CN208868306U - A kind of unmanned plane fast insert-pull carry platform - Google Patents
A kind of unmanned plane fast insert-pull carry platform Download PDFInfo
- Publication number
- CN208868306U CN208868306U CN201821550874.4U CN201821550874U CN208868306U CN 208868306 U CN208868306 U CN 208868306U CN 201821550874 U CN201821550874 U CN 201821550874U CN 208868306 U CN208868306 U CN 208868306U
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- trapezoidal
- carry
- supporting plate
- battery supporting
- unmanned plane
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- NJPPVKZQTLUDBO-UHFFFAOYSA-N novaluron Chemical compound C1=C(Cl)C(OC(F)(F)C(OC(F)(F)F)F)=CC=C1NC(=O)NC(=O)C1=C(F)C=CC=C1F NJPPVKZQTLUDBO-UHFFFAOYSA-N 0.000 claims abstract description 32
- 238000012545 processing Methods 0.000 claims description 6
- 230000001105 regulatory effect Effects 0.000 claims 1
- 238000010586 diagram Methods 0.000 description 4
- 238000009434 installation Methods 0.000 description 3
- 238000011161 development Methods 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 238000004891 communication Methods 0.000 description 1
- 238000013461 design Methods 0.000 description 1
- 239000002360 explosive Substances 0.000 description 1
- 238000003780 insertion Methods 0.000 description 1
- 230000037431 insertion Effects 0.000 description 1
- 238000007689 inspection Methods 0.000 description 1
- 238000011835 investigation Methods 0.000 description 1
- 238000013507 mapping Methods 0.000 description 1
- 230000013011 mating Effects 0.000 description 1
- 238000012544 monitoring process Methods 0.000 description 1
- 239000000178 monomer Substances 0.000 description 1
- 230000004083 survival effect 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
- B64D47/00—Equipment not otherwise provided for
-
- 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
-
- 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
- B64U2101/30—UAVs specially adapted for particular uses or applications for imaging, photography or videography
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Battery Mounting, Suspending (AREA)
Abstract
A kind of unmanned plane fast insert-pull carry platform including battery supporting plate, the carry pedestal being hinged below battery supporting plate, is symmetrically hinged on the clamping mechanism of battery supporting plate two sides, the angle adjustment arm for being symmetrically connected to battery supporting plate two sides, the trapezoidal grafting block being connected to below carry pedestal, the spring retaining mechanism that trapezoidal grafting block front end is arranged in and the matching used trapezoidal plug socket of trapezoidal grafting block；Wherein, the angle adjustment arm and battery supporting plate are connected, and angle adjustment arm is arc-shaped flaky structure, and an arc adjustment hole is provided in angle adjustment arm；An adjusting locking bolt is provided in the arc adjustment hole；Described one end for adjusting locking bolt is threadedly coupled with the threaded hole on carry pedestal；The trapezoidal plug socket is inserted on trapezoidal grafting block, is connected and fixed trapezoidal grafting block with trapezoidal plug socket by spring retaining mechanism, carry device is equipped with below trapezoidal plug socket.The carry platform can realize the quick-replaceable to carry device, versatile.
Description
Technical field
The utility model relates to unmanned plane carry technical field, specifically a kind of unmanned plane fast insert-pull carry is flat
Platform.
Background technique
UAV referred to as " unmanned plane ", is manipulated using radio robot and the presetting apparatus provided for oneself
Not manned vehicle, unmanned plane is actually the general designation of unmanned vehicle.Compared with manned aircraft, it has volume
Small, low cost, it is easy to use, to operational environment require it is low, battlefield survival is stronger the advantages that.Due to UAV pair
Future Air Combat has great significance, and each main military country, the world is all in the development work for stepping up progress UAV.
With the fast development of unmanned air vehicle technique, as a kind of mobility strong, small scale robot tool easy to operate,
The fields such as military, civilian have this to be widely applied, at present investigation, it is explosive, in terms of extensive application.
