CN110001969A - A kind of unmanned plane loading mechanism - Google Patents
A kind of unmanned plane loading mechanism Download PDFInfo
- Publication number
- CN110001969A CN110001969A CN201910367965.7A CN201910367965A CN110001969A CN 110001969 A CN110001969 A CN 110001969A CN 201910367965 A CN201910367965 A CN 201910367965A CN 110001969 A CN110001969 A CN 110001969A
- Authority
- CN
- China
- Prior art keywords
- supporting plate
- unmanned plane
- telescopic rod
- pressing plate
- plate
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Pending
Links
- 230000007246 mechanism Effects 0.000 title claims abstract description 31
- 238000003825 pressing Methods 0.000 claims description 24
- 230000003139 buffering effect Effects 0.000 claims description 10
- 229920001821 foam rubber Polymers 0.000 claims description 6
- 229920001971 elastomer Polymers 0.000 claims description 3
- 238000009434 installation Methods 0.000 claims description 2
- 238000000034 method Methods 0.000 description 4
- 238000011161 development Methods 0.000 description 2
- 208000035473 Communicable disease Diseases 0.000 description 1
- 239000000872 buffer Substances 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 230000006872 improvement Effects 0.000 description 1
- 208000015181 infectious disease Diseases 0.000 description 1
- 238000007689 inspection Methods 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 238000013507 mapping Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 238000012544 monitoring process Methods 0.000 description 1
- 230000008569 process Effects 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D9/00—Equipment for handling freight; Equipment for facilitating passenger embarkation or the like
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U2101/00—UAVs specially adapted for particular uses or applications
- B64U2101/60—UAVs specially adapted for particular uses or applications for transporting passengers; for transporting goods other than weapons
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Handcart (AREA)
Abstract
The present invention provides a kind of unmanned plane loading mechanism, the upper end of the telescopic rod is detachably secured to fuselage lower end, and the lower end of telescopic rod is weldingly fixed on supporting plate upper end, there are four level locating mechanism is set, four edges of supporting plate are extended through, level locating mechanism clamps the article in supporting plate jointly.The stability of loading of the present invention is preferable, and when not needing loading, luggage carrier can be disassembled, convenient for disassembly and assembly, and the telescopic rod of use can increase the space of loading.
Description
Technical field
The present invention relates to air vehicle technique fields, more particularly, to a kind of unmanned plane loading mechanism.
Background technique
UAV abbreviation unmanned plane, english abbreviation UAV are to utilize radio robot and the program provided for oneself
The not manned aircraft of control device manipulation, or fully or is intermittently automatically operated by car-mounted computer, and manned
Aircraft is compared, and unmanned plane is often more suitable for those too slow-witted, dirty or dangerous tasks, and unmanned plane is pressed application field, can be divided into
It is military with civilian, military aspect, unmanned plane is divided into reconnaissance plane and target drone, and civilian aspect is that unmanned plane has really just needed, exists at present
It takes photo by plane, agricultural, plant protection, miniature self-timer, express transportation, disaster relief, observation wild animal, monitoring infectious disease, mapping, Xin Wen Bao
The application in road, electric inspection process, the disaster relief, movies-making and manufacture romance etc. field, has greatly expanded the use of unmanned plane itself
On the way, developed country also in actively extension industrial application and develops unmanned air vehicle technique.
With scientific and technological continuous development, unmanned plane loading, which has, significantly to be developed, its development is brought
Very big convenience.But stability when existing loading unmanned plane loading is not so good, can move, fall on luggage carrier
Danger.When not needing loading, luggage carrier can not also be disassembled, and so that flight is increased resistance, and when placing
Compare land occupation side.
Summary of the invention
In view of this, the present invention is intended to provide a kind of unmanned plane loading mechanism, is able to solve the above problem.
