CN109941450A - A kind of multi-functional unmanned flight's device - Google Patents
A kind of multi-functional unmanned flight's device Download PDFInfo
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- CN109941450A CN109941450A CN201910232186.6A CN201910232186A CN109941450A CN 109941450 A CN109941450 A CN 109941450A CN 201910232186 A CN201910232186 A CN 201910232186A CN 109941450 A CN109941450 A CN 109941450A
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- main body
- connecting sleeve
- attachment base
- slide bar
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Abstract
The present invention relates to a kind of multi-functional unmanned flight's devices, including main body and four rotors, four rotors are circumferentially uniformly arranged on the periphery of main body, it further include replacement mechanism, the inside of the main body is equipped with cavity, the inside of main body is arranged in the replacement mechanism, the replacement mechanism includes connecting sleeve, air bag, attachment base, slide bar, spring, trigger assembly and two connection components, the connection component includes mobile casing, fluting, mobile bar and bolt, the trigger assembly includes the second drive rod and two the first drive rods, in multi-functional unmanned flight's device, two connection component operations are driven by trigger assembly, under the action of two connection components, improve the convenient degree dismounted between attachment base and connecting sleeve, unmanned plane is set to carry different types of instrument, improve the practicability of unmanned plane.
Description
Technical field
The present invention relates to unmanned plane field, in particular to a kind of multi-functional unmanned flight's device.
Background technique
UAV is the not manned aircraft manipulated using radio robot and the presetting apparatus provided for oneself,
Or fully or intermittently automatically operated by car-mounted computer, compared with manned aircraft, unmanned plane is often more suitable for
Those dirty or dangerous tasks, unmanned plane press application field, can be divided into it is military with it is civilian, greatly expanded unmanned plane itself
Purposes, developed country also actively extension industrial application and develop unmanned air vehicle technique.
When in use, the instrument of different function is mounted on unmanned plane present unmanned plane by user, can be incited somebody to action
Unmanned plane applies in corresponding field, but the unmanned plane of the prior art is fixedly connected with instrument mostly and is difficult to dismantle,
Cause a unmanned plane that can only carry a kind of instrument, cause the purposes of unmanned plane more single, reduces the practicability of unmanned plane.
Summary of the invention
The technical problem to be solved by the present invention is for overcome the deficiencies in the prior art, provide it is a kind of it is multi-functional nobody fly
Luggage is set.
The technical solution adopted by the present invention to solve the technical problems is: a kind of multi-functional unmanned flight's device, including master
Body and four rotors, four rotors are circumferentially uniformly arranged on the periphery of main body, further include replacement mechanism, the inside of the main body
Equipped with cavity, the inside of main body is arranged in the replacement mechanism；
The replacement mechanism includes connecting sleeve, air bag, attachment base, slide bar, spring, trigger assembly and two connection groups
The lower section of main body is arranged in part, the connecting sleeve, and the plane perpendicular of the connecting sleeve and main body, the air bag setting is even
One end of the close main body of the inside of female connector pipe, the shape of the attachment base are cylinder, and the attachment base is arranged in connector sleeve
The inside of pipe, the periphery of the attachment base and the inner wall of connecting sleeve are tightly connected, and the slide bar is fixed on the inside of main body, institute
The central axis upright of slide bar and connecting sleeve is stated, two connection components are arranged on slide bar, and the spring is set in slide bar
On, the both ends of the spring are connect with two connection components respectively, and the spring is in compressive state, the trigger assembly setting
In the top of slide bar, two connection components are connect with trigger assembly；
The connection component includes mobile casing, fluting, mobile bar and bolt, and the fluting is arranged in the close of main body and connects
On the inner wall of the side of female connector pipe, the fluting is parallel with slide bar, and the movable sleeving pipe sleeve is located on slide bar, the spring and shifting
Dynamic casing is fixedly connected, and the lower section of mobile casing is arranged in the mobile bar, and the mobile bar passes through fluting, and the mobile bar is set
It sets in the side of connecting sleeve, the bottom of the side of the close mobile bar of the connecting sleeve is equipped with aperture, the bolt and cunning
Bar is parallel, and the bolt passes through aperture, and one end of the bolt is fixedly connected with one end far from mobile casing of mobile bar, institute
State the equal length of the distance between the other end of bolt and the inner wall of side of close mobile bar of connecting sleeve with fluting.
