CN107651202A - A kind of hooking device and its unmanned plane - Google Patents
A kind of hooking device and its unmanned plane Download PDFInfo
- Publication number
- CN107651202A CN107651202A CN201710954630.6A CN201710954630A CN107651202A CN 107651202 A CN107651202 A CN 107651202A CN 201710954630 A CN201710954630 A CN 201710954630A CN 107651202 A CN107651202 A CN 107651202A
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- hole
- pin
- latch
- connecting rod
- hooking device
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- 230000007246 mechanism Effects 0.000 claims description 42
- 230000005540 biological transmission Effects 0.000 claims description 9
- 238000003780 insertion Methods 0.000 claims description 4
- 230000037431 insertion Effects 0.000 claims description 4
- 230000002093 peripheral effect Effects 0.000 abstract description 9
- 238000010276 construction Methods 0.000 abstract description 3
- 230000000694 effects Effects 0.000 description 3
- 238000005516 engineering process Methods 0.000 description 3
- 238000007599 discharging Methods 0.000 description 2
- 230000005484 gravity Effects 0.000 description 2
- 238000009434 installation Methods 0.000 description 2
- 238000012423 maintenance Methods 0.000 description 2
- 238000013507 mapping Methods 0.000 description 2
- 230000004043 responsiveness Effects 0.000 description 2
- 230000007547 defect Effects 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 230000008450 motivation Effects 0.000 description 1
- 238000013486 operation strategy Methods 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
- 230000000007 visual 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
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Load-Engaging Elements For Cranes (AREA)
- Connection Of Plates (AREA)
Abstract
The invention provides a kind of hooking device and its unmanned plane, hooking device includes hanger body, latch and executing agency；U-shaped groove is provided with the hanger body；The U-shaped groove is provided with the first pin-and-hole and the second pin-and-hole in two side walls；First pin-and-hole and second pin-and-hole are coaxially disposed；The latch is slidably disposed in first pin-and-hole；The present invention is simple in construction, and reliability is higher, can realize that peripheral hardware equipment is mounted and is smoothly detached with the quick of unmanned plane, so as to substantially increase the operating efficiency of hooking device and reliability.
Description
Technical field
The present invention relates to unmanned air vehicle technique field, more particularly, to a kind of hooking device and its unmanned plane.
Background technology
At present, as the operation strategies of the development unmanned plane of science and technology are more and more extensive, power department, public security department, traffic police
Mechanism, the units such as department, land mapping, video display shooting, live news purchase unmanned plane and are used for solving the various of all departments successively
Demand.
Unmanned plane can be completed as carry module of its purposes of carrier depending on unmanned plane, the different module of carry
Different tasks：Carry video camera, which can complete task, the carry infrared cameras such as boat fearness, can complete the tasks such as power-line patrolling, carry
Remote sensing equipment can complete mapping task；If single task role, a frame unmanned plane can is completed, if task is cumbersome to need carry
Disparate modules meet how quickly to change module during different demands just into stubborn problem.Existing unmanned plane carry device
It is not high, it is necessary to user oneself assembling, debugging aircraft to there is integrated level；Hardware interface is single, and versatility is not strong；Structure installation is multiple
Miscellaneous, delivered payload capability is indefinite；The SDK of non expansivity is opened, the defects of no software extensions ability.
And the problem of then performance structure is complex for the hook portion in carry module, reliability, and fault rate is high.
The content of the invention
It is more multiple to solve hook portion structure in the prior art it is an object of the invention to provide a kind of hooking device
Miscellaneous, reliability, the high technical problem of fault rate.
Another object of the present invention is to provide a kind of unmanned plane with above-mentioned hooking device, to solve existing unmanned plane
Hook portion structure is complex, reliability, the high technical problem of fault rate.
