CN107757934B - A kind of unmanned plane carry device - Google Patents
A kind of unmanned plane carry device Download PDFInfo
- Publication number
- CN107757934B CN107757934B CN201710955230.7A CN201710955230A CN107757934B CN 107757934 B CN107757934 B CN 107757934B CN 201710955230 A CN201710955230 A CN 201710955230A CN 107757934 B CN107757934 B CN 107757934B
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- carry
- unmanned plane
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- 230000007246 mechanism Effects 0.000 claims description 53
- 230000005540 biological transmission Effects 0.000 claims description 10
- 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 description 4
- 230000004308 accommodation Effects 0.000 claims description 3
- 230000005611 electricity Effects 0.000 claims 1
- 239000000725 suspension Substances 0.000 abstract description 5
- 230000002093 peripheral effect Effects 0.000 description 8
- 238000009434 installation Methods 0.000 description 4
- 238000003780 insertion Methods 0.000 description 3
- 230000037431 insertion Effects 0.000 description 3
- 238000007599 discharging Methods 0.000 description 2
- 238000005516 engineering process Methods 0.000 description 2
- 230000006870 function Effects 0.000 description 2
- 230000005484 gravity Effects 0.000 description 2
- 238000012423 maintenance Methods 0.000 description 2
- 238000013507 mapping Methods 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 230000000007 visual effect Effects 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000008878 coupling Effects 0.000 description 1
- 238000010168 coupling process Methods 0.000 description 1
- 238000005859 coupling reaction Methods 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- 230000008450 motivation Effects 0.000 description 1
- 238000013486 operation strategy 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
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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
Abstract
The present invention provides a kind of unmanned plane carry devices comprising general carry system and hooking device；The general carry system includes fuselage connection frame, steering assembly, carry component；The fuselage connection frame with unmanned plane for being fixedly connected；The carry component is adjustably arranged in below the fuselage connection frame by steering assembly direction；Connection structure there are many being arranged on the carry component for carry connection；The hooking device is arranged on the carry component.The configuration of the present invention is simple, it is easy to use, by the way that steering assembly, the directions such as pitching, the inclination of adjustable unmanned plane suspension equipment, to meet the cruise mission requirements of distinct device are arranged.
Description
Technical field
The present invention relates to air vehicle technique fields, more particularly, to a kind of unmanned plane carry device.
Background technique
Currently, the operation strategies of unmanned plane are more and more extensive with the development of science and technology, power department, public security department, traffic police
Mechanisms, the units such as department, land mapping, video display camera shooting, live news purchase unmanned plane for solving the various of each department successively
Demand.
Unmanned plane depends on the carry module of unmanned plane as its purposes of carrier, and the different module of carry can be completed
Different task: the tasks such as achievable boat fearness of carry video camera, the tasks such as achievable power-line patrolling of carry infrared camera, carry
The achievable mapping task of remote sensing equipment；If single task role, a frame unmanned plane can be completed, if task is cumbersome to need carry
How module is quickly replaced when disparate modules meet different demands just at stubborn problem.
Existing unmanned plane carry device has following defects that
1. integrated level is not high, user oneself assembling, debugging aircraft are needed；
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 open, no software extensions ability.
In short, existing unmanned plane carry apparatus function is single, poor universality is unable to satisfy the carry of a variety of cruise tasks
Demand.
Summary of the invention
The purpose of the present invention is to provide a kind of unmanned plane carry devices, to solve function list existing in the prior art
One, poor universality, the technical issues of being unable to satisfy the carry demand of a variety of cruise tasks.
In order to solve the above technical problems, a kind of unmanned plane carry device provided by the invention, comprising: general carry system and
Hooking device；
The general carry system includes: fuselage connection frame, steering assembly, carry component；
The fuselage connection frame with unmanned plane for being fixedly connected；
The carry component is adjustably arranged in below the fuselage connection frame by steering assembly direction；
Connection structure there are many being arranged on the carry component for carry connection；
The hooking device is arranged on the carry component.
