CN107757933A - A kind of unmanned plane carry device - Google Patents
A kind of unmanned plane carry device Download PDFInfo
- Publication number
- CN107757933A CN107757933A CN201710954605.8A CN201710954605A CN107757933A CN 107757933 A CN107757933 A CN 107757933A CN 201710954605 A CN201710954605 A CN 201710954605A CN 107757933 A CN107757933 A CN 107757933A
- Authority
- CN
- China
- Prior art keywords
- carry
- unmanned plane
- hole
- general
- pin
- 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.)
- Granted
Links
- 230000007246 mechanism Effects 0.000 claims description 32
- 230000005540 biological transmission Effects 0.000 claims description 10
- 238000010276 construction Methods 0.000 abstract description 7
- 239000000725 suspension Substances 0.000 abstract description 5
- 238000009434 installation Methods 0.000 description 6
- 230000002093 peripheral effect Effects 0.000 description 5
- 238000005516 engineering process Methods 0.000 description 3
- 238000007599 discharging Methods 0.000 description 2
- 238000003780 insertion Methods 0.000 description 2
- 230000037431 insertion Effects 0.000 description 2
- 238000013507 mapping Methods 0.000 description 2
- 230000000007 visual effect Effects 0.000 description 2
- 230000000712 assembly Effects 0.000 description 1
- 238000000429 assembly Methods 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 230000005611 electricity Effects 0.000 description 1
- 230000005484 gravity Effects 0.000 description 1
- 238000012423 maintenance 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
- 238000013486 operation strategy Methods 0.000 description 1
- 230000004043 responsiveness Effects 0.000 description 1
- 238000006467 substitution reaction Methods 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
- B64C—AEROPLANES; HELICOPTERS
- B64C39/00—Aircraft not otherwise provided for
- B64C39/02—Aircraft not otherwise provided for characterised by special use
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
Abstract
The invention provides a kind of unmanned plane carry device, and it includes the general carry plate, the circuit board that are arranged on uav bottom；The attachment structure for carry connection is provided with the general carry plate；The attachment structure includes link slot group；The link slot group is included in circumferentially upper several the uniform link slots of the general carry plate；The control panel connection of the circuit board and unmanned plane.The present invention is simple in construction, easy to use, by setting steering assembly, the directions such as pitching, the inclination of unmanned plane suspension equipment can be adjusted, so as to meet the cruise mission requirements of distinct device.
Description
Technical field
The present invention relates to unmanned air vehicle technique field, more particularly, to a kind of unmanned plane carry device.
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.
Following defect be present in existing unmanned plane carry device：
1. integrated level is not high, it is necessary to user oneself assembling, debugging aircraft；
2. hardware interface is single, versatility is not strong；
3. structure installation is complicated, delivered payload capability is indefinite；
4. the SDK of non expansivity is opened, no software extensions ability.
In a word, existing unmanned plane carry apparatus function is single, poor universality, can not meet the carry of a variety of cruise tasks
Demand.
The content of the invention
It is an object of the invention to provide a kind of unmanned plane carry device, to solve function list present in prior art
One, poor universality, the technical problem of the carry demand of a variety of cruise tasks can not be met.
In order to solve the above technical problems, the invention provides a kind of unmanned plane carry device, including：It is arranged on unmanned plane bottom
General carry plate, the circuit board in portion；
The attachment structure for carry connection is provided with the general carry plate；
The attachment structure includes link slot group；It is circumferentially upper uniform that the link slot group is included in the general carry plate
Several link slots；
The control panel connection of the circuit board and unmanned plane.
The link slot is evolvent type, i.e., the polar diameter length of the center line of link slot with polar angle change gradually increase or
Person reduces；
The circuit board is arranged in general carry version, and the control panel is also connected with the power supply on unmanned plane；
A variety of data-interfaces and power supply interface are provided with the circuit board；
The attachment structure also includes multiple connecting hole groups, and the multiple connecting hole group is distributed in radius on general carry plate
On different multiple circumference；The connecting hole group includes several connecting holes being distributed on the general same circumference of carry plate；
Or the attachment structure includes multiple connecting holes being dispersed on general carry plate.
The unmanned plane carry device, in addition to carry component；The general carry plate is arranged on nothing by carry component
Man-machine bottom；
The carry component includes box body；
The box body includes the intermediate connector and upper cover body of tubular, and the upper cover body and the general carry plate are set respectively
Put the upper and lower ends in the intermediate connector；
The receiving space for accommodating circuit board is provided with the box body；
A variety of data-interfaces and power supply interface are provided with the circuit board；
The opening stretched out or exposed for data-interface and power supply interface is provided with the upper cover body.
