CN113479338A - Unmanned aerial vehicle descending equipment and unmanned aerial vehicle system applying same - Google Patents
Unmanned aerial vehicle descending equipment and unmanned aerial vehicle system applying same Download PDFInfo
- Publication number
- CN113479338A CN113479338A CN202110887449.4A CN202110887449A CN113479338A CN 113479338 A CN113479338 A CN 113479338A CN 202110887449 A CN202110887449 A CN 202110887449A CN 113479338 A CN113479338 A CN 113479338A
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- Prior art keywords
- unmanned aerial
- aerial vehicle
- doors
- door
- hatch
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- 230000000903 blocking effect Effects 0.000 claims description 9
- 238000003032 molecular docking Methods 0.000 claims 1
- 230000008901 benefit Effects 0.000 abstract description 4
- 230000006872 improvement Effects 0.000 description 8
- 238000000034 method Methods 0.000 description 4
- 230000000694 effects Effects 0.000 description 3
- 238000010586 diagram Methods 0.000 description 2
- 230000008569 process Effects 0.000 description 2
- 208000035473 Communicable disease Diseases 0.000 description 1
- 230000002567 autonomic effect Effects 0.000 description 1
- 208000015181 infectious disease Diseases 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000001360 synchronised effect Effects 0.000 description 1
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Classifications
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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
- B64F1/007—Helicopter portable landing pads
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- E—FIXED CONSTRUCTIONS
- E05—LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
- E05F—DEVICES FOR MOVING WINGS INTO OPEN OR CLOSED POSITION; CHECKS FOR WINGS; WING FITTINGS NOT OTHERWISE PROVIDED FOR, CONCERNED WITH THE FUNCTIONING OF THE WING
- E05F15/00—Power-operated mechanisms for wings
- E05F15/50—Power-operated mechanisms for wings using fluid-pressure actuators
- E05F15/53—Power-operated mechanisms for wings using fluid-pressure actuators for swinging wings
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Forklifts And Lifting Vehicles (AREA)
Abstract
The invention provides unmanned aerial vehicle landing equipment and an unmanned aerial vehicle system using the same, wherein the unmanned aerial vehicle landing equipment comprises a parking case for parking an unmanned aerial vehicle, the top of the parking case is open and provided with a passage opening, the passage opening is provided with a cabin door, the cabin door is arranged in a half-and-half split mode to form two groups of half cabin doors, the two groups of half cabin doors are rotatably connected with the parking case to form an outward opening window, and a driving part for driving the half cabin doors to open and close is arranged in the parking case. The cabin door is integrally and mechanically arranged, so that the cabin door can be opened and closed by the operation driving part, and the cabin door has the advantage of higher operation efficiency.
Description
Technical Field
The invention relates to the technical field of unmanned aerial vehicles, in particular to unmanned aerial vehicle landing equipment and an unmanned aerial vehicle system using the same.
Background
Unmanned aerial vehicle is the unmanned aircraft that utilizes radio remote control equipment and program control device to control, current unmanned aerial vehicle is by the autonomic operation of on-vehicle computer, unmanned aerial vehicle can divide into military unmanned aerial vehicle and civilian unmanned aerial vehicle according to the application, military unmanned aerial vehicle divide into scout and target plane, the use is the civilian unmanned aerial vehicle the most extensively, civilian unmanned aerial vehicle cooperation industry is used to be the real just-needed market of unmanned aerial vehicle, at present there is extensive application in the fields of aerial photograph, agriculture, plant protection, miniature autodyne, express delivery transportation, disaster relief, observe wild animal, control infectious disease, survey and drawing, news report, electric power is patrolled and examined, the relief disaster, the movie & TV is shot, it is romantic to make, unmanned aerial vehicle's use itself has been expanded.