Further, the hooking device includes hanger body, bolt and executing agency；
The hanger body is arranged on the general carry plate by bindiny mechanism；
U-shaped groove is provided in the hanger body；
The U-shaped groove is provided with the first pin hole and the second pin hole in two side walls；
First pin hole and second pin hole coaxial arrangement；
The bolt is slidably disposed in first pin hole；
The executing agency connect with the end of the bolt, for driving the bolt front end to stretch out first pin hole
And it is inserted into second pin hole, or drive the front end of the bolt from exiting and be retracted into the first pin hole in the second pin hole.
The configuration of the present invention is simple, easy to use, by the way that steering assembly is arranged, adjustable unmanned plane suspension equipment is bowed
The directions such as face upward, tilt, to meet the cruise mission requirements of distinct device.
Meanwhile there are many connection structures by setting on carry plate, so as to carry different model, specification and kind
Equipment, to further improve the versatility and flexibility of carry system.
Hooking device structure in the present invention is simple, and reliability is higher, and when carry, the hook of peripheral device is inserted into the U
Type groove, executing agency drive the bolt front end to stretch out first pin hole, after the through-hole intermediate across hook described in insertion
Second pin hole, the front end of bolt are inserted in the second pin hole, and the posterior segment of bolt is inserted in the first pin hole；Two pin 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 bolt deformation, or influence to continue to use next time, increase maintenance
Cost or use cost.
Since the probability of bolt deformation greatly reduces, when discharging or launching peripheral hardware equipment, described in executing agency's drive
From exiting and being retracted into the first pin hole in the second pin hole, hook exits U-shaped recessed under the external forces such as gravity for the front end of bolt
Slot, peripheral hardware equipment is smoothly detached with unmanned plane, to substantially increase the working efficiency and reliability of hooking device.
Further, the steering assembly is universal connecting components.
Wherein, there are many form of the universal connecting components, for example, joint coupling, flexural pivot assembly etc..
Further, the steering assembly includes cross ontology；
The fuselage connection frame is articulated on the cross ontology by the first drive-connecting shaft adjustable angle；
The carry component is articulated on the cross ontology by the second drive-connecting shaft adjustable angle；
On horizontal projection plane, first drive-connecting shaft and second drive-connecting shaft are arranged in a mutually vertical manner.
Further, the fuselage connection frame includes pedestal and two connection wing plates；
Two connection wing plates, which are parallel to each other, is spaced setting；The cross ontology setting two connection wing plates it
Between；
It is symmetrically arranged on two connection wing plates for the mounting hole with the first pivot joint axis connection.
Further, the carry component further include: box body, circuit board and general carry plate；
The accommodation space for accommodating circuit board is provided in the box body；
The box opening is downward, and general carry plate is arranged in box body bottom；
The connection structure there are many being arranged on the general carry plate for carry connection；
The hooking device is arranged in the general carry board bottom portion.Further, two are provided at the top of the box body
A connecting plate,
The cross ontology is arranged between two connecting plates；
It is symmetrically arranged on two connecting plates for the mounting hole with the second pivot joint axis connection.
Further, the box body includes the intermediate connector and upper cover body of tubular, the upper cover body and the general extension
Support plate is separately positioned on the both ends of the intermediate connector；
The connecting plate is vertically set on the top surface of the upper cover body.
Further, there are many data-interface and power supply interfaces for setting on the circuit board；Data-interface and power supply interface
It can satisfy demand of the user to different carry tasks as scalability interface.
Further, the opening stretched out or exposed for data-interface and power supply interface is provided in the upper cover body.
Further, it is provided between the circuit board and the inner wall of the intermediate connector circumferentially positioned for circuit board
Or the limiting structure of limit.
Preferably, limiting structure includes the limiting slot being arranged on circuit board upper edge, and is matched with the limiting slot
Connecting column.
Preferably, the internal thread hole for connecting the upper cover body is provided on connecting column.
Further, the connection structure includes multiple connecting hole groups and a link slot group；
The link slot group includes uniformly distributed 3-5 link slot in the general carry plate circumferential direction；
The link slot be evolvent type, i.e., the polar diameter length of the center line of link slot with polar angle change be gradually increased or
Person reduces；
Multiple connecting hole groups are respectively distributed on multiple circumference that radius is different on the general carry plate；
The connecting hole group includes several connecting holes being evenly arranged on the general 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.