Classification by use, unmanned plane can be divided into military unmanned air vehicle and civilian unmanned plane.Military unmanned air vehicle, which can be divided into, to be detectd
Examine unmanned plane, bait unmanned plane, UAV for electronic countermeasure, communication relay unmanned plane, unmanned fighter and target drone
Deng；Civilian unmanned plane can be divided into inspection/monitoring unmanned plane, agricultural unmanned plane, meteorological unmanned plane, exploration unmanned plane and mapping nothing
It is man-machine etc..
Unmanned plane depends on the carry platform of unmanned plane as its purposes of carrier, and the different module of carry can be completed
Different tasks, carry video camera is achievable the tasks such as to take photo by plane, the tasks such as achievable power-line patrolling of carry infrared camera, carry
Military equipment can complete the aerial precisely combat duties such as strike, currently, unmanned plane carry platform majority is that monomer is fixed, peace
Dress is inconvenient, can not be general, is not able to satisfy a variety of carry devices and is switched fast use.
Summary of the invention
The purpose of this utility model is to provide a kind of unmanned plane fast insert-pull carry platforms, which can not only be right
Carry design factors are adjusted, additionally it is possible to meet a variety of unmanned plane carry devices and be switched fast use, realize each device flat
General on platform, Fast Installation is switched fast.
To achieve the above object, the utility model adopts the following technical scheme that realization:
A kind of unmanned plane fast insert-pull carry platform, including battery supporting plate, the carry pedestal being hinged below battery supporting plate,
Symmetrically it is hinged on the clamping mechanism of battery supporting plate two sides, the angle adjustment arm for being symmetrically connected to battery supporting plate two sides, is connected to extension
Carry the trapezoidal grafting block below pedestal, spring retaining mechanism that trapezoidal grafting block front end is set, with trapezoidal grafting block is mating makes
Trapezoidal plug socket；Wherein, the battery supporting plate, for placing unmanned plane battery, four foot props of unmanned plane are fixed on
On clamping mechanism；The angle adjustment arm and battery supporting plate are connected, and angle adjustment arm is arc-shaped flaky structure, in angle adjustment arm
On be provided with an arc adjustment hole；An adjusting locking bolt is provided in the arc adjustment hole；The adjusting locking bolt
One end be threadedly coupled with the threaded hole on carry pedestal；The trapezoidal plug socket is inserted on trapezoidal grafting block, passes through springlock
Trapezoidal grafting block is connected and fixed by tight mechanism with trapezoidal plug socket, and carry device is equipped with below trapezoidal plug socket.
As the preferred of the utility model, the side that the battery supporting plate is connect with carry pedestal is symmetrically connected, and there are two connect
Spindle seat, the first articulated shaft passes through two connection shaft seats and carry pedestal, and battery supporting plate and carry pedestal is hinged；The battery
The two sides of supporting plate also band is machined with hinge hole there are two engaging lug on the engaging lug, the second articulated shaft passes through hinge hole and card
Connection mechanism, clamping mechanism is hinged with battery supporting plate.
As the preferred of the utility model, the clamping mechanism includes the fixing card hinged with battery supporting plate and passes through fast-assembling
The active card that bolt is connect with fixing card；The fixing card forms two blocked holes after connecting with active card.
As the preferred of the utility model, the trapezoidal grafting block is connected to below carry pedestal by multiple screws,
The front end of trapezoidal grafting block is machined with one first protrusion；One is machined in first protrusion for installing spring locking machine
The mounting hole of structure；Two sides of trapezoidal grafting block are the inclined surface being symmetrically inclined outwardly；It is machined on the trapezoidal plug socket
The connecting hole of multiple connection carry objects, is machined with the trapezoidal grafting of one with trapezoidal grafting Block- matching on trapezoidal plug socket
Slot；The front end of the trapezoidal plug socket is machined with one second protrusion；A locking slot is machined in second protrusion；It is described
Locking slot is corresponding with mounting hole.
