2-3-3 is formed with a water guide groove 2 on the side facing the butting thin edge 2-3-2. -3-4.

第一天窗体2-1和第二天窗体2-2均由多面体架构的骨架和搭建在骨架上的盖板组成, 其中,骨架设置有中心向上鼓起的坡面以用于将停落在第一天窗体2-1和第二天窗体2-2上 的水从其外沿位置滑落,其中,当第一天窗体2-1和第二天窗体2-2处于闭合状态时,整体 形成中间高,两边低的结构状态,方便雨水滑落,其中,骨架的下挠为0.8mm,该骨架的自 身重量为30kg,质量轻便,并且骨架由铝型材制成,该材料重量小,强度高,盖板由PVC材 料制成,不仅减少了金属材质的使用,而且还避免了对物流无人机停落定位时产生干扰。The first-day form 2-1 and the second-day form 2-2 are both composed of a polyhedral frame skeleton and a cover plate built on the skeleton, wherein the frame is provided with a slope with the center bulging upwards for stopping the parking The water falling on the first day form 2-1 and the second day form 2-2 slides off its outer edge position, wherein when the first day form 2-1 and the second day form 2-2 are in In the closed state, the overall structure is high in the middle and low on both sides, which is convenient for rainwater to slide down. Among them, the lower deflection of the skeleton is 0.8mm, the weight of the skeleton is 30kg, and the weight is light, and the skeleton is made of aluminum. Light weight, high strength, and the cover plate is made of PVC material, which not only reduces the use of metal materials, but also avoids interference when the logistics drone is parked and positioned.

其中,第一天窗体2-1和第二天窗体2-2的侧面盖板上均设置有骨架筋板2-4,骨架筋 板2-4与驱动机构2-5传动连接。Wherein, the side cover plates of the window 2-1 on the first day and the window 2-2 on the second day are all provided with a skeleton rib plate 2-4, and the skeleton rib plate 2-4 is connected with the driving mechanism 2-5 by transmission.

驱动机构2-5为单侧滚珠双向丝杠驱动机构以实现第一天窗体2-1和第二天窗体2-2同 步异向动作,该单侧滚珠双向丝杠驱动机构包括电机(该电机为伺服电机,其功率为200W)、 丝杠以及两个分别安装在第一天窗体2-1和第二天窗体2-2上的丝杠螺母,其中,丝杠的中 间位置套装有一轴承,且该轴承固装在滚珠双向丝杠驱动机构的导轨体上,该两个丝杠螺母 带动第一天窗体2-1和第二天窗体2-2闭合或者打开,使用方便;滚珠双向丝杠可单侧设置, 另一侧仅通过导轨滑块进行导向实现整体移动,单侧驱动,成本低,使用方便,当然也可采 用双侧同步由滚珠丝杠驱动,减少天窗体的扭矩,能够防止天窗体产生撕裂的情况,使用更 加安全可靠,精确度更高。The driving mechanism 2-5 is a single-sided ball bidirectional screw driving mechanism to realize the synchronous and anisotropic actions of the first-day window 2-1 and the second-day window 2-2, and the single-sided ball bidirectional screw driving mechanism includes a motor ( The motor is a servo motor with a power of 200W), a lead screw and two lead screw nuts installed on the first-day window 2-1 and the second-day window 2-2, wherein the middle position of the lead screw There is a bearing in the sleeve, and the bearing is fixed on the guide rail body of the ball two-way screw drive mechanism. The two screw nuts drive the first day window 2-1 and the second day window 2-2 to close or open, use It is convenient; the ball bidirectional screw can be set on one side, and the other side can only be guided by the guide rail to move as a whole. It is driven on one side, with low cost and easy to use. Of course, it can also be driven by the ball screw on both sides. The torque of the window can prevent the sky window from tearing, which is more safe and reliable, and has higher precision.

进一步,以一个天窗体朝向另一天窗体的方向为前,一个天窗体背离另一天窗体的方向 为后。Further, the direction of one day form facing the other day form is taken as the front, and the direction of one day form away from the other day form is the back.