Further, further include camera, the fixed branch for fixing the camera is provided at the top of the carry component
Frame.
Further, the fixed bracket is adjustably arranged in the camera angle.Specifically, camera passes through drive-connecting shaft
It is articulated on fixed bracket, after pitch angle is adjusted, determines fastener using nut, screw and fix camera.The camera and institute
State circuit board electrical connection.
Further, the aperture of first pin hole is consistent with the bolt outer diameter size, for being oriented to when bolt sliding.
Further, first pin hole is consistent with the internal diameter of second pin hole, and second pin hole is in groove side
Opening's edge at be provided with chamfering or rounding for guiding bolt insertion.
Further, the executing agency includes driving mechanism and transmission mechanism, and the driving mechanism passes through transmission mechanism
It is connect with the bolt, for driving the bolt to move along first pin hole.
Further, the driving mechanism is steering engine or servo motor.
The driving mechanism and the circuit board electrical connection.Specifically, driving mechanism passes through the number of route and circuit board
It connects according to interface and/or power supply interface, and is connect by circuit board with unmanned aerial vehicle control system signal.
Further, the transmission mechanism is link mechanism, and the link mechanism includes that first be sequentially connected end to end connects
Bar and second connecting rod；
The head end of the first connecting rod is connect with the driving mechanism；The end of the first connecting rod and the second connecting rod
Head end is hinged；
The end of second connecting rod and the end of the bolt are hinged；
The driving mechanism passes sequentially through the first connecting rod and second connecting rod drives the bolt along first pin hole
Move back and forth.
The head end of the first connecting rod is arranged at intervals with several for selecting the connecting hole of the connection second connecting rod.It is logical
It crosses and different connecting holes is selected to connect with second connecting rod, to adjust the movement speed of torque and bolt.
It further, further include being provided on external power for providing the external power of power supply to the driving mechanism
Power switch.
Further, the hanger body further include for seat board that is indirect or directly being connect with unmanned plane portion, it is described
Several connection through-holes are provided in seat board portion.
Further, the hanger body includes the fixed part for fixing the driving mechanism, the frame of fixed part
There are two fast assembling-disassembling modules for setting on frame；
Two fast assembling-disassembling modules are oppositely arranged on the two sides of the driving mechanism respectively；
The fast assembling-disassembling module includes the link block being fixedly connected in the fixed part, and the link block is driving
Mechanism side is provided with slot；
The shell two sides of the driving mechanism are provided with the plate that cooperation is plugged with the slot.
Further, the link block is removably attached in the fixed part by bolt or screw, described
The interlude of bolt or screw passes through the slot；
The U-shaped opening slot for mutually interting cooperation with the interlude is provided on the plate.
Further, the interlude is cone type, two sides of the U-shaped opening slot be in the frustum type
Between section wedge inserting close inclined working.
When the link block is assembled in fixed part by bolt or screw, the interlude deepens continuously simultaneously
Agree with U-shaped opening slot side, the two is fixed simultaneously by frictional fit driving mechanism.When disassembly, screw or bolt are screwed out, is driven
Motivation structure is also separated with the link block simultaneously, to realize fast assembling-disassembling.
By adopting the above technical scheme, the invention has the following beneficial effects:
A kind of unmanned plane carry device provided by the invention, structure is simple, easy to use, can by the way that steering assembly is arranged
With directions such as the pitching, the inclinations that adjust unmanned plane suspension equipment, to meet the cruise mission requirements of distinct device.Pass through carry
There are many connection structures for setting on plate, so as to the equipment of carry different model, specification and kind, to further increase
The versatility and flexibility of carry system.
Detailed description of the invention
It below will be to specific in order to illustrate more clearly of the specific embodiment of the invention or technical solution in the prior art
Embodiment or attached drawing needed to be used in the description of the prior art be briefly described, it should be apparent that, it is described below
Attached drawing is some embodiments of the present invention, for those of ordinary skill in the art, before not making the creative labor
It puts, is also possible to obtain other drawings based on these drawings.
