CN209617512U - Attachment device and UAV system - Google Patents
Attachment device and UAV system Download PDFInfo
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- CN209617512U CN209617512U CN201822138387.3U CN201822138387U CN209617512U CN 209617512 U CN209617512 U CN 209617512U CN 201822138387 U CN201822138387 U CN 201822138387U CN 209617512 U CN209617512 U CN 209617512U
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- fixing seat
- attachment device
- unmanned plane
- supporting element
- hook
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Abstract
The utility model discloses a kind of attachment devices, can be used for unmanned plane hanging articles, comprising: fixing seat, the fixing seat is for being fixed on the unmanned plane；The side that the fixing seat deviates from the unmanned plane, fixing seat described in the other end elastic connection of the supporting element are fixed in supporting element, one end of the supporting element；And hook, the hook connect the other end of the supporting element, the hook is for hanging the object.The utility model additionally provides a kind of UAV system.By the way that supporting element, one end elastic connection fixing seat of supporting element are arranged between fixing seat and hook；When one end of supporting element is by extraneous impact force, one end of supporting element can apply elastic force close to fixing seat and to fixing seat under external force, be set to the unmanned plane in fixing seat with elastic buffer, and unmanned plane is avoided to be collided damage.
Description
Technical field
It is specifically a kind of for the attachment device of unmanned plane and with the company the utility model relates to air vehicle technique field
The UAV system of connection device.
Background technique
UAV is benefit referred to as " unmanned plane " (also referred to as Unmanned Aerial Vehicle, be abbreviated as UAV)
The not manned aircraft manipulated with radio robot and presetting apparatus, or fully or intermittently by car-mounted computer
Automatically operate.Compared with manned aircraft, unmanned plane is more suitable for the task of some more " dirty or dangerous ", and unmanned plane is pressed
Application field, can be divided into it is military with it is civilian, military aspect, unmanned plane is divided into reconnaissance plane and target drone.Civilian aspect, unmanned plane+row
Industry application is that unmanned plane has really just needed；At present take photo by plane, agricultural, plant protection, miniature self-timer, express transportation, disaster relief, sight
Examine wild animal, monitoring infectious disease, mapping, news report, electric inspection process, the disaster relief, movies-making, manufacture romance etc. field
Using greatly having expanded the purposes of unmanned plane itself.When unmanned plane needs Suspended Cargo, need to hang using attachment device
Holder is fixed on unmanned plane.
Therefore, how a kind of attachment device for unmanned plane and carry part is provided, to realize Suspended Cargo on unmanned plane,
As the technical issues that need to address.
Utility model content
The utility model provides a kind of attachment device and UAV system, to realize Suspended Cargo on unmanned plane.
On the one hand, the utility model provides a kind of attachment device, can be used for unmanned plane hanging articles, comprising:
Fixing seat, the fixing seat is for being fixed on the unmanned plane；
The side that the fixing seat deviates from the unmanned plane, the support are fixed in supporting element, one end of the supporting element
Fixing seat described in the other end elastic connection of part；And
Hook, the hook connect the other end of the supporting element, and the hook is for hanging the object.
On the other hand, the utility model additionally provides a kind of UAV system, including unmanned plane and the attachment device,
The attachment device is detachably connected the unmanned plane.
By the way that supporting element is arranged between fixing seat and hook, supporting element can connect hook and fixing seat, and support
One end elastic connection fixing seat of part；The supporting element when one end of supporting element is by extraneous impact force, such as unmanned plane lands
One end can be applied close to fixing seat and to fixing seat under external force by the impact force from bottom surface, one end of supporting element
Elastic force is set to the unmanned plane in fixing seat with elastic buffer, unmanned plane is avoided to be collided damage.
Detailed description of the invention
It, below will be to use required in embodiment in order to illustrate more clearly of the technical solution of the utility model embodiment
Attached drawing be briefly described, it should be apparent that, the drawings in the following description are merely some embodiments of the present invention, right
For those of ordinary skill in the art, without creative efforts, it can also be obtained according to these attached drawings
His attached drawing.