作为优选,下沉式的对接薄边2-3-2形成有对接唇边2-3-1的限位台,采用对接唇边2-3-1 覆盖在对接薄边2-3-2上能实现雨水的初级密封,同时在第一天窗体2-1和第二天窗体2-2 间设置单边固定式密封条,采用闭合后夹紧的方式利用密封条实现再次密封,同时,在密封 条上设置导水槽2-3-4,该导水槽2-3-4能够将盖合的对接薄边2-3-2和对接唇边2-3-1之 间的缝隙流入的水导出,避免了水降落到物流无人机上,达到了多次防水的目的,使用方便。 具体地,密封条包括用于连接的侧连接边以及设置在侧连接边一侧的导水槽2-3-4,密封条 通过侧连接边固定设置于对接唇边2-3-1的内侧,对接薄边2-3-2的前端部与密封条的侧连 接边相顶持。该密封条由橡胶等材质构成,具有一定的弹性,对接唇边2-3-1和侧连接边的 相顶持,首先能够增强密封效果,而且还能实现柔性定位,避免对接唇边2-3-1的硬性撞击。Preferably, the sunken butting thin edge 2-3-2 is formed with a limit platform for the butting lip 2-3-1, and the butting lip 2-3-1 is used to cover the butting thin edge 2-3-2 It can realize the primary sealing of rainwater. At the same time, a unilateral fixed sealing strip is set between the window 2-1 of the first day and the window 2-2 of the second day, and the sealing strip is used to achieve resealing by clamping after closing. , a water guide groove 2-3-4 is set on the sealing strip, and the water guide groove 2-3-4 can flow into the gap between the covered butting thin edge 2-3-2 and the butting lip 2-3-1. The water is exported, which avoids the water falling on the logistics drone, achieves the purpose of waterproofing many times, and is easy to use. Specifically, the sealing strip includes a side connecting edge for connection and a water guide groove 2-3-4 arranged on one side of the side connecting edge, and the sealing strip is fixedly arranged on the inner side of the butt lip 2-3-1 through the side connecting edge, The front end of the butted thin edge 2-3-2 is held against the side connecting edge of the sealing strip. The sealing strip is made of rubber and other materials, and has a certain elasticity. The butting lip 2-3-1 and the side connecting edge support each other, which can firstly enhance the sealing effect, and can also achieve flexible positioning, avoiding the butting lip 2- 3-1 hard hit.

第一天窗体2-1和第二天窗体2-2闭合能够将停落在机舱体3的物流无人机封闭,避免 了物流无人机受到外界环境的影响。The closing of the window 2-1 on the first day and the window 2-2 on the second day can seal the logistics drone parked in the cabin body 3, so as to avoid the logistics drone from being affected by the external environment.

为了易于说明,实施例中使用了诸如“上”、“下”、“左”、“右”等空间相对术语,用于说明 图中示出的一个元件或特征相对于另一个元件或特征的关系。应该理解的是,除了图中示出 的方位之外,空间术语意在于包括装置在使用或操作中的不同方位。例如,如果图中的装置 被倒置,被叙述为位于其他元件或特征“下”的元件将定位在其他元件或特征“上”。因此,示 例性术语“下”可以包含上和下方位两者。装置可以以其他方式定位(旋转90度或位于其他方 位),这里所用的空间相对说明可相应地解释。For ease of description, spatially relative terms such as "upper", "lower", "left", "right" and the like are used in the embodiments to describe how one element or feature shown in the figures is relative to another element or feature. relation. It should be understood that, in addition to the orientation shown in the figures, spatial terms are intended to encompass different orientations of the device in use or operation. For example, if the device in the figures is turned over, elements described as "below" other elements or features would then be oriented "above" the other elements or features. Thus, the exemplary term "lower" can encompass both upper and lower positions. The device may be otherwise oriented (rotated 90 degrees or at other orientations) and the spatially relative references used herein interpreted accordingly.

而且,诸如“第一”和“第二”等之类的关系术语仅仅用来将一个与另一个具有相同名称的 部件区分开来,而不一定要求或者暗示这些部件之间存在任何这种实际的关系或者顺序。Moreover, relational terms such as "first" and "second" etc. are only used to distinguish one element from another having the same name and do not necessarily require or imply any such actual existence between those elements relationship or order.

以上对本发明做了示例性的描述,应该说明的是,在不脱离本发明的核心的情况下,任 何简单的变形、修改或者其他本领域技术人员能够不花费创造性劳动的等同替换均落入本发 明的保护范围。The present invention has been exemplarily described above. It should be noted that, without departing from the core of the present invention, any simple deformation, modification, or other equivalent replacements that can be performed by those skilled in the art without any creative effort fall into the scope of the present invention. the scope of protection of the invention.

