CN207242062U - A kind of unmanned plane landing pedestal - Google Patents

A kind of unmanned plane landing pedestal Download PDF

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Publication number
CN207242062U
CN207242062U CN201721206288.3U CN201721206288U CN207242062U CN 207242062 U CN207242062 U CN 207242062U CN 201721206288 U CN201721206288 U CN 201721206288U CN 207242062 U CN207242062 U CN 207242062U
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CN
China
Prior art keywords
push rod
longitudinal
platform
cylinder
horizontal
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Active
Application number
CN201721206288.3U
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Chinese (zh)
Inventor
杨凌
文朋
冯小淋
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Chaonongli (Zhejiang) Intelligent Technology Co.,Ltd.
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Chengdu Tianqi Technology Co Ltd
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Priority to CN201721206288.3U priority Critical patent/CN207242062U/en
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Publication of CN207242062U publication Critical patent/CN207242062U/en
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Abstract

The utility model discloses a kind of unmanned plane landing pedestal, it is related to unmanned plane field, including platform, web plate, push rod, the platform is frame structure, the web plate is arranged in the frame structure of platform, the push rod is slidably connected with platform, push rod is located above web plate, push rod includes two opposite horizontal push rods, two opposite longitudinal push rods, horizontal direction of the axis of horizontal push rod parallel to platform, the axis of longitudinal push rod is parallel to the longitudinal direction of platform, and two horizontal push rods slide along the longitudinal direction, and two longitudinal push rods are slided in transverse direction;The utility model can not only make unmanned plane rest in the designated position of platform base, also have and reduce human resources consumption, the effect for avoiding rotor casualty accident from occurring.