Fig. 1 is a kind of structural schematic diagram of attachment device provided by the embodiment of the utility model.
Fig. 2 is the structural schematic diagram of the supporting element in a kind of attachment device provided by the embodiment of the utility model.
Fig. 3 is the enlarged structure schematic diagram of part A in Fig. 1.
Fig. 4 is a kind of structural schematic diagram of UAV system provided by the embodiment of the utility model.
Specific embodiment
The following will be combined with the drawings in the embodiments of the present invention, carries out the technical scheme in the embodiment of the utility model
Clearly and completely describe, it is clear that the described embodiments are only a part of the embodiments of the utility model, rather than whole
Embodiment.Based on the embodiments of the present invention, those of ordinary skill in the art are under that premise of not paying creative labor
Every other embodiment obtained, fall within the protection scope of the utility model.
Referring to Fig. 1, Fig. 1 is a kind of attachment device 100 provided by the embodiment of the utility model.The attachment device 100 can
For unmanned plane hanging articles.The attachment device 100 can be by being installed on unmanned plane so that unmanned plane can hang, transport
Object.The attachment device 100 is also used as a part of unmanned plane, to realize the function of unmanned plane suspension, transport object.
Referring to Fig. 1, the attachment device 100 includes fixing seat 1, supporting element 2 and hook 3.The fixing seat 1 is for fixing
In the unmanned plane 4.The side that the fixing seat 1 deviates from the unmanned plane 4 is fixed in one end of the supporting element 2.The branch
Fixing seat 1 described in the other end elastic connection of support member 2.The other end of the 3 connection supporting element 2 of hook.The hook 3 is used
In the suspension object.
Specifically, referring to Fig. 1, fixing seat 1 can be substantially plate-like.Fixing seat 1 has the first surface being oppositely arranged
11 and second surface 12.The unmanned plane 4 is set to the second surface 12.Fixing seat 1 is fixed in one end of the supporting element 2
On first surface 11.
By the way that supporting element 2 is arranged between fixing seat 1 and hook 3, supporting element 2 can connect hook 3 and fixing seat 1, and
And one end elastic connection fixing seat 1 of supporting element 2；When one end of supporting element 2 is landed by extraneous impact force, such as unmanned plane 4
When supporting element 2 one end by the impact force from bottom surface, one end of supporting element 2 can be under external force close to fixing seat 1
And elastic force is applied to fixing seat 1, the unmanned plane 4 in fixing seat 1 is set to elastic buffer, unmanned plane 4 is avoided to be collided damage
Wound.
Fig. 1 and Fig. 2 is please referred to, the supporting element 2 includes be hinged first support bar 21 and second support bar 22.Described
The fixing seat is fixed in the end (one end of the first support bar 21 far from the second support bar 22) of one support rod 21
1.The attachment device 100 further includes elastic component 5.The elastic component 5 is connected to the second support bar 22 and the fixing seat 1
Between.When the end (one end of the second support bar 22 far from the first support bar 21) of the second support bar 22 gradually
When close to the fixing seat 1, the elastic component 5 compresses under the action of second support bar 22.
Specifically, referring to Fig. 1, supporting element 2 can be obliquely installed on first surface 11.First support bar 21 is fixed on
First surface 11.Second support bar 22 can be rotated relative to first support bar 21, so that second support bar 22 is far from described
Can be separate or close to fixing seat 1 in one end of one support rod 21.Elastic component 5 is set to the first of second support bar 22 and fixing seat 1
Between surface 11.When one end of second support bar 22 moves closer to first surface 11, second support bar 22 gradually reduces elasticity
Part 5, so that elastic component 5 flexibly supports power to the fixing seat 1 generation, so that the unmanned plane 4 on buffer fixed base 1, avoids nothing
When man-machine 4 landing or hit against when, is damaged, and protects unmanned plane 4.