Preferably, in order to provide power to two mobile casings, the trigger assembly includes the second drive rod and two
First drive rod, one end of first drive rod and mobile casing are hinged, and the other end of first drive rod and second passes
One end of lever is hinged, and second drive rod is vertical with slide bar, and the side of the separate connecting sleeve of the main body is equipped with through-hole,
The other end of second drive rod passes through through-hole.
Preferably, in order to improve the stability of attachment base installation, the inner wall of the connecting sleeve is equipped with locating piece, institute
The periphery for stating attachment base is equipped with locating slot, and the locating piece is matched with locating slot, and the locating piece is arranged in locating slot
Portion, the locating piece are slidably connected with locating slot.
Preferably, in order to improve the convenient degree of attachment base installation, the side of the separate main body of the other end of the bolt
Equipped with chamfering.
Preferably, in order to improve the convenient degree that attachment base is docked with connecting sleeve, the close main body of the attachment base
The shape of one end is circular cone cylindricality, and the minimum diameter position of the attachment base is located at the top at the maximum gauge position of attachment base.
Preferably, in order to improve the stability that mobile casing is connect with slide bar, the slide bar is equipped with sliding slot, the cunning
The inner wall of the centerline axis parallel of slot and slide bar, the mobile casing is equipped with sliding block, and the sliding block is matched with sliding slot, the cunning
The inside of sliding slot is arranged in block, and the sliding block is slidably connected with sliding slot.
The invention has the advantages that driving two connection groups by trigger assembly in multi-functional unmanned flight's device
Part operation, under the action of two connection components, improves the convenient degree dismounted between attachment base and connecting sleeve, makes unmanned plane
Different types of instrument can be carried, the practicability of unmanned plane is improved, compared with existing replacement mechanism, which passes through
Air bag reduces displacement of the attachment base on the axis direction of connecting sleeve to the thrust of attachment base, passes through locating piece and positioning
The effect of slot reduces rotation of the attachment base inside connecting sleeve to improve the stability of attachment base and improves nobody
The stability that machine installs instruments.
Detailed description of the invention
Present invention will be further explained below with reference to the attached drawings and examples.
Fig. 1 is the structural schematic diagram of multi-functional unmanned flight's device of the invention；
Fig. 2 is the structural schematic diagram of the connecting sleeve of multi-functional unmanned flight's device of the invention；
Fig. 3 is the structural schematic diagram of the attachment base of multi-functional unmanned flight's device of the invention；
In figure: 1. attachment bases, 2. air bags, 3. connecting sleeves, 4. main bodys, 5. mobile casings, 6. first drive rods, 7. second
Drive rod, 8. slide bars, 9. springs, 10. flutings, 11. mobile bars, 12. bolts, 13. locating pieces, 14. locating slots.
Specific embodiment
In conjunction with the accompanying drawings, the present invention is further explained in detail.These attached drawings are simplified schematic diagram, only with
Illustration illustrates basic structure of the invention, therefore it only shows the composition relevant to the invention.