Fig. 1 is the perspective view of the unmanned plane carry device provided in the embodiment of the present invention；
Fig. 2 is the perspective view of general carry system provided in an embodiment of the present invention；
Fig. 3 is the perspective view at another visual angle of general carry system provided in an embodiment of the present invention；
Fig. 4 is the main view of general carry system provided in an embodiment of the present invention；
Fig. 5 is the bottom 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 perspective view of camera in the embodiment of the present invention；
Fig. 9 is the main view of unmanned plane carry device in the embodiment of the present invention；
Figure 10 is the perspective view of hooking device provided in an embodiment of the present invention；
Figure 11 is the perspective view of hanger body in the embodiment of the present invention；
Figure 12 is the perspective view at another visual angle of hanger body in the embodiment of the present invention；
Figure 13 is the perspective view of driving mechanism in the embodiment of the present invention.
Appended drawing reference:
1- camera；2- hooking device；The general carry system of 3-；10- fuselage connection frame；11- pedestal；12- connection wing plate；
20- steering assembly；The cross ontology of 21-；The first drive-connecting shaft of 22-；The second drive-connecting shaft of 23-；30- carry component；31- box body；
31a- upper cover body；31b- intermediate connector；32- circuit board；33- connecting plate；34- route；35- connecting flange；36- connecting column；
37- fixes bracket；38- drive-connecting shaft；The general carry plate of 40-；41- connected unit；50- connection structure；51- connecting hole；52- connection
Slot；100- hanger body；110-U type groove；The first pin hole of 111-；The second pin hole of 112-；120- seat board portion；130- fixed frame
Portion；200- executing agency；210- driving mechanism；211- plug；212-U type open slot；213- route；220- transmission mechanism；
221- first connecting rod；222- connecting hole；223- second connecting rod；300- bolt；500- link block；510- slot；520- screw.
Specific embodiment
Technical solution of the present invention is clearly and completely described below in conjunction with attached drawing, it is clear that described implementation
Example is a part of the embodiment of the present invention, instead of all the embodiments.Based on the embodiments of the present invention, ordinary skill
Personnel's every other embodiment obtained without making creative work, shall fall within the protection scope of the present invention.
In the description of the present invention, it should be noted that term " center ", "upper", "lower", "left", "right", "vertical",
The orientation or positional relationship of the instructions such as "horizontal", "inner", "outside" be based on the orientation or positional relationship shown in the drawings, merely to
Convenient for description the present invention and simplify description, rather than the device or element of indication or suggestion meaning must have a particular orientation,
It is constructed and operated in a specific orientation, therefore is not considered as limiting the invention.In addition, term " first ", " second ",
" third " is used for descriptive purposes only and cannot be understood as indicating or suggesting relative importance.
In the description of the present invention, it should be noted that unless otherwise clearly defined and limited, term " installation ", " phase
Even ", " connection " shall be understood in a broad sense, for example, it may be being fixedly connected, may be a detachable connection, or be integrally connected；It can
To be mechanical connection, it is also possible to be electrically connected；It can be directly connected, can also can be indirectly connected through an intermediary
Connection inside two elements.For the ordinary skill in the art, above-mentioned term can be understood at this with concrete condition
Concrete meaning in invention.
Below 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 provided in this embodiment, comprising: general carry system 3 and extension
Hook device 2；
As shown in figures 2-6, general carry system 3 includes fuselage connection frame 10, steering assembly 20 and carry component 30；
Fuselage connection frame 10 with unmanned plane for being fixedly connected；
Carry component 30 is adjustably arranged on fuselage connection frame 10 by 20 direction of steering assembly；
30 bottom of carry component is provided with general carry plate 40；
Connection structure 50 there are many being arranged on general carry plate 40 for carry connection.
The configuration of the present invention is simple, easy to use, by the way that steering assembly 20 is arranged, adjustable unmanned plane suspension equipment is bowed
The directions such as face upward, tilt, to meet the cruise mission requirements of distinct device.
Meanwhile there are many connection structures 50 by setting on general carry plate 40, so as to carry different model, specification
And the equipment of kind, to further improve the versatility and flexibility of carry system.