In order to solve the above technical problems, a kind of hooking device provided by the invention, including：Hanger body, latch and execution
Mechanism；
U-shaped groove is provided with the hanger body；
The U-shaped groove is provided with the first pin-and-hole and the second pin-and-hole in two side walls；
First pin-and-hole and second pin-and-hole are coaxially disposed；
The latch is slidably disposed in first pin-and-hole；
The executing agency is connected with the end of the latch, for driving the latch front end to stretch out first pin-and-hole
And second pin-and-hole is inserted, or drive the front end of the latch to exit and be retracted into the first pin-and-hole from the second pin-and-hole.
The present invention is simple in construction, and reliability is higher, and during carry, the hook of external device inserts the U-shaped groove, performs machine
Structure drives the latch front end to stretch out first pin-and-hole, and second pin-and-hole, latch are inserted after the through hole middle through hook
Front end be inserted in the second pin-and-hole, the posterior segment of latch is inserted in the first pin-and-hole；Two pin-and-holes have effectively shared peripheral hardware equipment
Load, can not be retracted so as to avoid latch deformation, or influence to be continuing with next time, increase maintenance cost or use
Cost.
Because the probability of latch deformation greatly reduces, when discharging or launching peripheral hardware equipment, described in executing agency's drive
The front end of latch is exited from the second pin-and-hole and is retracted into the first pin-and-hole, link up with the external force such as gravity effect under exit it is U-shaped recessed
Groove, peripheral hardware equipment is smoothly detached with unmanned plane, so as to substantially increase the operating efficiency of hooking device and reliability.
In any of the above-described technical scheme, further, the aperture of first pin-and-hole and the latch external diameter size phase
Symbol, is oriented to when being slided for latch.
In any of the above-described technical scheme, further, first pin-and-hole is consistent with the internal diameter of second pin-and-hole, institute
State the second pin-and-hole and chamfering or rounding for guiding latch insertion are provided with the opening's edge of groove side.
In any of the above-described technical scheme, further, the executing agency includes drive mechanism and transmission mechanism, described
Drive mechanism is connected by transmission mechanism with the latch, for driving the latch to be moved along first pin-and-hole.
In any of the above-described technical scheme, further, the drive mechanism is steering wheel or servomotor.
In any of the above-described technical scheme, further, the transmission mechanism is linkage, and the linkage includes
The first connecting rod and second connecting rod of head and the tail connection successively；
The head end of the first connecting rod is hinged and connected in the hanger body；The end of the first connecting rod and described second
Connecting rod head end is hinged；
The end of second connecting rod and the end of the latch are hinged；
The drive mechanism is connected with the first connecting rod, drives the first connecting rod to be swung around the jointed shaft of its head end,
And then the latch is driven to move back and forth along first pin-and-hole by second connecting rod.
In any of the above-described technical scheme, further, the head end of the first connecting rod is arranged at intervals with several and is used for
Select the connecting hole of the connection second connecting rod.By selecting different connecting holes to be connected with second connecting rod, so as to adjust moment of torsion
And the responsiveness of latch.
In any of the above-described technical scheme, further, the hanger body also include be used for indirectly or directly with nothing
The seat board portion of man-machine connection, several connection through holes are provided with the seat board portion.
In any of the above-described technical scheme, further, the hanger body includes being used to fix the drive mechanism
Fixed mount portion, two fast assembling-disassembling modules are provided with the framework in fixed mount portion；
Two fast assembling-disassembling modules are oppositely arranged on the both sides of the drive mechanism respectively；
The fast assembling-disassembling module includes the contiguous block being fixedly connected in the fixed mount portion, is set on the contiguous block
There is slot；
The housing both sides of the drive mechanism are provided with the plate that cooperation is plugged with the slot.
In any of the above-described technical scheme, further, the contiguous block is removably secured by bolt or screw
In the fixed mount portion, the interlude of the bolt or screw passes through the slot；
It is provided with the plate and mutually interts the U-shaped opening groove coordinated with the interlude.