Specifically, referring to Fig. 2, first support bar 21 can be rotatablely connected with second support bar 22 by rotating pin.
Specifically, one end of first support bar 21 offers card slot 210, one end of second support bar 22 is equipped with fixture block 220.The fixture block
220 are inserted into card slot 210.The one end and fixture block 220 of rotating pin through first support bar 21, to realize first support bar
21 are hinged with second support bar 22.
Specifically, supporting element 2 and fixing seat 1 can be metal, alloy, rigid plastics, carbon fiber with certain rigidity
Etc. materials.First support bar 21 can be integrally formed with fixing seat 1.
Specifically, the elastic component 5 can be spring, it can also be the energy such as elastic slice or elastoplastic, elastic rubber
It enough generates certain deformation and the material of deformation can be restored.In other embodiments, the elastic component 5 can also use air bag, water
Capsule replaces.
Specifically, referring to Fig. 1, fixed plate 15 can be equipped on the first surface 11 of fixing seat 1, for fixing elastic component
5, avoid elastic component 5 from being directly fixed on pedestal 1, and increase the intensity of pedestal 2.
Further, referring to Fig. 1, the compression direction of the elastic component 5 perpendicular to the fixing seat 1 first surface
11.The elastic component 5 connects the first surface 11 with the end of the first support bar 21, so that elastic component 5 is to fixing seat 1
The active force perpendicular to first surface 11 is generated, it can, generation inclination unstable under the action of elastic component 5 to avoid fixing seat 1
Or it shakes.
Further, referring to Fig. 1, one end of the elastic component 5 connects 22 end of second support bar, this second
22 end of strut be far from the first support bar 21 one end so that 22 one end of the second support bar close to fixing seat 1 compared with
Small distance may make that deformation occurs for elastic component 5, improve the sensitivity of 5 deformation of elastic component.
It should be understood that first support bar 21 and second support bar 22 can be total to when supporting element 2 is in relaxation state
Line.When object landing, unmanned plane 4 continues to fall, and object generates opposition to hook 3, so that the one of the first supporting element 2
Hold close to fixing seat 1, and compression elastic piece 5, fixing seat 1 are slowly slowed down under the cushion effect of elastic component 5, avoid unmanned plane 4 by
To impact force.When one end of the first supporting element 2 is close to fixing seat 1, supporting element 2 is in rounding state, 21 He of first support bar
Angle between second support bar 22 can be acute angle or obtuse angle.
Referring to Fig. 1, any one above embodiment is combined, referring to Fig. 1, the quantity of the supporting element 2 is more
It is a.The attachment device 100 further includes block set 6.Multiple supporting elements 2 are rotatablely connected institute far from one end of the fixing seat 1
State block set 6.The connection of block set 6 hook 3.When the block set 6 is close to the fixing seat 1, one end of the second support bar 22 exists
The fixing seat 1 is moved closer under the action of the block set 6.
Specifically, referring to Fig. 1, the connection of multiple supporting elements 2 hook 3.Multiple supporting elements 2 can share the gravity of object,
The problems such as pulling force being subject to when to avoid 2 hanging articles of supporting element is larger, and supporting element 2 is pulled off, the service life is reduced.
Specifically, referring to Fig. 1, multiple supporting elements 2 are all connected with block set 6, so block set 6 can be by multiple supporting elements
2 one end combines, and one end of each supporting element 2 is rotatablely connected block set 6.Specifically, block set 6 can be in a ring.
Wherein, multiple supporting elements 2 are arranged successively along the circumferential direction of block set 6, and multiple supporting elements 2 are scattered centered on sleeve.
It should be understood that the material of multiple supporting elements 2, structure and size can be identical.
Further, referring to Fig. 1, the spacing between multiple supporting elements 2 is equal, so that multiple supporting elements 2 are to fixing seat 1
Amount of force it is identical, and make active force of the fixing seat 1 only by multiple supporting elements 2 perpendicular to first surface 11, to keep away
It is unstable to exempt from fixing seat 1, so that the inclination of unmanned plane 4 or shaking.