Wherein, steering assembly 20 can be universal connecting components.There are many form of universal connecting components, for example, universal connection
Device, flexural pivot assembly etc..
As shown in fig. 6, in the present embodiment, steering assembly 20 includes cross ontology 21；
Fuselage connection frame 10 is articulated on cross ontology 21 by 22 adjustable angle of the first drive-connecting shaft；
Carry component 30 is articulated on cross ontology 21 by 23 adjustable angle of the second drive-connecting shaft.
Fuselage connection frame 10 includes pedestal 11 and two connection wing plates 12；
First drive-connecting shaft 22 and the second drive-connecting shaft 23 are arranged in parallel with pedestal 11；First drive-connecting shaft 22 and the second drive-connecting shaft 23
It is arranged on cross ontology 21 mutual vertically.
Two connection wing plates 12, which are parallel to each other, is spaced setting；Cross ontology 21 is arranged between two connection wing plates 12；
The mounting hole for connecting with the first drive-connecting shaft 22 is symmetrically arranged on two connection wing plates 12.
As shown in fig. 7, carry component 30 further includes box body 31 and circuit board 32；
The accommodation space for accommodating circuit board 32 is provided in box body 31；
General carry plate 40 is arranged in the opening's edge of 31 lower ending opening of box body.
The top of box body 31 is arranged there are two connecting plate 33,
Cross ontology 21 is arranged between two connecting plates 33；
The mounting hole for connecting with the second drive-connecting shaft 23 is symmetrically arranged on 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 diameter
The connecting flange 35 for connection universal carry plate 40 of convex.
Upper cover body 31a and general carry plate 40 are separately positioned on the upper and lower ends of intermediate connector 31b；
Connecting plate 33 is vertically set on the top surface of upper cover body 31a.
There are many data-interface and power supply interfaces for setting on circuit board 32；Data-interface and power supply interface connect as scalability
Mouth can satisfy demand of the user to different carry tasks.
The opening stretched out or exposed for data-interface and power supply interface is provided on upper cover body 31a.Data-interface or
Person's power supply interface is connect by route 34 with other external devices.
Be provided between circuit board 32 and the inner wall of intermediate connector 31b for circuit board 32 it is circumferentially positioned or limit limit
Determine structure.
Specifically, limiting structure includes the limiting slot 32a being arranged on 32 top edge of circuit board, and with limiting slot 32a
The connecting column 36 matched.
Preferably, the internal thread hole for connecting upper cover body 31a is provided on connecting column 36.
Connection structure 50 includes multiple connecting hole groups and a link slot group；
Link slot group includes uniformly distributed 3-5 link slot 52 in general 40 circumferential direction of carry plate；
Link slot 52 be evolvent type, i.e., the polar diameter length of the center line of link slot 52 with polar angle change be gradually increased 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 evenly arranged on the same circumference of general carry plate 40.
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 further includes camera 1, and the top of carry component 30 is provided with for fixed camera 1
Fixation bracket 37.
Fixed bracket 37 is adjustably arranged in 1 pitch angle of camera.Specifically, camera 1 is articulated in by drive-connecting shaft 38
On fixed bracket 37, after pitch angle is adjusted, fastener is determined using nut, screw camera 1 is fixed.
Camera 1 is connect by route with the data-interface of circuit board 32 and/or power supply interface, and passes through circuit board 32 and nothing
The connection of man-machine control system signal.
A kind of unmanned plane carry device provided by the invention, structure is simple, easy to use, by the way that steering assembly 20 is arranged,
The directions such as pitching, the inclination of adjustable unmanned plane suspension equipment, to meet the cruise mission requirements of distinct device.Pass through extension
There are many connection structures 50 for setting on support plate, so as to the equipment of carry different model, specification and kind, thus further
Improve the versatility and flexibility of carry system.
As shown in figures 10-13, hooking device 2 includes: hanger body 100, bolt 300 and executing agency 200；
Hanger body 100 further includes seat board portion 120, several connection through-holes are provided in seat board portion 120；Institute referring to Fig.1
Show, hanger body is fixedly connected on general carry plate 40 by seat board portion 120 and connection structure 50.