Described unmanned plane carry device, in addition to steering assembly；
The steering assembly is universal connecting components, and the universal connecting components are cross body；
The carry component is arranged on uav bottom by universal connecting components.
Described unmanned plane carry device, in addition to fuselage link；
The fuselage link is used to be fixedly connected with unmanned plane；
The carry component is adjustably arranged on below the fuselage link by steering assembly direction.
The steering assembly includes cross body；
The fuselage link is articulated in by the first drive-connecting shaft adjustable angle on the cross body；
The carry component is articulated in by the second drive-connecting shaft adjustable angle on the cross body, in the throwing of level
In shadow plane, first drive-connecting shaft and second drive-connecting shaft are arranged in a mutually vertical manner.
The fuselage link includes base and two connection wing plates；
Two connection wing plates are parallel to each other interval setting；The cross body be arranged on two connection wing plates it
Between；
It is symmetrically arranged with two connection wing plates for the mounting hole with the described first pivot joint axis connection；
Two connecting plates are provided with the top of the box body, the cross body is arranged between two connecting plates, and two
It is symmetrically arranged with the individual connecting plate for the mounting hole with the described second pivot joint axis connection.
Described unmanned plane carry device, in addition to camera, it is provided with the top of the carry component for described in fixed
The fixed support of camera；The camera angle is adjustably arranged on the fixed support；The camera and circuit board electrical connection.
Described unmanned plane carry device, in addition to hooking device；
The hooking device includes hanger body, latch and executing agency；
The executing agency includes drive mechanism and transmission mechanism, and the drive mechanism passes through transmission mechanism and the latch
Connection；
The hanger body is arranged on the carry component by bindiny 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 circuit board electrically connects with drive mechanism；
The transmission mechanism 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.
Described unmanned plane carry device, in addition to some connecting rods；
The connecting rod is arranged on general carry plate by link slot；
Or the connecting rod is arranged on general carry plate by connecting hole.
The present invention is simple in construction, easy to use, by setting steering assembly, can adjust bowing for unmanned plane suspension equipment
The direction such as face upward, tilt, so as to meet the cruise mission requirements of distinct device.
Meanwhile by being provided with a variety of attachment structures on carry plate, so as to carry different model, specification and kind
Equipment, so as to further increase the versatility of carry system and flexibility.
Hooking device in the present invention is simple in construction, and reliability is higher, and during carry, the hook of external device inserts the U
Type groove, executing agency drive the latch front end to stretch out first pin-and-hole, after the through hole middle through hook described in insertion
Second pin-and-hole, the front end of latch are inserted in the second pin-and-hole, and the posterior segment of latch is inserted in the first pin-and-hole；Two pin-and-holes effectively divide
The load of peripheral hardware equipment has been carried on a shoulder pole, can not have been retracted so as to avoid latch deformation, or has influenceed to be continuing with next time, increase is safeguarded
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.
Using above-mentioned technical proposal, the present invention has the advantages that：
A kind of unmanned plane carry device provided by the invention, it is simple in construction, it is easy to use, can by setting steering assembly
To adjust the directions such as the pitching of unmanned plane suspension equipment, inclination, so as to meet the cruise mission requirements of distinct device.Pass through carry
A variety of attachment structures are provided with plate, so as to the equipment of carry different model, specification and kind, so as to further improve
The versatility of carry system and flexibility.
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 the unmanned plane carry device provided in the embodiment of the present invention；
Fig. 2 is the stereogram of general carry system provided in an embodiment of the present invention；
Fig. 3 is the stereogram at another visual angle of general carry system provided in an embodiment of the present invention；
Fig. 4 is the front view of general carry system provided in an embodiment of the present invention；
Fig. 5 is the upward view of general carry system provided in an embodiment of the present invention；
Fig. 6 is the exploded view of general carry system provided in an embodiment of the present invention；
Fig. 7 is the exploded view of box body in the embodiment of the present invention；
Fig. 8 is the stereogram of camera in the embodiment of the present invention；
Fig. 9 is the front view of unmanned plane carry device in the embodiment of the present invention；
Figure 10 is the stereogram of hooking device provided in an embodiment of the present invention；
Figure 11 is the stereogram of hanger body in the embodiment of the present invention；
Figure 12 is the stereogram at another visual angle of hanger body in the embodiment of the present invention；
Figure 13 is the stereogram of drive mechanism in the embodiment of the present invention；
Figure 14 is the upward view of unmanned plane carry device in the embodiment of the present invention；
Figure 15 is a stereogram of general carry plate in the embodiment of the present invention.