When object landing, unmanned plane 4 continues to fall, and object generates opposition to hook 3, so that hook 3 drives
Block set 6 is close to fixing seat 1, and block set 6 drives one end of second support bar 22 to move closer to the fixing seat 1, with compression elastic piece
5 the landing so that unmanned plane 4 can slow down, prevent unmanned plane 4 landing when due to inertia is excessive and by biggish impact
Power.
For example, referring to Fig. 1, the quantity of supporting element 2 is four, being used cooperatively for four supporting elements 2, can be nothing
Man-machine 4 undertake stress in the carry cargo time-division, to extend the service life of each components.When there are four sides for the tool of fixing seat 1
Bian Shi, each supporting element 2 are both secured to the middle position close to a side of fixing seat 1.
In conjunction with any one above-mentioned embodiment, referring to Fig. 1, the hook 3 is detachably connected the supporting element 2.
Specifically, hook 3 is detachably connected block set 6.Further, the block set 6 referring to Fig. 1, hook 3 can be spirally connected, with
It is fixedly connected with hook 3 with block set 6, and can be dismantled from block set 6.Specifically, being provided with threaded hole in block set 6, hang
The outer surface of hook 3 is provided with external screw thread, and block set 6 threadedly links together with hook 3.
In other embodiments, hook 3 can also snap connection with block set 6, is magnetic connection, Nian Jie or pass through rope system
Together etc..
It is detachably connected by setting hook 3 in block set 6, attachment device 100 can remove extension when being not necessarily to hanging articles
Hook 3 hooks to avoid hook 3 to other structures, destroys other structures or hampers the flight of unmanned plane 4.
Referring to Fig. 1, the attachment device 100 further includes collecting part 7.The collecting part 7 is set in the fixing seat 1.
The collecting part 7 is for storing the hook 3.
When attachment device 100 be not necessarily to hanging articles when, hook 3 can be removed and be placed on collecting part 7.It both can be with
It avoids hook 3 from hampering other structures, can also avoid needing to find when needing next time using hook 3.
Specifically, collecting part 7 can be set on the first surface 11 of fixing seat 1.Wherein, collecting part 7 can be velcro.
Collecting part 7 includes magic patch 72 and magic female patch 71.Magic female patch 71 is fixed on first surface 11.Magic female patch 71 is glued
Veneer deviates from first surface 11.One end of magic patch 72 is fixed on first surface 11, and the other end of magic patch 72 is formed
Free end.When being sticked in magic female patch 71 of free end of magic patch 72, magic patch 72 can be arched, magic patch
72 middle section can surround closed space with first surface 11.It is logical hook 3 passed through into closed space hang over magic stick,
Due to store to hook 3, and take full advantage of the space in fixing seat 1.The quantity of collecting part 7 can be multiple groups.
In other embodiments, collecting part 7 can also be the cyclic structure or hook arrangement on first surface 11.
In other embodiments, collecting part 7 can also be the magnet on first surface 11, can be with the hook of magnetic metal material
3.In other embodiments, collecting part 7 can also be the screw hole on first surface 11, to be spirally connected with hook 3.
Fig. 1 and Fig. 3 is please referred to, the fixing seat 1 includes sliding panel 13 and pedestal 14.The sliding panel 13 is slidably connected institute
State pedestal 14.In the vertical direction of the pedestal 14, the relatively described pedestal 14 of the sliding panel 13 is fixed.The sliding panel 13
Or the pedestal 14 is fixed on the unmanned plane 4.
Referring to Fig. 3, the first surface 11 and second surface 12 of the fixing seat 1 can be the first surface 11 of pedestal 14
With second surface 12.Pedestal 14 has through-hole 141.The extending direction of through-hole 141 in parallel with first surface 11.Sliding panel 13 is set to
In the through-hole 141, and the pedestal 14 that is slidably connected.The insertion of first surface 11 of pedestal 14 is provided with locking bolt, will
Sliding panel 13 is fixed on suitable position.