U-shaped groove 110 is provided in hanger body 100；
U-shaped groove 110 is provided with the first pin hole 111 and the second pin in the opening of U-shaped groove 110 respectively in two side walls
Hole 112；
First pin hole 111 and the coaxial arrangement of the second pin hole 112；
Bolt 300 is slidably disposed in the first pin hole 111；
Executing agency 200 connect with the end of bolt, for driving 300 front end of bolt to stretch out the first pin hole 111 and being inserted into
Second pin hole 112, or drive the front end of bolt 300 from exiting and be retracted into the first pin hole 111 in the second pin hole 112.
2 structure of invention hook device is simple, and reliability is higher, and when carry, the hook of peripheral device is inserted into U-shaped groove
110, executing agency 200 drives 300 front end of bolt to stretch out the first pin hole 111, the second pin of insertion after the through-hole intermediate across hook
Hole 112, the front end of bolt 300 are inserted in the second pin hole 112, and the posterior segment of bolt 300 is inserted in the first pin hole 111；Two
Pin hole has effectively shared the load of peripheral hardware equipment, can not retract so as to avoid the deformation of bolt 300, or influence to continue next time
It uses, increases maintenance cost or use cost.
Since the probability that bolt 300 deforms greatly reduces, when discharging or launching peripheral hardware equipment, 200 band of executing agency
It links up with from exiting and being retracted into the first pin hole 111 in the second pin hole 112 in external forces such as gravity the front end of dynamic bolt 300
Under exit U-shaped groove 110, peripheral hardware equipment is smoothly detached with unmanned plane, thus substantially increase the working efficiency of hooking device with
Reliability.
The aperture of first pin hole 111 is consistent with 300 outer diameter size of bolt, is oriented to when sliding for bolt 300.
First pin hole 111 is consistent with the internal diameter of the second pin hole 112, and the second pin hole 112 is arranged at the opening's edge of groove side
There are the chamfering being inserted into for guide 300 or rounding.
Executing agency 200 include driving mechanism 210 and transmission mechanism 220, driving mechanism 210 by transmission mechanism 220 with
Bolt 300 connects, for driving bolt 300 to move along the first pin hole 111.
Driving mechanism 210 is steering engine or servo motor.For emphasis referring to shown in Fig. 9, driving mechanism 210 passes through route 213
It connect with the data-interface of circuit board 32 and/or power supply interface, and is connect by circuit board 32 with unmanned aerial vehicle control system signal.
As shown in figure 11, transmission mechanism 220 is link mechanism, and the link mechanism includes that first be sequentially connected end to end connects
Bar 221 and second connecting rod 223；
The end of the first connecting rod 221 is hinged with 223 head end of second connecting rod；
The end of second connecting rod 223 and the end of the bolt 300 are hinged；
The driving mechanism 210 is connect with the head end of the first connecting rod 221, passes sequentially through 221 He of first connecting rod
Second connecting rod 223 drives the bolt 300 to move back and forth along first pin hole 111.
The head end of first connecting rod 221 is arranged at intervals with several for selecting the connecting hole 222 of a connection second connecting rod 223.
By selecting different connecting holes 222 to connect with second connecting rod 223, to adjust the movement speed of torque and bolt 300.
As shown in figure 12, hanger body 100 includes the fixed part 130 for fixed drive mechanism 210, fixed part
There are two fast assembling-disassembling modules for setting on 130 frame；
Two fast assembling-disassembling modules are oppositely arranged on the two sides of driving mechanism 210 respectively；
Fast assembling-disassembling module includes the link block 500 being fixedly connected in fixed part 130, and link block 500 is in driving machine
210 side of structure is provided with slot 510；
As shown in figure 13, the shell two sides of driving mechanism 210 are provided with the plate 211 that cooperation is plugged with slot 510.
Link block 500 is removably attached in fixed part 130 by screw 520, and the interlude of screw 520, which passes through, to be inserted
Slot 510；
The U-shaped opening slot 212 for mutually interting cooperation with interlude is provided on plate 211.
Preferably, interlude is cone type, and two sides of U-shaped opening slot 212 are and frustum type interlude wedge inserting
The inclined working of conjunction.