In any of the above-described technical scheme, further, the interlude is cone type, the two of the U-shaped opening groove
Individual side is the inclined working closed with the frustum type interlude wedge inserting.
When the contiguous block is assembled in fixed mount portion by bolt or screw, the interlude deepens continuously simultaneously
Agree with U-shaped opening groove side, both are simultaneously fixed by frictional fit drive mechanism.During dismounting, screw or bolt are screwed out, is driven
Motivation structure also separates with the contiguous block simultaneously, so as to realize fast assembling-disassembling.
The invention also discloses the unmanned plane with above-mentioned hooking device, the hooking device is directly installed on unmanned plane
Bottom, or on the carry platform of uav bottom.
Using above-mentioned technical proposal, the present invention has the advantages that：
Carry apparatus structure provided by the invention is simple, and reliability is higher, and it is quick with unmanned plane to realize that peripheral hardware is equipped
Mount and be smoothly detached, so as to substantially increase the operating efficiency of hooking device and reliability.
Brief description of the drawings
Below will be to specific in order to illustrate more clearly of the specific embodiment of the invention or technical scheme of the prior art
The required accompanying drawing used is briefly described in embodiment or description of the prior art, it should be apparent that, in describing below
Accompanying drawing is some embodiments of the present invention, for those of ordinary skill in the art, before creative work is not paid
Put, other accompanying drawings can also be obtained according to these accompanying drawings.
Fig. 1 is the stereogram of hooking device provided in an embodiment of the present invention；
Fig. 2 is the stereogram of hanger body in the embodiment of the present invention；
Fig. 3 is the stereogram at another visual angle of hanger body in the embodiment of the present invention；
Fig. 4 is the stereogram of drive mechanism in the embodiment of the present invention.
Reference：
100- hanger bodies；110-U type grooves；The pin-and-holes of 111- first；The pin-and-holes of 112- second；120- seat boards portion；130- consolidates
Determine frame portion；200- executing agencies；210- drive mechanisms；211- is plugged；212-U type open slots；220- transmission mechanisms；221- first
Connecting rod；222- connecting holes；223- second connecting rods；300- latches；500- contiguous blocks；510- slots；520- screws.
Embodiment
Technical scheme is clearly and completely described below in conjunction with accompanying drawing, it is clear that described implementation
Example is part of the embodiment of the present invention, rather than whole embodiments.Based on the embodiment in the present invention, ordinary skill
The every other embodiment that personnel are obtained under the premise of creative work is not made, belongs to the scope of protection of the invention.
In the description of the invention, it is necessary to explanation, term " " center ", " on ", " under ", "left", "right", " vertical ",
The orientation or position relationship of the instruction such as " level ", " interior ", " outer " be based on orientation shown in the drawings or position relationship, merely to
Be easy to the description present invention and simplify description, rather than instruction or imply signified device or element must have specific orientation,
With specific azimuth configuration and operation, therefore it is not considered as limiting the invention.In addition, term " first ", " second ",
" the 3rd " is only used for describing purpose, and it is not intended that instruction or hint relative importance.
In the description of the invention, it is necessary to illustrate, unless otherwise clearly defined and limited, term " installation ", " phase
Even ", " connection " should be interpreted broadly, for example, it may be being fixedly connected or being detachably connected, or be integrally connected；Can
To be mechanical connection or electrical connection；Can be joined directly together, can also be indirectly connected by intermediary, Ke Yishi
The connection of two element internals.For the ordinary skill in the art, with concrete condition above-mentioned term can be understood at this
Concrete meaning in invention.
With reference to specific embodiment the present invention will be further explained explanation.