As the preferred of the utility model, below the carry pedestal, one is fixed with behind trapezoidal grafting block
Block；The block is for the limit after trapezoidal plug socket is inserted into trapezoidal grafting block.
As the further preferred of the utility model, it is additionally provided with limited block on two engaging lugs of the battery supporting plate,
The limited block is mounted on the second articulated shaft, and limited block is L-type structure, for limiting the upper gyration of clamping mechanism.
As the further preferred of the utility model, there are two lightening hole, the carry bases for processing on the battery supporting plate
Processing is machined with lightening hole in the fixing card and active card there are two lightening hole respectively on seat.
As the further preferred of the utility model, inserted below the spring retaining mechanism with spring locking
Head, the upper surface of described spring locking plug have a pull ring, and spring locking plug retracts when the pull ring pull-up, and pull ring is put down
When spring locking plug stretch out, the locking slot being caught on trapezoidal plug socket.
The utility model has the advantages that:
1, carry platform structure provided by the utility model is simple, easy to use, by clamping mechanism by platform and nobody
Under-chassis frame is fixed, and is installed fixed；In addition, by by trapezoidal plug socket quick insertion or extract trapezoidal grafting block, it can be achieved that
To the quick-replaceable of carry device, a variety of carry devices can be met and be switched fast use, the carry platform compatibility is strong,
It is applied widely.
2, the platform that a variety of carry systems may be implemented in carry platform provided by the utility model shares, Fast Installation, fastly
Speed switching；In addition, can adjust the tilt angle of carry device by angular adjustment fixing bolt, meet the need under a variety of environment
It asks.
3, multiple lightening holes are machined on carry platform provided by the utility model, carry platform overall weight is lighter, makes
Unmanned plane can the bigger carry device of load capacity take off.
Detailed description of the invention
Fig. 1 is one of the utility model overall structure diagram.
Fig. 2 is the exploded view of the utility model Fig. 1.
Fig. 3 is the two of the utility model overall structure diagram.
Fig. 4 is one of the utility model battery supporting plate and carry pedestal connection schematic diagram.
Fig. 5 is the two of the utility model battery supporting plate and carry pedestal connection schematic diagram.
Specific embodiment
To enable those skilled in the art to better understand the technical solution of the utility model and its advantage, below with reference to
The application is described in detail in attached drawing, but is not used to limit the protection scope of the utility model.
As shown in attached drawing 1,2: unmanned plane fast insert-pull carry platform provided by the utility model includes: battery supporting plate 1, leads to
It crosses carry pedestal 3 that the first articulated shaft 2 is hinged below battery supporting plate 1, battery supporting plate is symmetrically hinged on by the second articulated shaft 4
The clamping mechanism 5 of 1 two sides, the angle adjustment arm 6 for being symmetrically connected to 1 two sides of battery supporting plate, the ladder being connected to below carry pedestal 3
Shape grafting block 7, the spring retaining mechanism 8 that trapezoidal 7 front end of grafting block is set and the matching used trapezoidal grafting of trapezoidal grafting block
Seat 9；Wherein, the battery supporting plate 1, for placing unmanned plane battery, four foot props of unmanned plane are fixed on clamping mechanism 5
On；The angle adjustment arm 6 is connected by fixing bolt 6-2 and battery supporting plate 1, and angle adjustment arm 6 is arc-shaped flaky structure,
An arc adjustment hole 6-1 is provided in angle adjustment arm 6；6-1 is provided with an adjusting locking bolt in the arc adjustment hole
6-3；Described one end for adjusting locking bolt 6-3 is threadedly coupled with the threaded hole 3-2 on carry pedestal 3；The trapezoidal plug socket 9