As shown in Figure 1, a kind of multi-functional unmanned flight's device, including main body 4 and four rotors, four rotors are circumferentially uniform
It is arranged on the periphery of main body 4, further includes replacement mechanism, the inside of the main body 4 is equipped with cavity, and the replacement mechanism setting exists
The inside of main body 4；
So that unmanned plane is flown in the sky by the climbing power that rotor rotational generates, makes to grasp under the action of replacing mechanism
Making personnel can be mounted on different types of instrument on unmanned plane, improve the practicability of unmanned plane；
As shown in Figure 1, the replacement mechanism includes connecting sleeve 3, air bag 2, attachment base 1, slide bar 8, spring 9, triggering group
The lower section of main body 4 is arranged in part and two connection components, the connecting sleeve 3, and the bottom surface of the connecting sleeve 3 and main body 4 is hung down
Directly, one end of the close main body 4 of the inside of connecting sleeve 3 is arranged in the air bag 2, and the shape of the attachment base 1 is cylinder,
The inside of connecting sleeve 3 is arranged in the attachment base 1, and the periphery of the attachment base 1 and the inner wall of connecting sleeve 3 are tightly connected,
The slide bar 8 is fixed on the inside of main body 4, the central axis upright of the slide bar 8 and connecting sleeve 3, and two connection components are equal
It is arranged on slide bar 8, the spring 9 is set on slide bar 8, and the both ends of the spring 9 are connect with two connection components respectively, institute
It states spring 9 and is in compressive state, the top of slide bar 8 is arranged in the trigger assembly, and two connection components connect with trigger assembly
It connects；
In fact, a variety of different instruments can be mounted on multiple attachment bases 1 by operator in advance, operator is logical
Pressing trigger assembly is crossed, drives two connection components to be located remotely from each other along slide bar 8 by trigger assembly, then connection component is from connection
The side of the separate main body 4 of seat 1 is removed, and operator can take out attachment base 1 from the inside of connecting sleeve 3, makes operator
Member can remove the instrument currently connecting with unmanned plane, when operator needs to change different types of instrument, behaviour
Make personnel for the inside of the attachment base 1 connecting with instrument insertion connecting sleeve 3, operator unclamps press component later, then
It under the action of the restoring force of spring 9, pulls two connection components close to each other, two connection components is made to be moved to attachment base 1
Separate main body 4 side, attachment base 1 is fixed on to the inside of connecting sleeve 3 by two connection components later, to make nothing
The man-machine instrument that can be carried without type, improves the practicability of unmanned plane, and attachment base 1 is installed to connection in operator
When the inside of casing 3, attachment base 1 is press-connected the air bag 2 inside casing 3, and making air bag 2, deformation occurs, then 2 pairs of companies of air bag
Joint chair 1 generate a thrust, attachment base 1 and connection component tight abutment are made under the action of thrust, reduce attachment base 1 along
The probability of the axis sliding of connecting sleeve 3, improves the stability of attachment base 1 Yu connecting sleeve 3, to improve instrument installation
Stability；
As shown in Figure 1, the connection component includes mobile casing 5, fluting 10, mobile bar 11 and bolt 12, the fluting
10 are arranged on the inner wall of the side of the close connecting sleeve 3 of main body 4,10, the mobile casings parallel with slide bar 8 of the fluting
5 are set on slide bar 8, and the spring 9 is fixedly connected with mobile casing 5, and the mobile bar 11 is arranged under mobile casing 5
Side, the mobile bar 11 pass through fluting 10, and the side of connecting sleeve 3 is arranged in the mobile bar 11, and the connecting sleeve 3 is leaned on
The bottom of the side of nearly mobile bar 11 is equipped with aperture, and the bolt 12 is parallel with slide bar 8, and the bolt 12 passes through aperture, described
One end of bolt 12 is fixedly connected with one end far from mobile casing 5 of mobile bar 11, the other end of the bolt 12 and connection
The equal length of the distance between inner wall of side of close mobile bar 11 of casing 3 and fluting 10；
When mobile casing 5 is moved along slide bar 8, mobile casing 5 drives mobile bar 11 to move along fluting 10, from
And drive bolt 12 mobile by mobile bar 11, when the other end of bolt 12 is moved to the side of the separate main body 4 of attachment base 1
When, by bolt 12 to the position-limiting action of attachment base 1, attachment base 1 is fixed on to the inside of connecting sleeve 3, when bolt 12
When the other end is removed from the side of the separate main body 4 of attachment base 1, bolt 12 disappears to the position-limiting action of attachment base 1, makes to grasp
Making personnel can take out attachment base 1 from the inside of connecting sleeve 3, to improve the convenient degree of the dismounting of attachment base 1.
As shown in Figure 1, the trigger assembly includes the second drive rod 7 and two the first drive rods 6, first drive rod
6 one end and mobile casing 5 are hinged, and the other end of first drive rod 6 and one end of the second drive rod 7 are hinged, and described the
Two drive rods 7 are vertical with slide bar 8, and the side of the separate connecting sleeve 3 of the main body 4 is equipped with through-hole, second drive rod 7
The other end passes through through-hole；
When operator presses the second drive rod 7, the second drive rod 7 then exists to close to the movement of the direction of slide bar 8
Under the transmission effect of two the first drive rods 6, it is located remotely from each other two mobile casings 5 along slide bar 8, when operator unclamps the
When two drive rod 7, under the action of the restoring force of spring 9, pull two mobile casings 5 close to each other along slide bar 8.