Reference：
1- cameras；2- hooking devices；The general carry systems of 3-；4- connecting rods；4a- connection through holes；4b- connection elongated slots；10-
Fuselage link；11- bases；12- connection wing plates；20- steering assemblies；The cross bodies of 21-；The drive-connecting shafts of 22- first；23-
Two drive-connecting shafts；30- carry components；31- box bodys；31a- upper cover bodies；31b- intermediate connectors；32- circuit boards；33- connecting plates；
34- circuits；35- adpting flanges；36- connecting poles；37- fixed supports；38- drive-connecting shafts；The general carry plates of 40-；50- connections are tied
Structure；51- connecting holes；52- link slots；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- fixed mounts portion；200- executing agencies；210- drive mechanisms；211- is plugged；212-U type open slots；220-
Transmission mechanism；221- first connecting rods；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 illustrated in figs 1 and 9, a kind of unmanned plane carry device that the present embodiment provides, including：General carry system 3, hook
Device 2 and some connecting rods 4；
As illustrated in figs. 2-7, in the present invention, general carry system 3 includes fuselage link 10, steering assembly 20 and carry
Component 30；
Fuselage link 10 is used to be fixedly connected with unmanned plane；
Carry component 30 is adjustably arranged on fuselage link 10 by the direction of steering assembly 20；
The bottom of carry component 30 is provided with general carry plate 40；
A variety of attachment structures 50 for carry connection are provided with general carry plate 40.
Hooking device 2 and some connecting rods 4 are arranged on general carry plate 40.
The present invention is simple in construction, easy to use, by setting steering assembly 20, can adjust bowing for unmanned plane suspension equipment
The direction such as face upward, tilt, so as to meet the cruise mission requirements of distinct device.
Meanwhile by being provided with a variety of attachment structures 50 on general carry plate 40, so as to carry different model, specification
And the equipment of kind, so as to further increase the versatility of carry system and flexibility.
Wherein, steering assembly 20 can be universal connecting components.The form of universal connecting components is a lot, for example, universal connection
Device, flexural pivot assembly etc..
In the present invention, general carry plate 40 is also used for directly being fixedly connected with unmanned plane, by being set on general carry plate 40
The a variety of attachment structures 50 put, connection can be included with the equipment of carry different model, specification and kind, the attachment structure 50
Hole 51 and link slot 52；
Link slot 52 is evolvent type, i.e., the polar diameter length of the center line of link slot 52 with polar angle change gradually increase or
Person reduces；
Multiple connecting holes 51 are respectively distributed on multiple circumference that radius is different on general carry plate 40；
The link slot 52 and multiple connecting holes 51 of evolvent type substantially increase the versatility of carry system of the present invention, can
To meet the installation needs of different size, kind external equipment；
As shown in figure 15, circuit board 32, the control of the circuit board 32 and unmanned plane are provided with the general carry plate 40
The power supply of making sheet and unmanned plane is connected, and a variety of data-interfaces and power supply interface, the data are provided with the circuit board 32
Interface is connected with external equipment, and the power supply interface is powered for external equipment.
In the present invention, carry component 30 is also used for directly being fixedly connected with unmanned plane, and the bottom of carry component 30 is set
There is general carry plate 40, camera 1 is additionally provided with the carry component 30；
The carry component 30 includes box body 31；
The box body includes the intermediate connector 31b and upper cover body 31a, the upper cover body 31a and the general extension of tubular
Support plate 40 is separately positioned on the upper and lower ends of the intermediate connector 31b；
The receiving space for accommodating circuit board 32 is provided with the box body 31；
A variety of data-interfaces and power supply interface are provided with the circuit board 32；
The opening stretched out or exposed for data-interface and power supply interface is provided with the upper cover body 31a；
Connecting plate 33 is provided with the upper cover body 31a, the carry component 30 is connected by connecting plate 33 with unmanned plane；
The general carry plate 40 is connected by screw with carry component 30, a variety of by being set on general carry plate 40
Attachment structure 50, can be with the equipment of carry different model, specification and kind, and the attachment structure 50 includes connecting hole 51 and connected
Access slot 52；
Link slot 52 is evolvent type, i.e., the polar diameter length of the center line of link slot 52 with polar angle change gradually increase or
Person reduces；
Multiple connecting holes 51 are respectively distributed on multiple circumference that radius is different on general carry plate 40；
The link slot 52 and multiple connecting holes 51 of evolvent type substantially increase the versatility of carry system of the present invention, can
To meet the installation needs of different size, kind external equipment；
The camera 1 is connected on carry component 30 by fixed support 37, while camera 1 electrically connects with circuit board 32,
The camera 1 is used for the image for obtaining carry thing below ground image and general carry plate in real time；
The data-interface is connected with external equipment, and the power supply interface is powered for external equipment.