In order to achieve the above objectives, the technical scheme of the present invention is realized as follows:
A kind of unmanned plane loading mechanism, including supporting plate, telescopic rod and level locating mechanism, the upper end of the telescopic rod are removable
It unloads and is fixed on fuselage lower end, the lower end of telescopic rod is weldingly fixed on supporting plate upper end, and the surrounding of supporting plate is equipped with edge upwards, and level is fixed
Position mechanism extends through four edges of supporting plate, level locating mechanism clamps the article in supporting plate, telescopic rod jointly there are four setting
There are four if, it is separately fixed at four edges of supporting plate.
Further, the center of the supporting plate is equipped with placing groove, and placing groove is in rectangle.
Further, the level locating mechanism includes screw rod, handle and pressing plate, is threadedly engaged between screw rod and edge,
Hand is fixed on one end of screw rod, and pressing plate is fixed on the other end of screw rod, and handle is located on the outside of supporting plate, and pressing plate is located on the inside of supporting plate.
Further, the fuselage lower end is also removably connected with buffering pressing plate, and buffering pressing plate is located at the surface of placing groove.
Further, the buffering pressing plate is connected to the first mounting plate by spring, and the first mounting plate is bolted on
Fuselage lower end.
Further, the telescopic rod is fixed on fuselage lower end by the second mounting plate, and the second mounting plate is bolted
In fuselage lower end.
Further, the bottom in the placing groove is equipped with foam-rubber cushion, and the thickness of foam-rubber cushion is less than the depth of placing groove.
Further, the pressing plate is uniformly fixed with several rubber columns back to the side of screw rod.
Compared with the existing technology, the invention has the following advantages: the stability of loading is preferable, when not needing loading
When, luggage carrier can disassemble, and convenient for disassembly and assembly, the telescopic rod of use can increase the space of loading.
Detailed description of the invention
The attached drawing for constituting a part of the invention is used to provide further understanding of the present invention, schematic reality of the invention
It applies example and its explanation is used to explain the present invention, do not constitute improper limitations of the present invention.In the accompanying drawings:
Fig. 1 is the structural diagram of the present invention；
Fig. 2 is the positional relationship top view of supporting plate, telescopic rod and level locating mechanism；
Description of symbols:
1- fuselage；2- buffers pressing plate；3- spring；The first mounting plate of 4-；The second mounting plate of 5-；6- telescopic rod；7- handle；8-
Screw rod；9- supporting plate；10- foam-rubber cushion；11- pressing plate；The edge 12-.
Specific embodiment
It should be noted that in the absence of conflict, the feature in embodiment and embodiment in the present invention can phase
Mutually combination.
In the description of the present invention, it is to be understood that, term " center ", " longitudinal direction ", " transverse direction ", "upper", "lower",
The orientation or positional relationship of the instructions such as "front", "rear", "left", "right", "vertical", "horizontal", "top", "bottom", "inner", "outside" is
It is based on the orientation or positional relationship shown in the drawings, is merely for convenience of description of the present invention and simplification of the description, rather than instruction or dark
Show that signified device or element must have a particular orientation, be constructed and operated in a specific orientation, therefore should not be understood as pair
Limitation of the invention.In addition, term " first ", " second " etc. are used for description purposes only, it is not understood to indicate or imply phase
To importance or implicitly indicate the quantity of indicated technical characteristic.The feature for defining " first ", " second " etc. as a result, can
To explicitly or implicitly include one or more of the features.In the description of the present invention, unless otherwise indicated, " multiple "
It is meant that two or more.
In the description of the present invention, it should be noted that unless otherwise clearly defined and limited, term " installation ", " phase
Even ", " connection " shall be understood in a broad sense, for example, it may be being fixedly connected, may be a detachable connection, or be integrally connected；It can
To be mechanical connection, it is also possible to be electrically connected；It can be directly connected, can also can be indirectly connected through an intermediary
Connection inside two elements.For the ordinary skill in the art, above-mentioned term can be understood by concrete condition
Concrete meaning in the present invention.
The present invention will be described in detail below with reference to the accompanying drawings and embodiments.