As Figure 2-3, the inner wall of the connecting sleeve 3 is equipped with locating piece 13, and the periphery of the attachment base 1 is equipped with
Locating slot 14, the locating piece 13 are matched with locating slot 14, and the inside of locating slot 14, the positioning is arranged in the locating piece 13
Block 13 is slidably connected with locating slot 14；
In locating piece 13 under the position-limiting action of locating slot 14, reducing attachment base 1 in the several of 3 inner rotation of connecting sleeve
Rate, to improve the stability that attachment base 1 is connect with connecting sleeve 3.
Preferably, in order to improve the convenient degree of the installation of attachment base 1, the separate main body 4 of the other end of the bolt 12
Side is equipped with chamfering；
When attachment base 1 is moved up along connecting sleeve 3, by the effect of chamfering, push attachment base 1
Bolt 12 is mobile to the direction far from attachment base 1, can be with to make operator in the case where not pressing the second drive rod 7
Attachment base 1 is installed to the inside of connecting sleeve 3.
Preferably, in order to improve the convenient degree that attachment base 1 is docked with connecting sleeve 3, the close main body of the attachment base 1
The shape of 4 one end is circular cone cylindricality, and the minimum diameter position of the attachment base 1 is located at the maximum gauge position of attachment base 1
Top；
The size that attachment base 1 Yu the close one end of connecting sleeve 3 are reduced by fillet, improving operator will connect
Convenient degree inside insertion connecting sleeve 3 in one end close with connecting sleeve 3 of seat 1, to improve attachment base 1 and connecting sleeve
The convenient degree of 3 docking.
Preferably, in order to improve the stability that mobile casing 5 is connect with slide bar 8, the slide bar 8 is equipped with sliding slot, institute
The centerline axis parallel of sliding slot Yu slide bar 8 is stated, the inner wall of the mobile casing 5 is equipped with sliding block, and the sliding block is matched with sliding slot,
The inside of sliding slot is arranged in the sliding block, and the sliding block is slidably connected with sliding slot；
By the mutual position-limiting action between sliding slot and sliding block, the probability that mobile casing 5 is rotated around slide bar 8 is reduced,
To improve the stability that mobile casing 5 is connect with slide bar 8.
It is drivingly connected component by trigger assembly to remove from the side of attachment base 1, operator can be by attachment base 1 from even
The inside of female connector pipe 3 is taken out, and removes operator by the instrument currently connecting with unmanned plane, when operator needs to change
When upper different types of instrument, the attachment base 1 connecting with the instrument is inserted into the inside of connecting sleeve 3 by operator, it
Operator's release press component pulls two connection components to be moved to attachment base then under the action of the restoring force of spring 9 afterwards
Attachment base 1 is fixed on the inside of connecting sleeve 3 by two connection components later, so that unmanned plane be allow to take by 1 side
The instrument for not having to type is carried, the practicability of unmanned plane is improved.
Compared with prior art, in multi-functional unmanned flight's device, two connection component fortune are driven by trigger assembly
Row, under the action of two connection components, improves the convenient degree dismounted between attachment base 1 and connecting sleeve 5, makes unmanned plane can
To carry different types of instrument, the practicability of unmanned plane is improved, compared with existing replacement mechanism, which passes through gas
Capsule 2 reduces displacement of the attachment base 1 on the axis direction of connecting sleeve 3 to the thrust of attachment base 1, by locating piece 13 with
The effect of locating slot 14 reduces rotation of the attachment base 1 inside connecting sleeve 3, so that the stability of attachment base 1 is improved,
Improve the stability that unmanned plane installs instruments.
Taking the above-mentioned ideal embodiment according to the present invention as inspiration, through the above description, relevant staff is complete
Various changes and amendments can be carried out without departing from the scope of the technological thought of the present invention' entirely.The technology of this invention
Property range is not limited to the contents of the specification, it is necessary to which the technical scope thereof is determined according to the scope of the claim.