As shown in Figure 1-2, a kind of hooking device that the present embodiment provides, including：Hanger body 100, latch 300 and execution
Mechanism 200；
U-shaped groove 110 is provided with the hanger body 100；
Opening of the U-shaped groove 110 respectively in U-shaped groove 110 in two side walls is provided with the He of the first pin-and-hole 111
Second pin-and-hole 112；
First pin-and-hole 111 and second pin-and-hole 112 are coaxially disposed；
The latch 300 is slidably disposed in first pin-and-hole 111；
The executing agency 200 is connected with the end of the latch, for driving the front end of latch 300 to stretch out described the
One pin-and-hole 111 simultaneously inserts second pin-and-hole 112, or drives the front end of the latch 300 to be exited simultaneously from the second pin-and-hole 112
It is retracted into the first pin-and-hole 111.
The present invention is simple in construction, and reliability is higher, and during carry, the hook of external device inserts the U-shaped groove 110, holds
Row mechanism 200 drives the front end of latch 300 to stretch out first pin-and-hole 111, after the through hole middle through hook described in insertion
Second pin-and-hole 112, the front end of latch 300 are inserted in the second pin-and-hole 112, and the posterior segment of latch 300 is inserted in the first pin-and-hole 111
It is interior；Two pin-and-holes have effectively shared the load of peripheral hardware equipment, deform and can not retract so as to avoid latch 300, or influence
Next time is continuing with, and increases maintenance cost or use cost.
Because the probability that latch 300 deforms greatly reduces, when discharging or launching peripheral hardware equipment, the band of executing agency 200
The front end for moving the latch 300 is exited from the second pin-and-hole 112 and is retracted into the first pin-and-hole 111, links up with external force such as gravity
U-shaped groove 110 is exited under effect, peripheral hardware equipment is smoothly detached with unmanned plane, so as to substantially increase the work of hooking device effect
Rate and reliability.
Further, the aperture of first pin-and-hole 111 is consistent with the external diameter size of latch 300, is slided for latch 300
It is oriented to when dynamic.
Further, first pin-and-hole 111 is consistent with the internal diameter of second pin-and-hole 112, and second pin-and-hole 112 exists
The chamfering or rounding for guiding the insertion of latch 300 are provided with the opening's edge of groove side.
Further, the executing agency 200 includes drive mechanism 210 and transmission mechanism 220, the drive mechanism 210
It is connected by transmission mechanism 220 with the latch 300, for driving the latch 300 to be moved along first pin-and-hole 111.
Further, the drive mechanism 210 is steering wheel or servomotor.
Further, as shown in figure 3, the transmission mechanism 220 is linkage, the linkage includes head and the tail successively
The first connecting rod 221 and second connecting rod 223 of connection；
The end of the first connecting rod 221 is hinged with the head end of second connecting rod 223；
The end of second connecting rod 223 and the end of the latch 300 are hinged；
The drive mechanism 210 is connected with the head end of the first connecting rod 221, passes sequentially through the He of first connecting rod 221
Second connecting rod 223 drives the latch 300 to move back and forth along first pin-and-hole 111.
The head end of first connecting rod 221 is arranged at intervals with several connecting holes 222 for being used to select a connection second connecting rod 223.
By selecting different connecting holes 222 to be connected with second connecting rod 223, so as to adjust the responsiveness of moment of torsion and latch 300.
Further, the hanger body 100 also includes being used for the seat board portion being directly connected indirectly or with unmanned plane
120, several connection through holes are provided with the seat board portion 120.
Further, as shown in figure 3, the hanger body 100 includes being used for the fixed mount for fixing the drive mechanism 210
Portion 130, two fast assembling-disassembling modules are provided with the framework in fixed mount portion 130；
Two fast assembling-disassembling modules are oppositely arranged on the both sides of the drive mechanism 210 respectively；
The fast assembling-disassembling module includes the contiguous block 500 being fixedly connected in the fixed mount portion 130, the contiguous block
500 are provided with slot 510 in the side of drive mechanism 210；
As shown in figure 4, the housing both sides of the drive mechanism 210 are provided with plugs inserting for cooperation with the slot 510
Plate 211.