In the present invention, carry component 30 is also connected by steering assembly 20 with unmanned plane；
The steering assembly 20 is cross body 21, and the cross body 21 includes the first drive-connecting shaft 22 and the second pivot
Spindle 23；
The bottom of carry component 30 is provided with general carry plate 40, and camera 1 is additionally provided with the carry component 30；
The general carry plate 40 is connected by screw with carry component 30, a variety of by being set on general carry plate 40
Attachment structure 50, can be with the equipment of carry different model, specification and kind, and the attachment structure 50 includes connecting hole 51 and connected
Access slot 52；
Link slot 52 is evolvent type, i.e., the polar diameter length of the center line of link slot 52 with polar angle change gradually increase or
Person reduces；
Multiple connecting holes 51 are respectively distributed on multiple circumference that radius is different on general carry plate 40；
The link slot 52 and multiple connecting holes 51 of evolvent type substantially increase the versatility of carry system of the present invention, can
To meet the installation needs of different size, kind external equipment；
The carry component 30 includes box body 31；
The box body includes the intermediate connector 31b and upper cover body 31a, the upper cover body 31a and the general extension of tubular
Support plate 40 is separately positioned on the upper and lower ends of the intermediate connector 31b；
The receiving space for accommodating circuit board 32 is provided with the box body 31；
A variety of data-interfaces and power supply interface are provided with the circuit board 32；
The opening stretched out or exposed for data-interface and power supply interface is provided with the upper cover body 31a；
The carry component 30 is connected by connecting plate 33 with the adjustable angle of the second drive-connecting shaft 23；
It is connected to uav bottom the adjustable angle of first drive-connecting shaft 22；
The camera 1 is connected on carry component 30 by fixed support 37, while camera 1 electrically connects with circuit board 32,
The camera 1 is used for the image for obtaining carry thing below ground image and general carry plate in real time；
The data-interface is connected with external equipment, and the power supply interface is powered for external equipment.
In the present invention, as shown in figure 14, general carry plate 40 is additionally provided with connecting rod 4 below, and connecting rod 40 includes connection
Through hole 4a and connection elongated slot 4b；Connection through hole 4a is arranged on one end or both ends of connecting rod 4, for connecting with general carry plate 40
Connect；
Elongated slot 4b radially extending from inside to outside in general carry plate 40 is connected, for being adapted to the outer of connection plurality of specifications
Connect equipment.
As shown in fig. 6, in the present embodiment, steering assembly 20 includes cross body 21；
Fuselage link 10 is articulated in by the adjustable angle of the first drive-connecting shaft 22 on cross body 21；
Carry component 30 is articulated in by the adjustable angle of the second drive-connecting shaft 23 on cross body 21.
Fuselage link 10 includes base 11 and two connection wing plates 12；
First drive-connecting shaft 22 and the second drive-connecting shaft 23 be arranged in parallel with base 11；First drive-connecting shaft 22 and the second drive-connecting shaft 23
It is arranged on mutual vertically on cross body 21.
Two connection wing plates 12 are parallel to each other interval setting；Cross body 21 is arranged between two connection wing plates 12；
The mounting hole for being connected with the first drive-connecting shaft 22 is symmetrically arranged with two connection wing plates 12.
As shown in fig. 7, carry component 30 also includes box body 31 and circuit board 32；
The receiving space for accommodating circuit board 32 is provided with box body 31；
General carry plate 40 is arranged in the opening's edge of the lower ending opening of box body 31.
The top of box body 31 is provided with two connecting plates 33,
Cross body 21 is arranged between two connecting plates 33；
The mounting hole for being connected with the second drive-connecting shaft 23 is symmetrically arranged with two connecting plates 33.
Box body 31 includes intermediate connector 31b and upper cover body 31a, and intermediate connector 31b is tubular, and lower end is provided with footpath
The adpting flange 35 for connection universal carry plate 40 of convex.
Upper cover body 31a and general carry plate 40 are separately positioned on intermediate connector 31b upper and lower ends；
Connecting plate 33 is vertically set on upper cover body 31a top surface.
A variety of data-interfaces and power supply interface are provided with circuit board 32；Data-interface and power supply interface connect as autgmentability
Mouth can meet the needs of user is to different carry tasks.
The opening stretched out or exposed for data-interface and power supply interface is provided with upper cover body 31a.Data-interface or
Person's power supply interface is connected by circuit 34 with other external devices.