When link block 500 is assembled in fixed part 130 by screw 520, interlude deepens continuously and opens with U-shaped
212 side of mouth slot is agreed with, and the two is fixed simultaneously by frictional fit driving mechanism 210.When disassembly, screw 520 or bolt are screwed out,
Driving mechanism 210 is also separated with link block 500 simultaneously, to realize fast assembling-disassembling.
Finally, it should be noted that the above embodiments are only used to illustrate the technical solution of the present invention., rather than its limitations；To the greatest extent
Pipe present invention has been described in detail with reference to the aforementioned embodiments, those skilled in the art should understand that: its according to
So be possible to modify the technical solutions described in the foregoing embodiments, or to some or all of the technical features into
Row equivalent replacement；And these are modified or replaceed, various embodiments of the present invention technology that it does not separate the essence of the corresponding technical solution
The range of scheme.
Claims (15)
1. a kind of unmanned plane carry device characterized by comprising general carry system and hooking device；
The general carry system includes fuselage connection frame, steering assembly, carry component；
The fuselage connection frame with unmanned plane for being fixedly connected；
The carry component is adjustably arranged in below the fuselage connection frame by steering assembly direction；
Connection structure there are many being arranged on the carry component for carry connection；
The hooking device is arranged on the carry component；
The steering assembly includes cross ontology；
The fuselage connection frame is articulated on the cross ontology by the first drive-connecting shaft adjustable angle；
The carry component is articulated on the cross ontology by the second drive-connecting shaft adjustable angle；It is flat in horizontal projection
On face, first drive-connecting shaft and second drive-connecting shaft are arranged in a mutually vertical manner.
2. unmanned plane carry device according to claim 1, which is characterized in that the hooking device include hanger body,
Bolt and executing agency；
The hanger body is arranged on the carry component by bindiny mechanism；
U-shaped groove is provided in the hanger body；
The U-shaped groove is provided with the first pin hole and the second pin hole in two side walls；
First pin hole and second pin hole coaxial arrangement；
The bolt is slidably disposed in first pin hole；
The executing agency connect with the end of the bolt, for driving the bolt front end to stretch out first pin hole and inserting
Enter second pin hole, or drives the front end of the bolt from exiting and be retracted into the first pin hole in the second pin hole.
3. unmanned plane carry device according to claim 2, which is characterized in that
The fuselage connection frame includes pedestal and two connection wing plates；
Two connection wing plates, which are parallel to each other, is spaced setting；The cross ontology is arranged between two connection wing plates；
It is symmetrically arranged on two connection wing plates for the mounting hole with the first pivot joint axis connection.
4. unmanned plane carry device according to claim 3, which is characterized in that the carry component further includes box body, electricity
Road plate and general carry plate；
The accommodation space for accommodating circuit board is provided in the box body；
The box opening is downward, and general carry plate is arranged in box body bottom；
The connection structure there are many being arranged on the general carry plate for carry connection；
The hooking device is arranged in the general carry board bottom portion.
5. unmanned plane carry device according to claim 4, which is characterized in that there are two connect for the top setting of the box body
Fishplate bar,
The cross ontology is arranged between two connecting plates；
It is symmetrically arranged on two connecting plates for the mounting hole with the second pivot joint axis connection.
6. unmanned plane carry device according to claim 5, which is characterized in that the box body includes the intermediate connection of tubular
Part and upper cover body, the upper cover body and the general carry plate are separately positioned on the upper and lower ends of the intermediate connector；
The connecting plate is vertically set on the top surface of the upper cover body.
7. unmanned plane carry device according to claim 6, which is characterized in that there are many data for setting on the circuit board
Interface and power supply interface；
The opening stretched out or exposed for data-interface and power supply interface is provided in the upper cover body.
8. unmanned plane carry device according to claim 4, which is characterized in that the connection structure includes multiple connecting holes
Group and a link slot group；
The link slot group includes uniformly distributed 3-5 link slot in the general carry plate circumferential direction；
The link slot is evolvent type, i.e., the polar diameter length of the center line of link slot is as polar angle change is gradually increased or is subtracted
It is small；
Multiple connecting hole groups are respectively distributed on multiple circumference that radius is different on the general carry plate；
The connecting hole group includes several connecting holes being evenly arranged on the general same circumference of carry plate.