It is inserted on trapezoidal grafting block 7, is connected and fixed trapezoidal grafting block 7 and trapezoidal plug socket 9 by spring retaining mechanism 8, trapezoidal
Carry device is installed below plug socket 9；
There are two lightening hole 1-1, the side that battery supporting plate 1 is connect with carry pedestal 3 is symmetrical for processing on the battery supporting plate 1
Being connected, there are two connection shaft seat 1-2；First articulated shaft 2 passes through two connection shaft seat 1-2 and carry pedestal 3, by battery tray
Plate 1 and carry pedestal 3 are hinged；It is processed on the two sides of the battery supporting plate 1 engaging lug 1-3 also with there are two, the engaging lug 1-3
There is hinge hole 1-4, second articulated shaft 4 passes through hinge hole 1-4 and clamping mechanism 5, clamping mechanism 5 and battery supporting plate 1 are cut with scissors
It connects；Limited block 1-5 is additionally provided on two engaging lug 1-3 of the battery supporting plate 1, the limited block 1-5 is mounted on second
On articulated shaft 4, limited block 1-5 is L-type structure, for limiting the upper gyration of clamping mechanism 5；
There are two lightening hole 3-1 for processing on the carry pedestal 3, are machined with spiral shell respectively in two sides of carry pedestal 3
Pit 3-2, the one end for adjusting locking bolt 6-3 are threadedly coupled with the threaded hole 3-2 on carry pedestal 3；
The clamping mechanism 5 includes the fixing card 5-1 hinged with battery supporting plate 1 and passes through fast-assembling bolt 5-2 and fixing card
The active card 5-3 of 5-1 connection；The fixing card 5-1 forms two blocked hole 5-4 after connecting with active card 5-3；The fixing card
It is machined with lightening hole 5-5 respectively on 5-1 and active card 5-3；
The trapezoidal grafting block 7 is connected to below carry pedestal 3 by multiple screws, and the front end of trapezoidal grafting block 7 adds
Work has one first protrusion 7-1；One is machined on the first protrusion 7-1 for installing the mounting hole of spring retaining mechanism 8
7-2；Two sides of trapezoidal grafting block 7 are the inclined surface 7-3 being symmetrically inclined outwardly；
It is machined with the connecting hole 9-1 of multiple connection carry objects on the trapezoidal plug socket 9, adds on trapezoidal plug socket 9
Work has one and the matched trapezoidal inserting groove 9-2 of trapezoidal grafting block 7；The front end of the trapezoidal plug socket 9 is machined with one second
Raised 9-3；A locking slot 9-4 is machined on the second protrusion 9-3；The locking slot 9-4 is corresponding with mounting hole 7-2；
Spring locking plug 8-1, the upper surface of described spring locking plug 8-1 are had below the spring retaining mechanism 8
With a pull ring 8-2, spring locking plug 8-1 is retracted when the pull ring 8-2 pull-up, and spring locking is inserted when pull ring 8-2 is put down
Head 8-1 stretches out, the locking slot 9-4 being caught on trapezoidal plug socket 9；
Below the carry pedestal 3, a block 10 is fixed with behind trapezoidal grafting block 7；The block 10 is used
In the limit after trapezoidal plug socket 9 is inserted into trapezoidal grafting block 7.
The course of work: when installation, first unloading fast-assembling bolt 5-2, by four leg supports of unmanned plane be fixed on fixing card 5-1 with
In the blocked hole 5-4 of active card 5-3, then fast-assembling bolt 5-2 is tightened, carry platform is connect with unmanned plane；
Battery used in unmanned plane is placed on battery supporting plate 1 again, trapezoidal plug socket 9 is connect admittedly with carry device
It is fixed, then trapezoidal plug socket 9 is inserted on trapezoidal grafting block 7 together with carry device, it will be trapezoidal by spring retaining mechanism 8
Plug socket 9 is connected and fixed with trapezoidal grafting block 7；
The angle for adjusting carry device by adjusting locking bolt 6-3 later will adjust locking bolt 6-3 after determining angle
It tightens, unmanned plane drives carry platform and carry device to take off；When needing replacing carry device, it is only necessary to pull up pull ring 8-
2, trapezoidal plug socket 9 is unloaded, another carry device for having trapezoidal plug socket 9 is then changed, it is easy to operate, it is convenient,
It is time saving and energy saving.