Unmanned aerial vehicle airport can realize unmanned aerial vehicle's automatic flight and take off and land, unmanned aerial vehicle storage is inside automatic airport, automatic airport deploys in the operation place region, realize the operation scene unmanned on duty, unmanned aerial vehicle is automatic to patrol and fly the operation, automatic landing, fill fast and trade electric high frequency normal state flight, functions such as data intelligent identification, it is not enough to have solved the personnel that unmanned aerial vehicle patrols and examines and meet and compile, the cost of commuting is high, the timeliness is poor, manual control the degree of difficulty is high, it uses inconvenient scheduling problem to patrol and examine data.
The existing unmanned aerial vehicle hangar generally carries out switching on and off on the cabin door through manual operation, and the whole working efficiency is lower, and the problem of poor practicability exists.
Disclosure of Invention
This scheme purpose provides an unmanned aerial vehicle descending equipment, can realize the switching of hatch door through operation drive division, has the higher advantage of operating efficiency.
In order to achieve the above object, an embodiment of the present invention provides an unmanned aerial vehicle landing device, including a parking box for parking an unmanned aerial vehicle, wherein a passage opening is opened at a top of the parking box, a hatch door is arranged on the passage opening cover, the hatch door is arranged in a half-and-half split manner to form two half hatch doors, the two half hatch doors and the parking box are rotatably connected to form an outward opening window, and a driving portion for driving the half hatch doors to open and close is arranged in the parking box.
Through carrying out holistic mechanized setting to the hatch door, make the switching that operation drive division can realize the hatch door, have the higher advantage of operating efficiency, its whole practicality is higher, more excellent, this drive division can with controller electric connection, so operating personnel can control the switch of hatch door through long-range control end, and its concrete application method does not describe here again tiredly.
As an improvement of the above scheme, the driving part comprises a telescopic hydraulic cylinder, the telescopic hydraulic cylinder is rotatably connected with the shutdown box, and a telescopic shaft of the telescopic hydraulic cylinder is rotatably connected with one side of the half-cabin door;
the driving parts are provided with two groups and are arranged corresponding to the two groups of half-cabin doors.
As an improvement of the scheme, the stopping case is provided with an avoiding groove for the half cabin door to rotate.
As an improvement of the scheme, the splicing position formed by the two half doors is positioned in the middle of the parking box.
As an improvement of the scheme, the two half cabin doors are respectively and rotatably connected with the shutdown box through a rotating shaft, and the telescopic shaft is positioned on one side of the rotating shaft far away from the splicing part.
As an improvement of the scheme, the telescopic hydraulic cylinder is arranged at the bottom of the parking case.
As an improvement of the scheme, one side of one group of the half-cabin doors is provided with a blocking convex edge in a protruding mode, and the other group of the half-cabin doors are provided with grooves for the blocking convex edge to sink into matching, so that the splicing positions of the stacked lap joint are formed.
As an improvement of the scheme, when the blocking convex edge sinks into the groove, the cabin door is horizontal.
As an improvement of the scheme, the driving part is arranged in a mirror image mode.
The invention also provides an unmanned aerial vehicle system which comprises the unmanned aerial vehicle landing equipment.
Drawings
Fig. 1 is a schematic structural diagram of an embodiment of the present invention.
Detailed Description
The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only a part of the embodiments of the present invention, and not all of the embodiments. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present invention.
Referring to fig. 1, fig. 1 is a schematic structural diagram of an embodiment of the present invention.
The utility model provides an unmanned aerial vehicle descending equipment, stops quick-witted case 1 that stops that unmanned aerial vehicle parks, stops 1 top of quick-witted case and opens and be provided with passway 2, and passway 2 lid is equipped with the hatch door, and the hatch door is to half the split type setting and forms two sets of half hatch doors 3, and two sets of half hatch doors 3 rotate with stop quick-witted case 1 and are connected and form the outward opening window, stop the drive division that is provided with the 3 switchs of half hatch doors of drive in quick-witted case 1.
It should be noted that, in this embodiment, the two half doors 3 are respectively rotatably connected to the parking box 1 through the rotating shaft 4, and meanwhile, in order to expand the deployment area of the doors as much as possible, the telescopic shaft 7 is located on a side of the rotating shaft 4 away from the joint 5 of the two half doors 3.