The limit circumferentially positioned or spacing for circuit board 32 is provided between circuit board 32 and intermediate connector 31b inwall
Determine structure.
Specifically, limiting structure includes the stopper slot 32a that sets on the top edge of circuit board 32, and with stopper slot 32a
The connecting pole 36 being engaged.
Preferably, the internal thread hole for connecting upper cover body 31a is provided with connecting pole 36.
Attachment structure 50 includes multiple connecting hole groups and a link slot group；
Link slot group is included in the circumferential uniform 3-5 link slot 52 of general carry plate 40；
Link slot 52 is evolvent type, i.e., the polar diameter length of the center line of link slot 52 with polar angle change gradually increase or
Person reduces；
Multiple connecting hole groups are respectively distributed on multiple circumference that radius is different on general carry plate 40；
Connecting hole group includes several connecting holes 51 being distributed on general 40 same circumference of carry plate.
The link slot group of evolvent type and multiple connecting hole groups substantially increase the versatility of carry system of the present invention, can
To meet the installation needs of different size, kind external equipment.
As seen in figs. 6 and 8, the present embodiment also includes camera 1, and the top of carry component 30 is provided with for fixed camera 1
Fixed support 37.Camera 1 is FPV cameras.
The luffing angle of camera 1 is adjustably arranged on fixed support 37.Specifically, camera 1 is articulated in by drive-connecting shaft 38
On fixed support 37, after luffing angle regulation, determine fastener using nut, screw and fix camera 1.
Camera 1 is connected by circuit with the data-interface and/or power supply interface of circuit board 32, and passes through circuit board 32 and nothing
Man-machine control system signal connects.
A kind of unmanned plane carry device provided by the invention, it is simple in construction, it is easy to use, by setting steering assembly 20,
The directions such as pitching, the inclination of unmanned plane suspension equipment can be adjusted, so as to meet the cruise mission requirements of distinct device.Pass through extension
A variety of attachment structures 50 are provided with support plate, so as to the equipment of carry different model, specification and kind, so as to further
Improve versatility and the flexibility of carry system.
As shown in figures 10-13, hooking device 2 includes：Hanger body 100, latch 300 and executing agency 200；
Hanger body 100 also includes seat board portion 120, and several connection through holes are provided with seat board portion 120；The institute of reference picture 1
Show, hanger body is fixedly connected on general carry plate 40 by seat board portion 120 and attachment structure 50.
U-shaped groove 110 is provided with hanger body 100；
U-shaped groove 110 is provided with the first pin-and-hole 111 and the second pin in the opening of U-shaped groove 110 respectively in two side walls
Hole 112；
First pin-and-hole 111 and the second pin-and-hole 112 are coaxially disposed；
Latch 300 is slidably disposed in the first pin-and-hole 111；
Executing agency 200 is connected with the end of latch, for driving the front end of latch 300 to stretch out the first pin-and-hole 111 and inserting
Second pin-and-hole 112, or drive the front end of latch 300 to exit and be retracted into the first pin-and-hole 111 from the second pin-and-hole 112.
Invention hook device 2 is simple in construction, and reliability is higher, and during carry, the hook of external device inserts U-shaped groove
110, executing agency 200 drives the front end of latch 300 to stretch out the first pin-and-hole 111, the pin of insertion second after the through hole middle through hook
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；Two
Pin-and-hole has effectively shared the load of peripheral hardware equipment, deforms and can not retract so as to avoid latch 300, or influences to continue next time
Use, increase 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 of dynamic latch 300 is exited from the second pin-and-hole 112 and is retracted into the first pin-and-hole 111, and hook exits U-shaped groove 110, outside
If equipment is smoothly detached with unmanned plane, so as to substantially increase the operating efficiency of hooking device and reliability.
The aperture of first pin-and-hole 111 is consistent with the external diameter size of latch 300, is oriented to when being slided for latch 300.
First pin-and-hole 111 is consistent with the internal diameter of the second pin-and-hole 112, and the second pin-and-hole 112 is set at the opening's edge of groove side
There are the chamfering inserted for guide 300 or rounding.
Executing agency 200 includes drive mechanism 210 and transmission mechanism 220, drive mechanism 210 by transmission mechanism 220 with
Latch 300 connects, for driving latch 300 to be moved along the first pin-and-hole 111.
Drive mechanism 210 is steering wheel or servomotor.Shown in emphasis reference picture 9, drive mechanism 210 passes through circuit and electricity
Data-interface and/or the power supply interface connection of road plate 32, and be connected by circuit board 32 with unmanned aerial vehicle control system signal.