As shown in Figs. 1-2, a kind of unmanned plane loading mechanism, including supporting plate 9, telescopic rod 6 and level locating mechanism, it is described to stretch
The upper end of contracting bar 6 is detachably secured to 1 lower end of fuselage, and the lower end of telescopic rod 6 is weldingly fixed on 9 upper end of supporting plate, the surrounding of supporting plate 9
It is equipped with edge 12 upwards, there are four level locating mechanism is set, extends through four edges 12 of supporting plate 9, level locating mechanism is total
With the article clamped in supporting plate 9, there are four telescopic rod 6 is set, it is separately fixed at four edges of supporting plate 9.
The center of the supporting plate 9 is equipped with placing groove, and placing groove is in rectangle.
The level locating mechanism includes screw rod 8, handle 7 and pressing plate 11, is threadedly engaged between screw rod 8 and edge 12,
Hand 7 is fixed on one end of screw rod 8, and pressing plate 11 is fixed on the other end of screw rod 8, and handle 7 is located at 9 outside of supporting plate, and pressing plate 11 is located at
9 inside of supporting plate.
1 lower end of fuselage is also removably connected with buffering pressing plate 2, and buffering pressing plate 2 is located at the surface of placing groove.
The buffering pressing plate 2 is connected to the first mounting plate 4 by spring 3, and the first mounting plate 4 is bolted on fuselage
1 lower end.
The telescopic rod 6 is fixed on 1 lower end of fuselage by the second mounting plate 5, and the second mounting plate 5 is bolted on machine
1 lower end of body.
Bottom in the placing groove is equipped with foam-rubber cushion 10, and the thickness of foam-rubber cushion 10 is less than the depth of placing groove.
The pressing plate 11 is uniformly fixed with several rubber columns back to the side of screw rod 8.For increasing article by frictional force,
More stable clamping article.
In use, placing items in placing groove, the handle 7 of hand 4 level locating mechanisms can be by article level side
To clamping, buffering pressing plate 2 the stretching due to spring 3 of top can play auxiliary cushioning effect in the vertical direction.When not needing
When loading, the pressed sheet 2 that eases up of telescopic rod 6 can be disassembled from fuselage 1 by unclamping bolt.
The foregoing is merely illustrative of the preferred embodiments of the present invention, is not intended to limit the invention, all in essence of the invention
Within mind and principle, any modification, equivalent replacement, improvement and so on be should all be included in the protection scope of the present invention.
Claims (8)
1. a kind of unmanned plane loading mechanism, it is characterised in that: described including supporting plate (9), telescopic rod (6) and level locating mechanism
The upper end of telescopic rod (6) is detachably secured to fuselage (1) lower end, and the lower end of telescopic rod (6) is weldingly fixed on supporting plate (9) upper end,
The surrounding of supporting plate (9) is equipped with edge (12) upwards, there are four level locating mechanism is set, extends through four edges of supporting plate (9)
(12), level locating mechanism clamps the article in supporting plate (9) jointly, there are four telescopic rod (6) is set, is separately fixed at supporting plate (9)
Four edges.
2. unmanned plane loading according to claim 1 mechanism, it is characterised in that: the center of the supporting plate (9) is equipped with
Placing groove, placing groove are in rectangle.
3. unmanned plane loading according to claim 2 mechanism, it is characterised in that: the level locating mechanism includes screw rod
(8), handle (7) and pressing plate (11), are threadedly engaged between screw rod (8) and edge (12), and handle (7) is fixed on the one of screw rod (8)
End, pressing plate (11) are fixed on the other end of screw rod (8), and handle (7) is located on the outside of supporting plate (9), and pressing plate (11) is located in supporting plate (9)
Side.
4. unmanned plane loading according to claim 2 mechanism, it is characterised in that: fuselage (1) lower end also detachably connects
It is connected to buffering pressing plate (2), buffering pressing plate (2) is located at the surface of placing groove.
5. unmanned plane loading according to claim 4 mechanism, it is characterised in that: the buffering pressing plate (2) passes through spring (3)
It is connected to the first mounting plate (4), the first mounting plate (4) is bolted on fuselage (1) lower end.