The driving parts are further detailed, and in the embodiment, two groups of driving parts are arranged, and are arranged corresponding to the two groups of half doors 3. The driving part comprises a telescopic hydraulic cylinder 6, wherein the telescopic hydraulic cylinder 6 is rotatably connected with the parking case 1, the telescopic hydraulic cylinder is arranged at the bottom of the parking case 1, and a telescopic shaft 7 of the telescopic hydraulic cylinder 6 is rotatably connected with one side of the half-cabin door 3. Further, in order to optimize the synchronous rotation effect of the two half doors 3, the driving parts are arranged in a mirror image mode. Therefore, the retractable hydraulic cylinder 6 is operated to perform retractable movement, so that the opening and closing operation of the cabin door can be correspondingly controlled, and the specific operation process is as follows:
when the cabin door needs to be opened, the telescopic hydraulic cylinder 6 is operated to drive the telescopic shaft 7 of the telescopic hydraulic cylinder 6 to contract, at the moment, the telescopic shaft 7 synchronously pulls the side part of the half cabin door 3 to turn towards the inside of the shutdown box 1, the half cabin door 3 rotates around the rotating shaft 4, at the moment, the half cabin door 3 is gradually opened, when the telescopic shaft 7 contracts to the vertical state of the half cabin door 3, the whole cabin door is completely opened, and at the moment, the work of the telescopic hydraulic cylinder 6 can be stopped.
When the cabin door needs to be closed, the telescopic hydraulic cylinder 6 is operated to drive the telescopic hydraulic cylinder 6 to extend outwards, the telescopic shaft 7 synchronously pushes the side part of the half cabin door 3 to turn outwards the shutdown box 1, the half cabin door 3 rotates around the rotating shaft 4, the half cabin door 3 is gradually closed at the moment, when the telescopic shaft 7 extends outwards to the half cabin door 3 to be horizontal, the whole cabin door is completely closed, and the work of the telescopic hydraulic cylinder 6 can be stopped at the moment.
Through carrying out holistic mechanized setting to the hatch door, make the switching that operation drive division can realize the hatch door, have the higher advantage of operating efficiency, its whole practicality is higher, more excellent, this drive division can with controller electric connection, so operating personnel can control the switch of hatch door through long-range control end, and its concrete application method does not describe here again tiredly.
More preferably, in the present embodiment, the parking box 1 is provided with an escape slot 8 for rotation of the half-hatch 3.
It should be noted that the arrangement of the avoiding groove 8 can make the whole rotation process of the half-hatch 3 more flexible, and avoid the situation that the half-hatch 3 rotates to interfere with the inner wall of the shutdown box 1.
Preferably, in the present embodiment, in order to optimize the overall opening and closing effect of the cabin door, the splice 5 formed by the two half cabin doors 3 is located in the middle of the parking box 1.
Preferably, in the present embodiment, one side of one half door 3 is provided with a protruding blocking flange, and the other half door 3 is provided with a groove for the protruding blocking flange to sink into, so as to form a splicing portion 5 of the stacked lap joint. Through the setting of the range upon range of concatenation like this, this concatenation department 5 can possess the manger plate effect. Further, when the blocking convex edge sinks into the groove, the cabin door is horizontal.
The invention also provides an unmanned aerial vehicle system which comprises the unmanned aerial vehicle landing equipment.
While the foregoing is directed to the preferred embodiment of the present invention, it will be understood by those skilled in the art that various changes and modifications may be made without departing from the spirit and scope of the invention.
Claims (10)
1. The utility model provides an unmanned aerial vehicle descending equipment, is including the case that stops that supplies unmanned aerial vehicle to park, its characterized in that, it opens and is provided with the passway to shut down the roof portion, the passway flap is equipped with the hatch door, the hatch door is half split type setting and forms two sets of half hatch doors, and is two sets of half hatch doors with it rotates to connect and forms the outward opening window to shut down the case, it is provided with the drive to stop the incasement half hatch door switching drive division.