Claims (8)
1. a kind of unmanned plane fast insert-pull carry platform, it is characterised in that: including battery supporting plate, be hinged below battery supporting plate
Carry pedestal, symmetrically be hinged on the clamping mechanism of battery supporting plate two sides, the angle adjustment arm for being symmetrically connected to battery supporting plate two sides,
The trapezoidal grafting block that is connected to below carry pedestal, the spring retaining mechanism that trapezoidal grafting block front end is set, with trapezoidal grafting
The matching used trapezoidal plug socket of block；Wherein, the battery supporting plate, for placing unmanned plane battery, four feet of unmanned plane
Frame is fixed on clamping mechanism；The angle adjustment arm and battery supporting plate are connected, and angle adjustment arm is arc-shaped flaky structure, at angle
An arc adjustment hole is provided on degree regulating arm；An adjusting locking bolt is provided in the arc adjustment hole；The adjusting
One end of locking bolt is threadedly coupled with the threaded hole on carry pedestal；The trapezoidal plug socket is inserted on trapezoidal grafting block, is led to
It crosses spring retaining mechanism and is connected and fixed trapezoidal grafting block with trapezoidal plug socket, carry dress is installed below trapezoidal plug socket
It sets.
2. a kind of unmanned plane fast insert-pull carry platform according to claim 1, it is characterised in that: the battery supporting plate with
The side of carry pedestal connection is symmetrically connected there are two connection shaft seat, and the first articulated shaft passes through two connection shaft seats and carry base
Seat, battery supporting plate and carry pedestal is hinged；The two sides of the battery supporting plate also band there are two engaging lug, on the engaging lug plus
Work has hinge hole, and the second articulated shaft passes through hinge hole and clamping mechanism, and clamping mechanism is hinged with battery supporting plate.
3. a kind of unmanned plane fast insert-pull carry platform according to claim 1, it is characterised in that: the clamping mechanism packet
The active card for including the fixing card hinged with battery supporting plate and being connect by fast-assembling bolt with fixing card；The fixing card and active card
Two blocked holes are formed after connection.
4. a kind of unmanned plane fast insert-pull carry platform according to claim 1, it is characterised in that: the trapezoidal grafting block
It is connected to below carry pedestal by multiple screws, the front end of trapezoidal grafting block is machined with one first protrusion；Described first
One is machined in protrusion for installing the mounting hole of spring retaining mechanism；Two sides of trapezoidal grafting block are symmetrically to lean outward
Oblique inclined surface；It is machined with the connecting hole of multiple connection carry objects on the trapezoidal plug socket, is processed on trapezoidal plug socket
There are the trapezoidal inserting groove of one with trapezoidal grafting Block- matching；The front end of the trapezoidal plug socket is machined with one second protrusion；Institute
It states and is machined with a locking slot in the second protrusion；The locking slot is corresponding with mounting hole.
5. a kind of unmanned plane fast insert-pull carry platform according to claim 1, it is characterised in that: in the carry pedestal
Below, a block is fixed with behind trapezoidal grafting block；The block is used to be inserted into trapezoidal grafting block in trapezoidal plug socket
Limit afterwards.
6. a kind of unmanned plane fast insert-pull carry platform according to claim 2, it is characterised in that: the battery supporting plate
Limited block is additionally provided on two engaging lugs, the limited block is mounted on the second articulated shaft, and limited block is L-type structure, is used for
Limit the upper gyration of clamping mechanism.