Further, the contiguous block 500 is removably attached in the fixed mount portion 130 by screw 520, described
The interlude of screw 520 passes through the slot 510；
It is provided with the plate 211 and mutually interts the U-shaped opening groove 212 coordinated with the interlude.
Preferably, the interlude is cone type, and two sides of the U-shaped opening groove 212 are and the frustum type
The inclined working that the inserting of interlude wedge is closed.
When the contiguous block 500 is assembled in fixed mount portion 130 by screw 520, the interlude deepens continuously
And agree with the side of U-shaped opening groove 212, both are simultaneously fixed by frictional fit drive mechanism 210.During dismounting, screw is screwed out
520 or bolt, drive mechanism 210 also separates with the contiguous block 500 simultaneously, so as to realize fast assembling-disassembling.
The invention also discloses the unmanned plane with above-mentioned hooking device, the hooking device is directly installed on unmanned plane
Bottom, or on the carry platform of uav bottom.
Carry apparatus structure provided by the invention is simple, and reliability is higher, and it is quick with unmanned plane to realize that peripheral hardware is equipped
Mount and be smoothly detached, so as to substantially increase the operating efficiency of hooking device and reliability.
Finally it should be noted that：Various embodiments above is merely illustrative of the technical solution of the present invention, rather than its limitations；To the greatest extent
The present invention is described in detail with reference to foregoing embodiments for pipe, it will be understood by those within the art that：Its according to
The technical scheme described in foregoing embodiments can so be modified, either which part or all technical characteristic are entered
Row equivalent substitution；And these modifications or replacement, the essence of appropriate technical solution is departed from various embodiments of the present invention technology
The scope of scheme.
Claims (10)
- A kind of 1. hooking device, it is characterised in that including：Hanger body, latch and executing agency；U-shaped groove is provided with the hanger body；The U-shaped groove is provided with the first pin-and-hole and the second pin-and-hole in two side walls；First pin-and-hole and second pin-and-hole are coaxially disposed；The latch is slidably disposed in first pin-and-hole；The executing agency is connected with the end of the latch, for driving the latch front end to stretch out first pin-and-hole and inserting Enter second pin-and-hole, or drive the front end of the latch to exit and be retracted into the first pin-and-hole from the second pin-and-hole.
- 2. hooking device according to claim 1, it is characterised in that the aperture of first pin-and-hole and the latch external diameter Size is consistent, and is oriented to when being slided for latch；First pin-and-hole is consistent with the internal diameter of second pin-and-hole, and second pin-and-hole is provided with the opening's edge of groove side For guiding the chamfering or rounding of the latch insertion.
- 3. hooking device according to claim 1, it is characterised in that the executing agency includes drive mechanism and driver Structure, the drive mechanism are connected by transmission mechanism with the latch, for driving the latch to be moved along first pin-and-hole.
- 4. hooking device according to claim 1, it is characterised in that the drive mechanism is steering wheel or servomotor.
- 5. hooking device according to claim 3, it is characterised in that the transmission mechanism is linkage, the connecting rod Mechanism includes the first connecting rod and second connecting rod of head and the tail connection successively；The head end of the first connecting rod is connected with the drive mechanism；The end of the first connecting rod and the second connecting rod head end It is hinged；The end of second connecting rod and the end of the latch are hinged；The drive mechanism pass sequentially through the first connecting rod and second connecting rod drive the latch along first pin-and-hole back and forth It is mobile.
- 6. hooking device according to claim 5, it is characterised in that the head end of the first connecting rod is arranged at intervals with some The individual connecting hole for being used to select the connection second connecting rod.
- 7. hooking device according to claim 1, it is characterised in that the hanger body is also included for indirectly or straight The seat board portion being connected with unmanned plane is met, several connection through holes are provided with the seat board portion.