As shown in figure 11, transmission mechanism 220 is linkage, and the linkage includes the first company of head and the tail connection successively
Bar 221 and second connecting rod 223；
The head end of the first connecting rod 221 is hinged and connected in the drive mechanism 210；The end of the first connecting rod 221
It 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 first connecting rod 221, drives the first connecting rod 221 around the hinge of its head end
Spindle is swung, and then drives the latch 300 to move back and forth along first pin-and-hole 111 by second connecting rod 223.
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 connect, so as to adjust the responsiveness of moment of torsion and latch 300.
As shown in figure 12, hanger body 100 includes the fixed mount portion 130 for fixed drive mechanism 210, fixed mount portion
Two fast assembling-disassembling modules are provided with 130 framework；
Two fast assembling-disassembling modules are oppositely arranged on the both sides of drive mechanism 210 respectively；
Fast assembling-disassembling module includes the contiguous block 500 being fixedly connected in fixed mount portion 130, and contiguous block 500 is in driving machine
The side of structure 210 is provided with slot 510；
As shown in figure 13, the housing both sides of drive mechanism 210 are provided with the plate 211 that cooperation is plugged with slot 510.
Contiguous block 500 is removably attached in fixed mount portion 130 by screw 520, and the interlude of screw 520, which passes through, to be inserted
Groove 510；
It is provided with plate 211 and mutually interts the U-shaped opening groove 212 coordinated with interlude.
Preferably, interlude is cone type, and two sides of U-shaped opening groove 212 are and frustum type interlude wedge inserting
The inclined working of conjunction.
When contiguous block 500 is assembled in fixed mount portion 130 by screw 520, interlude deepens continuously and opened with U-shaped
Mouth groove 212 side is agreed with, and both are simultaneously fixed by frictional fit drive mechanism 210.During dismounting, screw 520 or bolt are screwed out,
Drive mechanism 210 also separates with contiguous block 500 simultaneously, so as to realize fast assembling-disassembling.
As shown in figure 14, connecting rod 4 includes connection through hole 4a and connection elongated slot 4b；Connection through hole 4a is arranged on connecting rod 4
One end or both ends, for being connected with general carry plate 40；
Elongated slot 4b radially extending from inside to outside in general carry plate 40 is connected, for being adapted to the outer of connection plurality of specifications
Connect equipment.
In use, pass through connection through hole 4a and general carry plate using fasteners such as bearing pin, screw or bolt and nuts
Link slot or connecting hole on 40, connecting rod 4 is fixed on general carry plate 40.The quantity of connecting rod 4 is 4,4 companies
Extension bar 4 is laid uniformly in the circumferential direction.
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 (11)
- A kind of 1. unmanned plane carry device, it is characterised in that including：It is arranged on general carry plate, the circuit board of uav bottom；The attachment structure for carry connection is provided with the general carry plate；The attachment structure includes link slot group；It is circumferentially upper uniform some that the link slot group is included in the general carry plate Individual link slot；The control panel connection of the circuit board and unmanned plane.
- 2. unmanned plane carry device according to claim 1, it is characterised in that：The link slot is evolvent type, i.e., the polar diameter length of the center line of link slot gradually increases or subtracted as polar angle changes It is small；The circuit board is arranged in general carry version, and the control panel is also connected with the power supply on unmanned plane；A variety of data-interfaces and power supply interface are provided with the circuit board；The attachment structure also includes multiple connecting hole groups, and it is different that the multiple connecting hole group is distributed in radius on general carry plate Multiple circumference on；The connecting hole group includes several connecting holes being distributed on the general same circumference of carry plate；Or the attachment structure includes multiple connecting holes being dispersed on general carry plate.
- 3. unmanned plane carry device according to claim 1, it is characterised in that also including carry component；The general extension Support plate is arranged on the bottom of unmanned plane by carry component；The carry component includes box body；The box body includes the intermediate connector and upper cover body of tubular, and the upper cover body and the general carry plate are separately positioned on The upper and lower ends of the intermediate connector；The receiving space for accommodating circuit board is provided with the box body；A variety of data-interfaces and power supply interface are provided with the circuit board；The opening stretched out or exposed for data-interface and power supply interface is provided with the upper cover body.
- 4. unmanned plane carry device according to claim 3, it is characterised in that also including steering assembly；The steering assembly is universal connecting components, and the universal connecting components are cross body；The carry component is arranged on uav bottom by universal connecting components.
- 5. unmanned plane carry device according to claim 4, it is characterised in that also including fuselage link；The fuselage link is used to be fixedly connected with unmanned plane；The carry component is adjustably arranged on below the fuselage link by steering assembly direction.