2. An unmanned aerial vehicle landing apparatus of claim 1, wherein the drive portion comprises a telescopic hydraulic cylinder, the telescopic hydraulic cylinder is rotatably connected with the shutdown box, and a telescopic shaft of the telescopic hydraulic cylinder is rotatably connected with one side of the half-cabin door;
the driving parts are provided with two groups and are arranged corresponding to the two groups of half-cabin doors.
3. An unmanned aerial vehicle landing apparatus of claim 2, wherein the parking box is provided with an escape slot for rotation of the half-hatch.
4. An unmanned aerial vehicle landing apparatus of claim 2, wherein the splice formed by the two half-doors is located in the middle of the docking station.
5. An unmanned aerial vehicle landing apparatus of claim 4, wherein two sets of half hatch doors are equally divided and are respectively connected with the shutdown box through a rotating shaft, the telescopic shaft is located on one side of the rotating shaft away from the splicing part.
6. An unmanned aerial vehicle landing apparatus of claim 5, wherein the telescopic hydraulic cylinder is disposed at the bottom of the parking box.
7. An unmanned aerial vehicle landing apparatus of claim 4, wherein one of the half-doors has a blocking flange protruding from one side thereof, and the other half-door has a groove for the blocking flange to sink into, thereby forming a stacked and overlapped splice.
8. An unmanned aerial vehicle landing apparatus of claim 7, wherein the bay door is horizontal when the blocking ledge is recessed into the recess.
9. An unmanned aerial vehicle landing apparatus of claim 2, wherein the drive portion is arranged in a mirror image.
10. An unmanned aerial vehicle system comprising the unmanned aerial vehicle landing apparatus of any of claims 1-9.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202110887449.4A CN113479338A (en) | 2021-08-03 | 2021-08-03 | Unmanned aerial vehicle descending equipment and unmanned aerial vehicle system applying same |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202110887449.4A CN113479338A (en) | 2021-08-03 | 2021-08-03 | Unmanned aerial vehicle descending equipment and unmanned aerial vehicle system applying same |
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| Publication Number | Publication Date |
|---|---|
| CN113479338A true CN113479338A (en) | 2021-10-08 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202110887449.4A Pending CN113479338A (en) | 2021-08-03 | 2021-08-03 | Unmanned aerial vehicle descending equipment and unmanned aerial vehicle system applying same |
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| CN (1) | CN113479338A (en) |
Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2002211306A (en) * | 2001-01-18 | 2002-07-31 | Toyota Auto Body Co Ltd | Cargo chamber structure of cargo vehicle |
| CN106043725A (en) * | 2016-06-30 | 2016-10-26 | 张春生 | Shipborne unmanned plane charging device |
| CN111577064A (en) * | 2020-05-22 | 2020-08-25 | 上海芝松航空科技有限公司 | Push rod driver storehouse door gear |
| CN112319835A (en) * | 2020-11-18 | 2021-02-05 | 南京新领空科技有限公司 | Unmanned aerial vehicle descending positioning device and unmanned aerial vehicle nest |
-
2021
- 2021-08-03 CN CN202110887449.4A patent/CN113479338A/en active Pending
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2002211306A (en) * | 2001-01-18 | 2002-07-31 | Toyota Auto Body Co Ltd | Cargo chamber structure of cargo vehicle |
| CN106043725A (en) * | 2016-06-30 | 2016-10-26 | 张春生 | Shipborne unmanned plane charging device |
| CN111577064A (en) * | 2020-05-22 | 2020-08-25 | 上海芝松航空科技有限公司 | Push rod driver storehouse door gear |
| CN112319835A (en) * | 2020-11-18 | 2021-02-05 | 南京新领空科技有限公司 | Unmanned aerial vehicle descending positioning device and unmanned aerial vehicle nest |
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Application publication date: 20211008 |