Description

A kind of unmanned plane landing pedestal
Technical field
It the utility model is related to unmanned plane field, more particularly to a kind of unmanned plane landing pedestal.
Background technology
Rotor wing unmanned aerial vehicle is increasingly widely used as a kind of emerging technology, and the intelligent of rotor wing unmanned aerial vehicle also becomes not The developing direction come.And the landing platform for the unmanned plane that the prior art provides simply provides one piece of smooth landing field for unmanned plane Ground, unmanned plane landing after then need manually by unmanned plane be moved to designated position charged, change battery, dosing etc. operation, people Work operation needs to wait unmanned plane rotor could carry out after completely stopping, this not only waste of manpower but also had lost time, while also easy sends out Raw rotor casualty accident.
Utility model content
The utility model aims to provide a kind of unmanned plane landing pedestal, for solving the orientation problem after unmanned plane lands.
To reach above-mentioned purpose, the technical solution adopted in the utility model is as follows:A kind of unmanned plane landing pedestal, including it is flat Platform, web plate, push rod, the platform are frame structure, and the web plate is arranged in the frame structure of platform, and the push rod is slided with platform Dynamic connection, push rod are located above web plate, and push rod includes two opposite horizontal push rods, two opposite longitudinal push rods, laterally pushes away The axis of bar is parallel to the horizontal direction of platform, and the axis of longitudinal push rod is parallel to the longitudinal direction of platform, two horizontal push rods Slide along the longitudinal direction, two longitudinal push rods are slided in transverse direction.
The push rod is connected with platform by slide, sliding block, and the slide is connected with platform, slide include horizontal slide rail, Longitudinal slide rail, horizontal push rod are connected by sliding block with longitudinal slide rail, and longitudinal push rod is connected by sliding block with horizontal slide rail.
The slide, sliding block are arranged on below web plate, and push rod is connected by connector with sliding block.
The push rod is driven by the cylinder, and cylinder is connected with platform, and cylinder includes crosswise movement cylinder, longitudinal actuating cylinder, The crosswise movement cylinder is connected with longitudinal push rod, and the longitudinal direction actuating cylinder is connected with horizontal push rod.
Preferably, the cylinder is arranged on below web plate, and the crosswise movement cylinder is connected with the sliding block in horizontal slide rail, institute Longitudinal actuating cylinder is stated to be connected with the sliding block in longitudinal slide rail.
Preferably, the cylinder is rodless cylinder, and cylinder includes cylinder block, piston, and cylinder block is connected with platform, piston It is connected with sliding block.
Preferably, the horizontal slide rail has two, and longitudinal push rod connects two horizontal slide rails.
Preferably, the longitudinal slide rail has two, and horizontal push rod connects two longitudinal slide rails.
The utility model is simple in structure, easy to manufacture, and wherein web plate has the work for the flow effects for slowing down unmanned plane rotor With;The setting of two horizontal push rods and two longitudinal push rods and cylinder, has the function that to make unmanned plane mobile on platform.
Brief description of the drawings
Fig. 1 is utility model diagram;
Fig. 2 is that the utility model removes the top-direction view after web plate;
Fig. 3 is that the utility model removes the bottom direction view after web plate.
In figure:1- platforms, 2- web plates, 3- transverse directions push rod, 4- longitudinal push rods, 5- horizontal slide rails, 6- longitudinal slide rails, 7- are horizontal Actuating cylinder, 8- longitudinal directions actuating cylinder.
Embodiment
In order to make the purpose of the utility model, technical solutions and advantages more clearly understood, below in conjunction with attached drawing, to this reality It is further elaborated with new.
As shown in Figs. 1-3, a kind of unmanned plane landing pedestal, including platform 1, web plate 2, push rod, the platform 1 are frame knot Structure, platform 1 are rectangle, and the web plate 2 is arranged in the frame structure of platform 1, and web plate 2 is flushed with the top surface of platform 1, the push rod It is slidably connected with platform 1, push rod is located at the top of web plate 2, and push rod includes two opposite 3, two opposite longitudinal directions of horizontal push rod Push rod 4, the axis of horizontal push rod 3 is parallel to the horizontal direction of platform 1, the longitudinal direction side of the axis of longitudinal push rod 4 parallel to platform 1 To two horizontal push rods 3 slide along the longitudinal direction, and two longitudinal push rods 4 are slided in transverse direction.
The push rod is connected with platform 1 by slide, sliding block, and the slide is connected with platform 1, and slide includes horizontal slide rail 5th, longitudinal slide rail 6, horizontal push rod 3 are connected by sliding block with longitudinal slide rail 6, and longitudinal push rod 4 is connected by sliding block and horizontal slide rail 5 Connect.
The slide, sliding block are arranged on the lower section of web plate 2, and push rod is connected by connector with sliding block.
The push rod is driven by the cylinder, and cylinder is connected with platform 1, and cylinder includes crosswise movement cylinder 7, longitudinal actuating cylinder 8, the crosswise movement cylinder 7 is connected with longitudinal push rod 4, and the longitudinal direction actuating cylinder 8 is connected with horizontal push rod 3.
The cylinder is arranged on the lower section of web plate 2, and the crosswise movement cylinder 7 is connected with the sliding block in horizontal slide rail 5, described vertical It is connected to actuating cylinder 8 with the sliding block in longitudinal slide rail 6.
The cylinder is rodless cylinder, and cylinder includes cylinder block, piston, and cylinder block is connected with platform, piston and sliding block Connection.
The horizontal slide rail 5 has two, and longitudinal push rod 4 connects two horizontal slide rails 5.
The longitudinal slide rail 6 has two, and horizontal push rod 3 connects two longitudinal slide rails 6.
The crosswise movement cylinder 7 has two groups, and every group has two crosswise movement cylinders 7, described two crosswise movement cylinders 7 Realize sliding in opposition for longitudinal push rod 4;The longitudinal direction actuating cylinder 8 has two groups, and every group has two longitudinal actuating cylinders 8, described Two longitudinal actuating cylinders 8 realize sliding in opposition for horizontal push rod 3.
The connector includes slider connecting plate, the push rod connecting plate being connected with each other, and slider connecting plate is connected with sliding block, pushes away Bar connecting plate connects push rod.The piston of the cylinder is connected with slider connecting plate accordingly.
To make the slider connecting plate under same slide not collide in movement, the piston of the cylinder is connected with sliding block Increase column between plate and/or equipped with different height between slider connecting plate and sliding block, increase column and be used to make at slider connecting plate In in different planes, avoid colliding;Meanwhile the dimensions and arrangement of slider connecting plate also differ, and are used for Make the slider connecting plate in inner side can be with uncrossed movement.
Before use, horizontal push rod 3 is respectively positioned on the edge of platform 1 with longitudinal push rod 4.In use, working as has unmanned plane to drop to When on web plate 2, crosswise movement cylinder 7, longitudinal actuating cylinder 8 and then two horizontal push rods 3 of longitudinal push rod 4, two are driven to net The designated position movement of plate 2, unmanned plane eventually stop designated position on the platform 1.
Certainly, the utility model can also have other various embodiments, without departing substantially from the utility model spirit and its essence In the case of, those skilled in the art can make various corresponding changes and deformation, but these phases according to the utility model The change and deformation answered should all belong to the scope of the claims appended by the utility model.