Claims (10)

1.一种空间节约型高防水机场,其特征在于,包括顶部形成有进出口的机舱体、受驱动可升降地设置在所述的架体内部且中心形成有停机位的停机坪台,用以调整降落在所述的停机坪台上的无人机位置的调整机构(1)、以及设置在所述的进出口的防水机构(2);1. A space-saving high-waterproof airport is characterized in that, comprising a nacelle body with an inlet and outlet formed on the top, a parking pad platform that can be raised and lowered by being driven inside the frame body and a parking space is formed in the center, an adjustment mechanism (1) for adjusting the position of the drone landed on the parking apron, and a waterproof mechanism (2) arranged at the entrance and exit; 所述的调整机构(1)包括用于调整使停落的无人机相对居中定位的正位机构(1-1),所述的正位机构(1-1)包括两个设置在所述的停机坪台(4)上表面且位于停机区前后两侧受驱动前后相向运动的推板(1-1-1),以及两个设置在停机坪台(4)上表面且位于停机区左右两侧受驱动沿左右相向运动的推块(1-1-2);The adjustment mechanism (1) includes an upright mechanism (1-1) for adjusting the relative centering of the parked drone, and the upright mechanism (1-1) includes two The push plates (1-1-1) on the upper surface of the apron platform (4) and located on the front and rear sides of the parking area are driven to move in opposite directions, and two push plates (1-1-1) arranged on the upper surface of the apron platform (4) and located on the left and right of the parking area Push blocks (1-1-2) that are driven to move in opposite directions on both sides; 所述的防水机构(2)包括左右对称设置且受驱动闭合对所述的物流无人机进行防护的第一天窗体(2-1)和第二天窗体(2-2),以及用于对闭合状态的所述的第一天窗体和第二天窗体密封的密封机构。The waterproof mechanism (2) includes a first-day window (2-1) and a second-day window (2-2) that are symmetrically arranged and driven to close to protect the logistics drone, and A sealing mechanism for sealing the first day window and the second day window in the closed state. 2.根据权利要求1所述的一种空间节约型高防水机场,其特征在于,所述的正位机构(1-1)还包括均设置所述的停机坪台(4)上在两个第一丝杠驱动机构(1-1-3)和两个第二丝杠驱动机构(1-1-4),两个所述的第一丝杠驱动机构(1-1-3)用于驱动所述的推板(1-1-1),两个所述的第二丝杠驱动机构(1-1-4)用于驱动所述的推块(1-1-2)。2. A space-saving high-waterproof airport according to claim 1, characterized in that, the positioning mechanism (1-1) further comprises two apron platforms (4). A first screw drive mechanism (1-1-3) and two second screw drive mechanisms (1-1-4), the two first screw drive mechanisms (1-1-3) are used for The push plate (1-1-1) is driven, and the two second screw drive mechanisms (1-1-4) are used to drive the push block (1-1-2). 3.根据权利要求1所述的一种空间节约型高防水机场,其特征在于,驱动所述的停机坪台上下动作的升降机构(1-2)包括两个丝杠升降机构(1-2-1),所述的两个丝杠升降机构(1-2-1)的丝杠分别竖直地安装在所述的停机坪台(4)的左侧中心位置和右侧中心位置,所述的丝杠升降机构(1-2-1)的螺母与所述的停机坪台(4)固定连接。3. A space-saving high-waterproof airport according to claim 1, characterized in that the lifting mechanism (1-2) that drives the up and down movement of the apron platform comprises two lead screw lifting mechanisms (1-2). -1), the lead screws of the two lead screw lifting mechanisms (1-2-1) are respectively vertically installed at the left center position and the right center position of the parking pad platform (4), so The nut of the lead screw lifting mechanism (1-2-1) is fixedly connected with the parking pad platform (4). 4.根据权利要求3所述的一种空间节约型高防水机场,其特征在于,所述的升降机构(1-2)还包括导向模组(1-2-2),所述的导向模组(1-2-2)包括四个分别固定在所述的停机坪台(4)的四个角的导向杆(1-2-2-1),停机坪台(4)的四个角分别设置有与四个所述的导向杆(1-2-2-1)相对应的导向孔(1-2-2-2),所述的导向孔(1-2-2-2)内插装有导向套(1-2-2-3)。