- 6. unmanned plane carry device according to claim 5, it is characterised in that the steering assembly includes cross Body；The fuselage link is articulated in by the first drive-connecting shaft adjustable angle on the cross body；The carry component is articulated in by the second drive-connecting shaft adjustable angle on the cross body, is put down in the projection of level On face, first drive-connecting shaft and second drive-connecting shaft are arranged in a mutually vertical manner.
- 7. unmanned plane carry device according to claim 6, it is characterised in that：The fuselage link includes base and two connection wing plates；Two connection wing plates are parallel to each other interval setting；The cross body is arranged between two connection wing plates；It is symmetrically arranged with two connection wing plates for the mounting hole with the described first pivot joint axis connection；Two connecting plates are provided with the top of the box body, the cross body is arranged between two connecting plates, two institutes State the mounting hole being symmetrically arranged with connecting plate for the described second pivot joint axis connection.
- 8. unmanned plane carry device according to claim 3, it is characterised in that also including camera, the carry component Top is provided with the fixed support for fixing the camera；The camera angle is adjustably arranged on the fixed support；Institute State camera and circuit board electrical connection.
- 9. unmanned plane carry device according to claim 1, it is characterised in that also including hooking device；The hooking device includes hanger body, latch and executing agency；The executing agency includes drive mechanism and transmission mechanism, and the drive mechanism is connected by transmission mechanism and the latch Connect；The hanger body is arranged on the carry component by bindiny mechanism.
- 10. unmanned plane carry device according to claim 9, it is characterised in that：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 circuit board electrically connects with drive mechanism；The transmission mechanism 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.
- 11. unmanned plane carry device according to claim 2, it is characterised in that also including some connecting rods；The connecting rod is arranged on general carry plate by link slot；Or the connecting rod is arranged on general carry plate by connecting hole.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710954605.8A CN107757933B (en) | 2017-10-13 | 2017-10-13 | A kind of unmanned plane carry device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710954605.8A CN107757933B (en) | 2017-10-13 | 2017-10-13 | A kind of unmanned plane carry device |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN107757933A true CN107757933A (en) | 2018-03-06 |
| CN107757933B CN107757933B (en) | 2019-11-29 |
Family
ID=61269546
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201710954605.8A Active CN107757933B (en) | 2017-10-13 | 2017-10-13 | A kind of unmanned plane carry device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN107757933B (en) |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108528738A (en) * | 2018-03-09 | 2018-09-14 | 深圳臻迪信息技术有限公司 | Multifunctional hanging carrying platform |
| CN108820214A (en) * | 2018-06-11 | 2018-11-16 | 天津航天中为数据系统科技有限公司 | A kind of aircraft, which is examined, beats control emission system |
| CN109625270A (en) * | 2018-12-29 | 2019-04-16 | 中航电测仪器股份有限公司 | A kind of helicopter handling carry device and its operation method |
| WO2020107563A1 (en) * | 2018-11-30 | 2020-06-04 | 深圳市大疆创新科技有限公司 | Load control circuit and movable platform |
| CN111348194A (en) * | 2020-04-22 | 2020-06-30 | 西安深瞳智控技术有限公司 | Microminiature unmanned aerial vehicle guided missile mounting and releasing device integrated with fire control system |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN204433059U (en) * | 2015-01-30 | 2015-07-01 | 马鞍山市赛迪智能科技有限公司 | A kind of aircraft carrying manipulator electric saw |
| CN106043699A (en) * | 2016-07-13 | 2016-10-26 | 绵阳空天科技有限公司 | Dropping device of unmanned aerial vehicle |
| CN205819577U (en) * | 2016-05-27 | 2016-12-21 | 优利科技有限公司 | For carry-on fast assembling and disassembling device and aircraft |
| 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 |
| CN206265323U (en) * | 2016-11-10 | 2017-06-20 | 西安理工大学 | A kind of bird repellent audio array device suitable for unmanned plane carry |
| CN106892126A (en) * | 2017-03-13 | 2017-06-27 | 广州鼎飞航空科技有限公司 | A kind of unmanned aerial vehicle onboard disassembly and assembly structure and unmanned plane |