Claims (6)
1. a kind of multi-functional unmanned flight's device, including main body (4) and four rotors, four rotors are circumferentially uniformly arranged on main body
(4) on periphery, which is characterized in that further include replacement mechanism, the inside of the main body (4) is equipped with cavity, the replacement mechanism
Inside in main body (4) is set；
The replacement mechanism include connecting sleeve (3), air bag (2), attachment base (1), slide bar (8), spring (9), trigger assembly and
Two connection components, the connecting sleeve (3) are arranged at the lower section of main body (4), the bottom of the connecting sleeve (3) and main body (4)
Face is vertical, one end of close main body (4) of air bag (2) setting in the inside of connecting sleeve (3), the attachment base (1)
Shape is cylinder, and the attachment base (1) is arranged in the inside of connecting sleeve (3), the periphery of the attachment base (1) and connector sleeve
The inner wall for managing (3) is tightly connected, and the slide bar (8) is fixed on the inside of main body (4), the slide bar (8) and connecting sleeve (3)
Central axis upright, two connection components are arranged on slide bar (8), and the spring (9) is set on slide bar (8), the bullet
The both ends of spring (9) are connect with two connection components respectively, and the spring (9) is in compressive state, and the trigger assembly setting exists
The top of slide bar (8), two connection components are connect with trigger assembly；
The connection component includes that mobile casing (5), fluting (10), mobile bar (11) and bolt (12), the fluting (10) set
It sets on the inner wall of the side of the close connecting sleeve (3) of main body (4), the fluting (10) is parallel with slide bar (8), the movement
Casing (5) is set on slide bar (8), and the spring (9) is fixedly connected with mobile casing (5), and mobile bar (11) setting exists
The lower section of mobile casing (5), the mobile bar (11) pass through fluting (10), and the mobile bar (11) is arranged in connecting sleeve (3)
Side, the bottom of the side of the close mobile bar (11) of the connecting sleeve (3) is equipped with aperture, the bolt (12) and slide bar
(8) in parallel, the bolt (12) passes through aperture, one end of the bolt (12) and separate movement casing (5) of mobile bar (11)
One end be fixedly connected, the inner wall of the side of the close mobile bar (11) of the other end and connecting sleeve (3) of the bolt (12)
The distance between equal length with fluting (10).
2. multi-functional unmanned flight's device as described in claim 1, which is characterized in that the trigger assembly includes the second transmission
Bar (7) and two the first drive rods (6), hingedly, described first passes for one end of first drive rod (6) and mobile casing (5)
The other end of lever (6) and one end of the second drive rod (7) are hinged, and second drive rod (7) is vertical with slide bar (8), described
The side of the separate connecting sleeve (3) of main body (4) is equipped with through-hole, and the other end of second drive rod (7) passes through through-hole.
3. multi-functional unmanned flight's device as described in claim 1, which is characterized in that on the inner wall of the connecting sleeve (3)
Equipped with locating piece (13), the periphery of the attachment base (1) is equipped with locating slot (14), the locating piece (13) and locating slot (14)
Matching, the locating piece (13) are arranged in the inside of locating slot (14), and the locating piece (13) is slidably connected with locating slot (14).
4. multi-functional unmanned flight's device as described in claim 1, which is characterized in that the other end of the bolt (12) it is remote
Side from main body (4) is equipped with chamfering.
5. multi-functional unmanned flight's device as described in claim 1, which is characterized in that the close main body of the attachment base (1)
(4) shape of one end is circular cone cylindricality, and the minimum diameter position of the attachment base 1 is located at the maximum gauge position of attachment base 1
Top.