- 8. hooking device according to claim 3, it is characterised in that the hanger body includes being used to fix the driving The fixed mount portion of mechanism, two fast assembling-disassembling modules are provided with the framework in fixed mount portion；Two fast assembling-disassembling modules are oppositely arranged on the both sides of the drive mechanism respectively；The fast assembling-disassembling module includes the contiguous block being fixedly connected in the fixed mount portion, is provided with the contiguous block slotting Groove；The housing both sides of the drive mechanism are provided with the plate that cooperation is plugged with the slot.
- 9. hooking device according to claim 8, it is characterised in that the contiguous block is detachable by bolt or screw Ground is fixed in the fixed mount portion, and the interlude of the bolt or screw passes through the slot；It is provided with the plate and mutually interts the U-shaped opening groove coordinated with the interlude.
- 10. the unmanned plane with the hooking device described in claim any one of 1-9, it is characterised in that the hooking device is straight Connect installed in the bottom of unmanned plane, or on the carry platform of uav bottom.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710954630.6A CN107651202B (en) | 2017-10-13 | 2017-10-13 | A kind of hooking device and its unmanned plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710954630.6A CN107651202B (en) | 2017-10-13 | 2017-10-13 | A kind of hooking device and its unmanned plane |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN107651202A true CN107651202A (en) | 2018-02-02 |
| CN107651202B CN107651202B (en) | 2019-11-29 |
Family
ID=61118660
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201710954630.6A Active CN107651202B (en) | 2017-10-13 | 2017-10-13 | A kind of hooking device and its unmanned plane |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN107651202B (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108820216A (en) * | 2018-06-14 | 2018-11-16 | 天津航天中为数据系统科技有限公司 | One kind having the double detachers of self-locking function |
| CN112238942A (en) * | 2019-07-16 | 2021-01-19 | 北京京东尚科信息技术有限公司 | Automatic cargo throwing mechanism and unmanned aerial vehicle |
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| CN204713431U (en) * | 2015-04-24 | 2015-10-21 | 深圳一电科技有限公司 | Carry device and unmanned plane |
| CN106043699A (en) * | 2016-07-13 | 2016-10-26 | 绵阳空天科技有限公司 | Dropping device of unmanned aerial vehicle |
| CN205738124U (en) * | 2016-05-12 | 2016-11-30 | 普宙飞行器科技（深圳）有限公司 | One is conveniently replaceable load device and unmanned plane |
| CN206012972U (en) * | 2016-07-25 | 2017-03-15 | 乐视控股（北京）有限公司 | A kind of general hanging piece base of unmanned plane |
| CN106882378A (en) * | 2017-03-31 | 2017-06-23 | 国网上海市电力公司 | A kind of automatically-unhooked Throwing device of unmanned plane |
| CN207258003U (en) * | 2017-10-13 | 2018-04-20 | 北京臻迪科技股份有限公司 | A kind of hooking device and its unmanned plane |
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| CN204713431U (en) * | 2015-04-24 | 2015-10-21 | 深圳一电科技有限公司 | Carry device and unmanned plane |
| CN205738124U (en) * | 2016-05-12 | 2016-11-30 | 普宙飞行器科技（深圳）有限公司 | One is conveniently replaceable load device and unmanned plane |
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| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108820216A (en) * | 2018-06-14 | 2018-11-16 | 天津航天中为数据系统科技有限公司 | One kind having the double detachers of self-locking function |
| CN108820216B (en) * | 2018-06-14 | 2023-12-22 | 天津航天中为数据系统科技有限公司 | Double unhooking device with self-locking function |
| CN112238942A (en) * | 2019-07-16 | 2021-01-19 | 北京京东尚科信息技术有限公司 | Automatic cargo throwing mechanism and unmanned aerial vehicle |
| CN112238942B (en) * | 2019-07-16 | 2024-04-16 | 北京京东乾石科技有限公司 | Automatic cargo throwing mechanism and unmanned aerial vehicle |
Also Published As
| Publication number | Publication date |
|---|---|
| CN107651202B (en) | 2019-11-29 |
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