-
2017
- 2017-10-13 CN CN201710954605.8A patent/CN107757933B/en active Active
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN204433059U (en) * | 2015-01-30 | 2015-07-01 | 马鞍山市赛迪智能科技有限公司 | A kind of aircraft carrying manipulator electric saw |
| CN205819577U (en) * | 2016-05-27 | 2016-12-21 | 优利科技有限公司 | For carry-on fast assembling and disassembling device and aircraft |
| CN106043699A (en) * | 2016-07-13 | 2016-10-26 | 绵阳空天科技有限公司 | Dropping device of unmanned aerial vehicle |
| 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 |
| CN206265323U (en) * | 2016-11-10 | 2017-06-20 | 西安理工大学 | A kind of bird repellent audio array device suitable for unmanned plane carry |
| CN106892126A (en) * | 2017-03-13 | 2017-06-27 | 广州鼎飞航空科技有限公司 | A kind of unmanned aerial vehicle onboard disassembly and assembly structure and unmanned plane |
Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108528738A (en) * | 2018-03-09 | 2018-09-14 | 深圳臻迪信息技术有限公司 | Multifunctional hanging carrying platform |
| CN108820214A (en) * | 2018-06-11 | 2018-11-16 | 天津航天中为数据系统科技有限公司 | A kind of aircraft, which is examined, beats control emission system |
| CN108820214B (en) * | 2018-06-11 | 2023-12-22 | 天津航天中为数据系统科技有限公司 | Aircraft scouting control transmitting system |
| WO2020107563A1 (en) * | 2018-11-30 | 2020-06-04 | 深圳市大疆创新科技有限公司 | Load control circuit and movable platform |
| CN111433706A (en) * | 2018-11-30 | 2020-07-17 | 深圳市大疆创新科技有限公司 | Load control circuit and movable platform |
| CN109625270A (en) * | 2018-12-29 | 2019-04-16 | 中航电测仪器股份有限公司 | A kind of helicopter handling carry device and its operation method |
| CN111348194A (en) * | 2020-04-22 | 2020-06-30 | 西安深瞳智控技术有限公司 | Microminiature unmanned aerial vehicle guided missile mounting and releasing device integrated with fire control system |
Also Published As
| Publication number | Publication date |
|---|---|
| CN107757933B (en) | 2019-11-29 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN107757933A (en) | A kind of unmanned plane carry device | |
| CN107757934A (en) | A kind of unmanned plane carry device | |
| CN105857603A (en) | Multi-rotor wing unmanned aerial vehicle of which booms can be folded | |
| CN106428596A (en) | Overall structure of unmanned aerial vehicle for patrolling distribution network and unmanned aerial vehicle thereof | |
| CN112607008A (en) | Anti-collision device based on large-scale many rotor unmanned aerial vehicle | |
| CN207258003U (en) | A kind of hooking device and its unmanned plane | |
| CN204291244U (en) | Electric power depopulated helicopter visible ray accurate detection system | |
| CN107719680A (en) | A kind of unmanned plane carry system | |
| CN107651202A (en) | A kind of hooking device and its unmanned plane | |
| CN217805337U (en) | Flight control test bench and test system | |
| CN105083584B (en) | Flutter model of plane missile system | |
| CN203845019U (en) | Unmanned helicopter inspection tour device carrying device for substation | |
| CN208897341U (en) | A kind of camera shooting unmanned plane with angle regulating function | |
| CN108557093A (en) | A kind of multi-rotor unmanned aerial vehicle cruising inspection system Rapid replacing device | |
| CN204013824U (en) | Power equipment testing fixture | |
| CN206272712U (en) | Image module and unmanned plane | |
| CN207191375U (en) | Connection electrical interface assembly in a kind of small-sized fixed-wing unmanned plane load modularization | |
| CN206243442U (en) | Fast disassembly type hatchcover and the unmanned plane with fast disassembly type hatchcover | |
| WO2023035236A1 (en) | Frame for unmanned aerial vehicle, unmanned aerial vehicle, and kit | |
| CN205916345U (en) | Small -size fixed wing uavs launching cradle | |
| CN205281108U (en) | Regular polyhedron 360 degree non -blind area panorama video capture device | |
| CN205168932U (en) | Unmanned aerial vehicle | |
| CN209938963U (en) | Novel modularization unmanned aerial vehicle | |
| CN209192224U (en) | A kind of easy-to-dismount propeller of unmanned plane | |
| CN203780803U (en) | Shell of multi-lens aerial photography stabilized platform |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CP03 | Change of name, title or address | ||
| CP03 | Change of name, title or address |
Address after: 264200 Zone E, blue venture Valley, No. 40, Yangguang Road, Nanhai new area, Weihai City, Shandong Province Patentee after: Zhendi Technology Co., Ltd Address before: Unit 301, unit a, 9 Fulin Road, Chaoyang District, Beijing 100107 Patentee before: POWERVISION TECH Inc. |