Claims (8)

  1. The pedestal 1. a kind of unmanned plane lands, it is characterised in that:Including platform (1), web plate (2), push rod, the platform (1) is frame Frame structure, the web plate (2) are arranged in the frame structure of platform (1), and the push rod is slidably connected with platform (1), and push rod is located at Above web plate (2), push rod includes two opposite horizontal push rods (3), two opposite longitudinal push rods (4), horizontal push rod (3) Axis is parallel to the horizontal direction of platform (1), and the axis of longitudinal push rod (4) is parallel to the longitudinal direction of platform (1), two transverse directions Push rod (3) slides along the longitudinal direction, and two longitudinal push rods (4) are slided in transverse direction.
  2. A kind of 2. unmanned plane landing pedestal according to claim 1, it is characterised in that:The push rod passes through with platform (1) Slide, sliding block connection, the slide are connected with platform (1), and slide includes horizontal slide rail (5), longitudinal slide rail (6), horizontal push rod (3) it is connected by sliding block with longitudinal slide rail (6), longitudinal push rod (4) is connected by sliding block with horizontal slide rail (5).
  3. A kind of 3. unmanned plane landing pedestal according to claim 2, it is characterised in that:The slide, sliding block are arranged on net Below plate (2), push rod is connected by connector with sliding block.
  4. A kind of 4. unmanned plane landing pedestal according to claim 1, it is characterised in that:The push rod is driven by the cylinder, gas Cylinder is connected with platform (1), and cylinder includes crosswise movement cylinder (7), longitudinal actuating cylinder (8), the crosswise movement cylinder (7) with Longitudinal push rod (4) connects, and the longitudinal direction actuating cylinder (8) is connected with horizontal push rod (3).
  5. A kind of 5. unmanned plane landing pedestal according to claim 4, it is characterised in that:The cylinder is arranged under web plate (2) Side, the crosswise movement cylinder (7) are connected with the sliding block in horizontal slide rail (5), the longitudinal direction actuating cylinder (8) and longitudinal slide rail (6) the sliding block connection on.
  6. A kind of 6. unmanned plane landing pedestal according to claim 5, it is characterised in that:The cylinder is rodless cylinder, Cylinder includes cylinder block, piston, and cylinder block is connected with platform (1), and piston is connected with sliding block.
  7. A kind of 7. unmanned plane landing pedestal according to claim 2, it is characterised in that:The horizontal slide rail (5) has two, Longitudinal push rod (4) connects two horizontal slide rails (5).
  8. A kind of 8. unmanned plane landing pedestal according to claim 2, it is characterised in that:The longitudinal slide rail (6) has two, Horizontal push rod (3) connects two longitudinal slide rails (6).
CN201721206288.3U 2017-09-20 2017-09-20 A kind of unmanned plane landing pedestal Active CN207242062U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201721206288.3U CN207242062U (en) 2017-09-20 2017-09-20 A kind of unmanned plane landing pedestal

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201721206288.3U CN207242062U (en) 2017-09-20 2017-09-20 A kind of unmanned plane landing pedestal

Publications (1)

Publication Number Publication Date
CN207242062U true CN207242062U (en) 2018-04-17

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Application Number Title Priority Date Filing Date
CN201721206288.3U Active CN207242062U (en) 2017-09-20 2017-09-20 A kind of unmanned plane landing pedestal

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Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110673625A (en) * 2018-07-02 2020-01-10 中光电智能机器人股份有限公司 Monitoring system, base station and control method of unmanned aerial vehicle
CN113799996A (en) * 2021-09-18 2021-12-17 河北工业大学 Unmanned aerial vehicle platform that resets based on limit switch

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110673625A (en) * 2018-07-02 2020-01-10 中光电智能机器人股份有限公司 Monitoring system, base station and control method of unmanned aerial vehicle
US11524596B2 (en) 2018-07-02 2022-12-13 Coretronic Intelligent Robotics Corporation Monitoring system, base station and control method of a drone
CN113799996A (en) * 2021-09-18 2021-12-17 河北工业大学 Unmanned aerial vehicle platform that resets based on limit switch
CN113799996B (en) * 2021-09-18 2023-05-23 河北工业大学 Unmanned aerial vehicle platform that resets based on limit switch

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GR01 Patent grant
GR01 Patent grant
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TR01 Transfer of patent right

Effective date of registration: 20211013

Address after: 315300 No. 598, enterprise East Road, Zhouxiang Town, Cixi City, Ningbo City, Zhejiang Province

Patentee after: Chaonongli (Zhejiang) Intelligent Technology Co.,Ltd.

Address before: 610000 room 3507, floor 35, building 1, No. 666, middle section of Tianfu Avenue, high tech Zone, Chengdu, Sichuan

Patentee before: CHENGDU SKYLIN TECHNOLOGY Co.,Ltd.