7. a kind of unmanned plane fast insert-pull carry platform according to claim 3, it is characterised in that: on the battery supporting plate
Processing is there are two lightening hole, and processing is processed in the fixing card and active card respectively there are two lightening hole on the carry pedestal
There is lightening hole.
8. a kind of unmanned plane fast insert-pull carry platform according to claim 4, it is characterised in that: the spring locks machine
Spring locking plug is had below structure, the upper surface of described spring locking plug has a pull ring, bullet when the pull ring pull-up
Spring locking plug retracts, and spring locking plug is stretched out when pull ring is put down, the locking slot being caught on trapezoidal plug socket.
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811067696 | 2018-09-13 | ||
| CN2018110676964 | 2018-09-13 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN208868306U true CN208868306U (en) | 2019-05-17 |
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ID=64823344
Family Applications (2)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201821550874.4U Active CN208868306U (en) | 2018-09-13 | 2018-09-21 | A kind of unmanned plane fast insert-pull carry platform |
| CN201811108401.3A Active CN109131916B (en) | 2018-09-13 | 2018-09-21 | Quick plug mounting platform of unmanned aerial vehicle |
Family Applications After (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201811108401.3A Active CN109131916B (en) | 2018-09-13 | 2018-09-21 | Quick plug mounting platform of unmanned aerial vehicle |
Country Status (1)
| Country | Link |
|---|---|
| CN (2) | CN208868306U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109131916A (en) * | 2018-09-13 | 2019-01-04 | 吉林省翼启飞科技有限公司 | A kind of unmanned plane fast insert-pull carry platform |
Families Citing this family (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111114786B (en) * | 2020-01-14 | 2021-08-31 | 吉林省翼启飞科技有限公司 | Grenade and grenade throwing device |
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| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104512556A (en) * | 2013-09-30 | 2015-04-15 | 哈尔滨飞机工业集团有限责任公司 | Four-link opening mechanism of radar cover of airplane |
| CN105270644B (en) * | 2015-11-16 | 2017-09-01 | 湖南云顶智能科技有限公司 | Carry platform for unmanned plane |
| CN205971878U (en) * | 2016-08-19 | 2017-02-22 | 深圳市鼎点航模有限公司 | Carry platform and unmanned aerial vehicle |
| CN206466184U (en) * | 2016-11-23 | 2017-09-05 | 丘之鹏 | Camera carry device for unmanned plane oblique photograph system |
| CN207029569U (en) * | 2017-07-11 | 2018-02-23 | 广东容祺智能科技有限公司 | A kind of unmanned plane load Quick Release interface arrangement |
| CN207389575U (en) * | 2017-10-27 | 2018-05-22 | 成都睿翼无人机科技有限公司 | A kind of oblique photograph holder |
| CN108248872A (en) * | 2017-12-29 | 2018-07-06 | 广州供电局有限公司 | Unmanned plane and its battery carry system installation method |
| CN108423188B (en) * | 2018-05-15 | 2024-05-17 | 南京理工大学 | Unmanned aerial vehicle cloud deck mechanism for mounting firearms |
| CN208868306U (en) * | 2018-09-13 | 2019-05-17 | 吉林省翼启飞科技有限公司 | A kind of unmanned plane fast insert-pull carry platform |
-
2018
- 2018-09-21 CN CN201821550874.4U patent/CN208868306U/en active Active
- 2018-09-21 CN CN201811108401.3A patent/CN109131916B/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109131916A (en) * | 2018-09-13 | 2019-01-04 | 吉林省翼启飞科技有限公司 | A kind of unmanned plane fast insert-pull carry platform |
| CN109131916B (en) * | 2018-09-13 | 2024-05-10 | 吉林省翼启飞科技有限公司 | Quick plug mounting platform of unmanned aerial vehicle |
Also Published As
| Publication number | Publication date |
|---|---|
| CN109131916B (en) | 2024-05-10 |
| CN109131916A (en) | 2019-01-04 |
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