6. unmanned plane loading according to claim 5 mechanism, it is characterised in that: the telescopic rod (6) passes through the second installation
Plate (5) is fixed on fuselage (1) lower end, and the second mounting plate (5) is bolted on fuselage (1) lower end.
7. unmanned plane loading according to claim 2 mechanism, it is characterised in that: the bottom in the placing groove is equipped with sponge
It pads (10), the thickness of foam-rubber cushion (10) is less than the depth of placing groove.
8. unmanned plane loading according to claim 3 mechanism, it is characterised in that: the pressing plate (11) is back to screw rod (8)
Side is uniformly fixed with several rubber columns.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910367965.7A CN110001969A (en) | 2019-05-05 | 2019-05-05 | A kind of unmanned plane loading mechanism |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910367965.7A CN110001969A (en) | 2019-05-05 | 2019-05-05 | A kind of unmanned plane loading mechanism |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN110001969A true CN110001969A (en) | 2019-07-12 |
Family
ID=67175636
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201910367965.7A Pending CN110001969A (en) | 2019-05-05 | 2019-05-05 | A kind of unmanned plane loading mechanism |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN110001969A (en) |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110550199A (en) * | 2019-09-03 | 2019-12-10 | 南京唐壹信息科技有限公司 | Cantilever type agricultural transportation unmanned aerial vehicle |
| CN110641701A (en) * | 2019-10-11 | 2020-01-03 | 宁夏翼航智控科技有限公司 | Unmanned aerial vehicle's thing mechanism of hanging for fire control reconnaissance rescue |
| CN111169639A (en) * | 2019-12-26 | 2020-05-19 | 中国科学院自动化研究所南京人工智能芯片创新研究院 | Intelligent anti-terrorist equipment and system based on face recognition unmanned aerial vehicle equipment |
| CN112623181A (en) * | 2020-12-16 | 2021-04-09 | 北华航天工业学院 | Shuttle-shaped structure for aircraft |
| CN114104294A (en) * | 2021-11-30 | 2022-03-01 | 杭州科技职业技术学院 | Suspension type unmanned aerial vehicle carries thing device |
-
2019
- 2019-05-05 CN CN201910367965.7A patent/CN110001969A/en active Pending
Cited By (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110550199A (en) * | 2019-09-03 | 2019-12-10 | 南京唐壹信息科技有限公司 | Cantilever type agricultural transportation unmanned aerial vehicle |
| WO2021042378A1 (en) * | 2019-09-03 | 2021-03-11 | 南京唐壹信息科技有限公司 | Cantilever agricultural transport unmanned aerial vehicle |
| CN110641701A (en) * | 2019-10-11 | 2020-01-03 | 宁夏翼航智控科技有限公司 | Unmanned aerial vehicle's thing mechanism of hanging for fire control reconnaissance rescue |
| CN110641701B (en) * | 2019-10-11 | 2022-09-20 | 宁夏翼航智控科技有限公司 | Unmanned aerial vehicle's thing of hanging mechanism is used in fire control reconnaissance rescue |
| CN111169639A (en) * | 2019-12-26 | 2020-05-19 | 中国科学院自动化研究所南京人工智能芯片创新研究院 | Intelligent anti-terrorist equipment and system based on face recognition unmanned aerial vehicle equipment |
| CN111169639B (en) * | 2019-12-26 | 2021-07-02 | 中国科学院自动化研究所南京人工智能芯片创新研究院 | Intelligent anti-terrorist equipment and system based on face recognition unmanned aerial vehicle equipment |
| CN112623181A (en) * | 2020-12-16 | 2021-04-09 | 北华航天工业学院 | Shuttle-shaped structure for aircraft |
| CN114104294A (en) * | 2021-11-30 | 2022-03-01 | 杭州科技职业技术学院 | Suspension type unmanned aerial vehicle carries thing device |
| CN114104294B (en) * | 2021-11-30 | 2023-09-19 | 杭州科技职业技术学院 | Suspended unmanned aerial vehicle carrying device |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| WD01 | Invention patent application deemed withdrawn after publication | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20190712 |