Specifically, referring to Fig. 3, the through-hole 141 can run through the second surface 12.The two side walls of sliding panel 13
It is equipped with retention bead 131, is set to the limiting slot 142 to match with the retention bead 131 on the hole wall of through-hole 141, so that
The retention bead 131 is limited in the limiting slot 142.
The opposite end of sliding panel 13 is stretched out from two openings of through-hole 141 respectively, can on the opposite end of sliding panel 13
To be equipped with fixation hole 132, the fixation hole 132 on sliding panel 13 is passed through using locking bolt 143 and is fixedly connected with unmanned plane 4.
The quantity of the sliding panel 13 can be two.Correspondingly, the quantity of through-hole 141 is also two.Two slidings
Plate 13 is respectively arranged on the opposite sides of pedestal 14.Two sliding panels 13 can be fixed on unmanned plane 4, so that attachment device 100
It is firmly fixed on unmanned plane 4.
Pedestal 14 and the part below of pedestal 14 are fixed on unmanned plane 4 by the way that sliding panel 13 is fixed, it is possible to reduce bottom
The design area of seat 14 saves material and space to reduce the size of attachment device 100.
Referring to Fig. 4, the utility model additionally provides a kind of UAV system 200, including unmanned plane 4 and above-mentioned any one
Attachment device 100 described in kind of embodiment, the attachment device 100 can hanging articles so that unmanned plane 4 can hang and transport
Defeated object.Attachment device 100 is detachably connected unmanned plane 4, in order to need hang and transport object when, installing and connecting apparatus
100, when without hanging and transporting object, dismantling connection device 100 improves the portability and flexibility of unmanned plane.
Unmanned plane 4 further includes multiple brackets 41, when multiple brackets 41 are supported in ground, to ensure that unmanned plane stabilization is fallen
Ground, and attachment device 100 will not contact bottom surface, influence the stability that unmanned plane 4 is stopped to avoid attachment device 100.
The installation process of attachment device 100 provided by the utility model may is that firstly, by sliding panel 13 on pedestal 14
Through-hole 141 in move, behind the mobile suitable position of sliding panel 13, locking bolt 143 is used to pass through consolidating on sliding panel 13
To determine hole 132, is fixed in the lower section of unmanned plane 4, such design method increases the fixed-area of the attachment device 100,
It ensure that stability between the two after installing；Then, hook 3 is installed in block set 6 by way of rotation, by goods
Object is suspended on hook 3, and when not needing to carry out suspension operation, hook 3 is disassembled, is consolidated using collecting part 7
The lower surface for being scheduled on pedestal 14 is stored, and the normal flight for influencing unmanned plane 4 is avoided；When Suspended Cargo, due to logical
Cross what multiple supporting elements 2 linked together pedestal 14 and block set 6, such multiple groups supporting element 2 can be the attachment device 100
It shares and being withstood forces, avoid that single supporting member stress is excessive to be caused to damage, when extending its use；Supporting element 2 includes mutually cutting with scissors
The first support bar 21 and second support bar 22 connect, card slot of the fixture block 220 in first support bar 21 in second support bar 22
210 inner rotations, when unmanned plane 4 is fallen on the ground, hook 3 and block set 6 first contact ground, so that being connected to one with block set 6
The second support bar 22 risen is rotated up relative to first support bar 21, so that elastic component 5 is driven to shrink, such design side
Formula, will the landing of unmanned plane 4 provide a good buffer function.
The utility model increases the fixed-area of the attachment device 100, protects by the way that sliding panel 13 is arranged on pedestal 1
The stability after it is installed between unmanned plane 4 is demonstrate,proved；The design of elastic component 5 can cooperate supporting element 2 during landing
Good buffer function is provided for unmanned plane 4, avoids vibration amplitude excessive, provides good protective effect；Collecting part 7 is set
Meter can store multiple hooks 3, improve its containment and convenience；Multiple groups supporting element 2 is used cooperatively, can be with
Stress is undertaken in the carry cargo time-division for unmanned plane 4, to extend the service life of each components.