4. A space-saving high-waterproof airport according to claim 3, characterized in that, the lifting mechanism (1-2) further comprises a guide module (1-2-2), the guide module The group (1-2-2) includes four guide rods (1-2-2-1) respectively fixed on the four corners of the apron platform (4), and the four corners of the apron platform (4) Guide holes (1-2-2-2) corresponding to the four guide rods (1-2-2-1) are respectively provided, and the guide holes (1-2-2-2) The guide sleeve (1-2-2-3) is inserted. 5.根据权利要求1所述的一种空间节约型高防水机场,其特征在于,所述的机舱体(3)包括支撑骨架和外护板,所述的支撑骨架由多根型材杆搭建组成。5. A space-saving high-waterproof airport according to claim 1, characterized in that the cabin body (3) comprises a support frame and an outer guard plate, and the support frame is composed of a plurality of profile rods . 6.根据权利要求1所述的一种空间节约型高防水机场,其特征在于,所述的密封机构(2-3)包括设置在所述的第一天窗体(2-1)的前侧边上且向前延伸的对接唇边(2-3-1)、设置在所述的第二天窗体(2-2)上前侧边上且向前延伸的对接薄边(2-3-2),以及与所述的第一天窗体(2-1)或第二天窗体(2-2)的前侧边固定连接的密封条(2-3-3),所述的对接薄边(2-3-2)可匹配地深入所述的对接唇边(2-3-1)内侧并实现密封,所述的密封条(2-3-3)于朝向对接薄边(2-3-2)侧形成有导水槽(2-3-4)。6. A space-saving high-waterproof airport according to claim 1, characterized in that, the sealing mechanism (2-3) comprises a front side of the first-day window (2-1). A butting lip (2-3-1) on the side edge and extending forward, and a butting thin edge (2- 3-2), and the sealing strip (2-3-3) fixedly connected with the front side of the first-day window (2-1) or the second-day window (2-2), the The butting thin edge (2-3-2) can be matched to the inner side of the butting lip (2-3-1) to achieve sealing, and the sealing strip (2-3-3) is facing the butting thin edge (2-3-3). A water guide groove (2-3-4) is formed on the (2-3-2) side. 7.根据权利要求6所述的一种空间节约型高防水机场,其特征在于,所述的第一天窗体(2-1)和所述的第二天窗体(2-2)均由多面体架构的骨架和搭建在所述的骨架上的盖板组成,其中,所述的骨架设置有中心向上鼓起的坡面以用于将停落在所述的第一天窗体(2-1)和所述的第二天窗体(2-2)上的水从其外沿位置滑落。7. A space-saving high-waterproof airport according to claim 6, wherein the first day window (2-1) and the second day window (2-2) are both It is composed of a skeleton of a polyhedron structure and a cover plate built on the skeleton, wherein the skeleton is provided with a sloped surface bulging upward in the center to be used to park on the first day window (2 -1) and the water on the said second day window (2-2) slipped from its outer edge position. 8.根据权利要求7所述的一种空间节约型高防水机场,其特征在于,所述的第一天窗体(2-1)和第二天窗体(2-2)的侧面盖板上均设置有骨架筋板(2-4),所述的骨架筋板(2-4)与驱动机构(2-5)传动连接。8. A space-saving high-waterproof airport according to claim 7, characterized in that the side covers of the first-day window (2-1) and the second-day window (2-2) A skeleton rib plate (2-4) is arranged on each of the above, and the skeleton rib plate (2-4) is connected with the driving mechanism (2-5) in a driving manner. 9.根据权利要求8所述的一种空间节约型高防水机场,其特征在于,所述的驱动机构(2-5)为单侧滚珠双向丝杠以实现第一天窗体(2-1)和第二天窗体(2-2)同步异向动作。9. A space-saving high-waterproof airport according to claim 8, wherein the driving mechanism (2-5) is a one-sided ball bidirectional screw to realize the first day window (2-1). ) and the next day's form (2-2) synchronous and opposite actions. 10.根据权利要求8所述的一种空间节约型高防水机场,其特征在于,所述的密封条通过侧连接边固定设置于所述的对接唇边的内侧,所述的对接薄边的前端部与密封条的侧连接边相顶持。10. A space-saving high-waterproof airport according to claim 8, wherein the sealing strip is fixedly arranged on the inner side of the docking lip through the side connecting edge, and the docking thin edge is The front end is butted against the side connecting edge of the sealing strip.
CN201811003563.0A 2018-08-30 2018-08-30 Space-saving high-waterproof airport Pending CN110871900A (en)

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