6. multi-functional unmanned flight's device as described in claim 1, which is characterized in that the slide bar (8) is equipped with sliding slot, institute
The centerline axis parallel of sliding slot Yu slide bar (8) is stated, the inner wall of the mobile casing (5) is equipped with sliding block, the sliding block and sliding slot
The inside of sliding slot is arranged in matching, the sliding block, and the sliding block is slidably connected with sliding slot.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910232186.6A CN109941450B (en) | 2019-03-26 | 2019-03-26 | Multifunctional unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910232186.6A CN109941450B (en) | 2019-03-26 | 2019-03-26 | Multifunctional unmanned aerial vehicle |
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| Publication Number | Publication Date |
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| CN109941450A true CN109941450A (en) | 2019-06-28 |
| CN109941450B CN109941450B (en) | 2020-12-04 |
Family
ID=67010766
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201910232186.6A Active CN109941450B (en) | 2019-03-26 | 2019-03-26 | Multifunctional unmanned aerial vehicle |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111106845A (en) * | 2019-12-25 | 2020-05-05 | 深圳市迅成科技有限公司 | Place stable on-vehicle intercom that has damping function |
Citations (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB962104A (en) * | 1959-10-19 | 1964-06-24 | Robert Spencer | Improvements in landing nets |
| JPH11117640A (en) * | 1997-10-17 | 1999-04-27 | Mitsuboshi Belting Ltd | Sealing device of turning door with extension flush bolt |
| CN103050901A (en) * | 2013-01-06 | 2013-04-17 | 杭州恒信电气有限公司 | Locking devices of valves in armoured movable-type metal-enclosed switchgear |
| CN106394919A (en) * | 2016-11-01 | 2017-02-15 | 合肥星服信息科技有限责任公司 | Rotor wing unmanned aerial vehicle with angle-adjustable aerial photography camera and storage structure |
| CN207030139U (en) * | 2017-07-10 | 2018-02-23 | 三六零医药电子商务有限公司 | A kind of logistics warehouse sorting plant |
| CN107933928A (en) * | 2018-01-16 | 2018-04-20 | 安徽翼讯飞行安全技术有限公司 | A kind of unmanned plane article loading device |
| CN207360572U (en) * | 2017-08-23 | 2018-05-15 | 广州市妙伊莲科技有限公司 | A kind of unmanned plane rack construction |
| CN207565853U (en) * | 2017-11-01 | 2018-07-03 | 恩欣格工程塑料（上海）有限公司 | A kind of unmanned plane camera carry device |
| CN207580157U (en) * | 2017-11-22 | 2018-07-06 | 江西天一航空装备有限公司 | A kind of holder connection device that rises and falls of helicopter |
| CN208226489U (en) * | 2018-05-18 | 2018-12-11 | 天津星网科技有限公司 | For the locking support device of cable testing bridge |
| CN109018363A (en) * | 2018-07-05 | 2018-12-18 | 深圳市律远汇智科技有限公司 | A kind of intelligent express delivery unmanned plane of good fixing effect |
-
2019
- 2019-03-26 CN CN201910232186.6A patent/CN109941450B/en active Active
Patent Citations (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB962104A (en) * | 1959-10-19 | 1964-06-24 | Robert Spencer | Improvements in landing nets |
| JPH11117640A (en) * | 1997-10-17 | 1999-04-27 | Mitsuboshi Belting Ltd | Sealing device of turning door with extension flush bolt |
| CN103050901A (en) * | 2013-01-06 | 2013-04-17 | 杭州恒信电气有限公司 | Locking devices of valves in armoured movable-type metal-enclosed switchgear |
| CN106394919A (en) * | 2016-11-01 | 2017-02-15 | 合肥星服信息科技有限责任公司 | Rotor wing unmanned aerial vehicle with angle-adjustable aerial photography camera and storage structure |
| CN207030139U (en) * | 2017-07-10 | 2018-02-23 | 三六零医药电子商务有限公司 | A kind of logistics warehouse sorting plant |
| CN207360572U (en) * | 2017-08-23 | 2018-05-15 | 广州市妙伊莲科技有限公司 | A kind of unmanned plane rack construction |
| CN207565853U (en) * | 2017-11-01 | 2018-07-03 | 恩欣格工程塑料（上海）有限公司 | A kind of unmanned plane camera carry device |
| CN207580157U (en) * | 2017-11-22 | 2018-07-06 | 江西天一航空装备有限公司 | A kind of holder connection device that rises and falls of helicopter |
| CN107933928A (en) * | 2018-01-16 | 2018-04-20 | 安徽翼讯飞行安全技术有限公司 | A kind of unmanned plane article loading device |
| CN208226489U (en) * | 2018-05-18 | 2018-12-11 | 天津星网科技有限公司 | For the locking support device of cable testing bridge |
| CN109018363A (en) * | 2018-07-05 | 2018-12-18 | 深圳市律远汇智科技有限公司 | A kind of intelligent express delivery unmanned plane of good fixing effect |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111106845A (en) * | 2019-12-25 | 2020-05-05 | 深圳市迅成科技有限公司 | Place stable on-vehicle intercom that has damping function |
Also Published As
| Publication number | Publication date |
|---|---|
| CN109941450B (en) | 2020-12-04 |
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