It is above-described, only some embodiments of the utility model, but the protection scope of the utility model not office
It is limited to this, anyone skilled in the art is within the technical scope disclosed by the utility model, practical new according to this
Technical solution and its utility model design of type are subject to equivalent substitution or change, should all cover in the protection scope of the utility model
Within.
Claims (10)
1. a kind of attachment device can be used for unmanned plane hanging articles characterized by comprising
Fixing seat, the fixing seat is for being fixed on the unmanned plane；
The side that the fixing seat deviates from the unmanned plane is fixed in supporting element, one end of the supporting element, the supporting element
Fixing seat described in other end elastic connection；And
Hook, the hook connect the other end of the supporting element, and the hook is for hanging the object.
2. attachment device according to claim 1, which is characterized in that the supporting element includes the first support bar being hinged
And the fixing seat is fixed in second support bar, the end of the first support bar, the attachment device further includes elastic component, institute
Elastic component is stated to be connected between the second support bar and the fixing seat；When the end of the second support bar moves closer to institute
When stating fixing seat, the elastic component compresses under the action of the second support bar.
3. attachment device according to claim 2, which is characterized in that one end connection of the elastic component second support
The end of bar.
4. attachment device according to claim 3, which is characterized in that the compression direction of the elastic component is perpendicular to described solid
The first surface of reservation, the elastic component connect the first surface with the end of the first support bar.
5. according to attachment device described in claim 2~4 any one, which is characterized in that the quantity of the supporting element is more
A, the attachment device further includes block set, and multiple supporting elements are rotatablely connected the block set far from one end of the fixing seat,
The block set connects the hook, and when the block set is close to the fixing seat, one end of the second support bar is in the set
The fixing seat is moved closer under the action of seat.
6. attachment device according to claim 5, which is characterized in that the spacing between multiple supporting elements is equal.
7. attachment device described in any one according to claim 1~4, which is characterized in that the hook is detachably connected institute
State supporting element.
8. attachment device according to claim 7, which is characterized in that the attachment device further includes collecting part, the receipts
Part of receiving is set in the fixing seat, and the collecting part is for storing the hook.
9. according to claim 1~4, attachment device described in 6 and 8 any one, which is characterized in that the fixing seat includes sliding
Movable plate and pedestal, the sliding panel are slidably connected the pedestal；In the vertical direction of the pedestal, the sliding panel is with respect to institute
It states pedestal to fix, the sliding panel or the pedestal are fixed on the unmanned plane.
10. a kind of UAV system, which is characterized in that filled including unmanned plane and connection described in any one of claim 1 to 9
It sets, the attachment device is detachably connected with the unmanned plane.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201822138387.3U CN209617512U (en) | 2018-12-18 | 2018-12-18 | Attachment device and UAV system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201822138387.3U CN209617512U (en) | 2018-12-18 | 2018-12-18 | Attachment device and UAV system |
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| Publication Number | Publication Date |
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| CN209617512U true CN209617512U (en) | 2019-11-12 |
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ID=68446175
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| Application Number | Title | Priority Date | Filing Date |
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| CN201822138387.3U Active CN209617512U (en) | 2018-12-18 | 2018-12-18 | Attachment device and UAV system |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112937860A (en) * | 2021-03-03 | 2021-06-11 | 深圳市春晖国际货运代理有限公司 | A unmanned aerial vehicle for logistics distribution |
-
2018
- 2018-12-18 CN CN201822138387.3U patent/CN209617512U/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112937860A (en) * | 2021-03-03 | 2021-06-11 | 深圳市春晖国际货运代理有限公司 | A unmanned aerial vehicle for logistics distribution |
| CN112937860B (en) * | 2021-03-03 | 2022-06-21 | 广东天浩智能科技有限公司 | Unmanned aerial vehicle for logistics distribution |
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