9. unmanned plane carry device according to claim 4, which is characterized in that it further include camera, the carry component
Top is provided with the fixation bracket for fixing the camera；
The fixed bracket is adjustably arranged in the camera angle；
The camera is connect with the circuit board.
10. unmanned plane carry device according to claim 2, which is characterized in that the aperture of first pin hole with it is described
Bolt outer diameter size is consistent, for being oriented to when bolt sliding.
11. unmanned plane carry device according to claim 4, which is characterized in that the executing agency includes driving mechanism
And transmission mechanism, the driving mechanism is connect by transmission mechanism with the bolt, for driving the bolt along described first
Pin hole is mobile；
The driving mechanism and the circuit board electrical connection.
12. unmanned plane carry device according to claim 11, which is characterized in that
The transmission mechanism is link mechanism, and the link mechanism includes the first connecting rod and second connecting rod being sequentially connected end to end；
The head end of the first connecting rod is connect with the driving 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 bolt are hinged；
The driving mechanism pass sequentially through the first connecting rod and second connecting rod drive the bolt along first pin hole back and forth
It is mobile.
13. unmanned plane carry device according to claim 12, which is characterized in that the head end interval of the first connecting rod is set
Several are equipped with for selecting the connecting hole of the connection second connecting rod.
14. unmanned plane carry device according to claim 11, which is characterized in that the hanger body includes for fixing
The fixed part of the driving mechanism, there are two fast assembling-disassembling modules for setting on the frame of fixed part；
Two fast assembling-disassembling modules are oppositely arranged on the two sides of the driving mechanism respectively；
The fast assembling-disassembling module includes the link block being fixedly connected in the fixed part, and the link block is in driving mechanism
Side is provided with slot；
The shell two sides of the driving mechanism are provided with the plate that cooperation is plugged with the slot.
15. unmanned plane carry device according to claim 14, which is characterized in that the link block passes through bolt or spiral shell
Nail is removably attached in the fixed part, and the interlude of the bolt or screw passes through the slot；
The U-shaped opening slot for mutually interting cooperation with the interlude is provided on the plate.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710955230.7A CN107757934B (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 |
|---|---|---|---|
| CN201710955230.7A CN107757934B (en) | 2017-10-13 | 2017-10-13 | A kind of unmanned plane carry device |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN107757934A CN107757934A (en) | 2018-03-06 |
| CN107757934B true CN107757934B (en) | 2019-10-11 |
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| CN201710955230.7A Expired - Fee Related CN107757934B (en) | 2017-10-13 | 2017-10-13 | A kind of unmanned plane carry device |
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Families Citing this family (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108528738B (en) * | 2018-03-09 | 2021-03-26 | 深圳臻迪信息技术有限公司 | Multifunctional mounting platform |
| CN209070404U (en) * | 2018-11-30 | 2019-07-05 | 深圳市大疆创新科技有限公司 | Load control circuit and moveable platform |
| CN109367788B (en) * | 2018-12-03 | 2023-08-22 | 中航技进出口有限责任公司 | Multifunctional universal suspension device |
| CN110127057B (en) * | 2019-05-22 | 2023-12-22 | 浙江大学滨海产业技术研究院 | Unmanned aerial vehicle's intelligent logistics system |
| CN112722301B (en) * | 2021-01-25 | 2023-04-14 | 中国南方电网有限责任公司超高压输电公司贵阳局 | Unmanned aerial vehicle's mounting mechanism is patrolled and examined with electric wire netting |
Family Cites Families (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| 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 |
| 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 |
| CN205872494U (en) * | 2016-08-01 | 2017-01-11 | 武汉拓普新科无人机科技有限公司 | Unmanned aerial vehicle carry quick detach mechanism |
| CN106394915B (en) * | 2016-11-11 | 2019-08-23 | 深圳市智璟科技有限公司 | Unmanned plane All-in-One mission payload |
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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. |
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Granted publication date: 20191011 |