CN109732515A - A kind of unmanned plane dynamical system is horizontally mounted debugging apparatus - Google Patents
A kind of unmanned plane dynamical system is horizontally mounted debugging apparatus Download PDFInfo
- Publication number
- CN109732515A CN109732515A CN201910071643.8A CN201910071643A CN109732515A CN 109732515 A CN109732515 A CN 109732515A CN 201910071643 A CN201910071643 A CN 201910071643A CN 109732515 A CN109732515 A CN 109732515A
- Authority
- CN
- China
- Prior art keywords
- track
- unmanned plane
- support
- adjusting
- assembly
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Granted
Links
Landscapes
- Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)
- Forklifts And Lifting Vehicles (AREA)
Abstract
The invention discloses a kind of unmanned plane dynamical systems to be horizontally mounted debugging apparatus, including assembly bench, assemble track, second track and telescopic leg support, support bracket is installed above the assembly bench, and support bar is installed on support bracket, the second adjusting ring is connected on the inside of the first adjusting ring, the first track is installed above the second adjusting ring, and first offers the first link slot on track, the telescopic leg support is located at the lower section of assembly bench, and mounting base is connected in telescopic leg support, and telescopic leg support is connected with each other by mounting base and assembly bench.The unmanned plane dynamical system is horizontally mounted debugging apparatus, the convenient power motor assembled to needs carries out horizontal stable clamping, motor is assembled to convenient, it avoids motor from occurring tilting in assembling process and the case where angle offset, improves the stability of motor assembly and improve the stability of unmanned plane during flying.
Description
Technical field
The present invention relates to air vehicle technique field, specially a kind of unmanned plane dynamical system is horizontally mounted debugging apparatus.
Background technique
Unmanned plane is a kind of Miniature Vehicle machine, is mostly used to be taken photo by plane or be assisted agriculture herbal sprinkling, existing nothing
Man-machine components carry out both assembly, inefficiency by worker mostly, while assembling accuracy is not high, and unmanned plane is caused to exist
Unstable situation is easy to appear in flight course, the assembly of especially unmanned plane power motor is particularly important, and motor assembles
Existing angular deviation is easy to cause unmanned plane that can not carry out steadily hovering or turning flight direction in flight course, influences normal
Flight operation, will appear air crash situation if serious, to reduce the product quality of unmanned plane, influence the normal of unmanned plane
It uses.
Summary of the invention
The purpose of the present invention is to provide a kind of unmanned plane dynamical systems to be horizontally mounted debugging apparatus, to solve above-mentioned background
There is angular deviation and is easy to cause unmanned plane that can not be stablized in flight course in the unmanned plane motor assembly proposed in technology
Hovering or turning flight direction, influence normal flight operation, will appear air crash situation if serious, to reduce nobody
The product quality of machine, the problem of influencing the normal use of unmanned plane.
To achieve the above object, the invention provides the following technical scheme: a kind of unmanned plane dynamical system is horizontally mounted debugging
Device, including assembly bench, assembly track, the second track and telescopic leg support, and are equipped with support bracket above the assembly bench, and
Support bar is installed on support bracket, level meter is installed below the assembly bench, and is provided with the first tune above assembly bench
Ring is saved, the second adjusting ring is connected on the inside of the first adjusting ring, and be fixed with barre on the second adjusting ring, described second adjusts
The first track is installed above section ring, and offers the first link slot on the first track, is set on the inside of first link slot
It is equipped with the first link block, and the first link block is connected with each other by the first link slot and the first track, the assembly track is located at
The top of first track, and assemble and vertical pivot is installed below track, and assemble track and pass through vertical pivot and the first link block phase
It connects, the second link slot is provided on the assembly track, and assemble and mounting clip, the mounting clip are installed above track
Lower section be provided with the second link block, and mounting clip is connected with each other by the second link block and the second link slot and assembly track,
And fastening bolt is provided on mounting clip, second track is located at the outside of the first track, and is equipped on the second track perpendicular
Bar offers regulating tank on the vertical bar, and is equipped with adjusting rod on the inside of regulating tank, and adjusting is equipped on the adjusting rod
Block, and connecting hole is reserved on adjusting block, the adjusting block is connected with each other by connecting hole and adjusting rod, and fixed on adjusting block
There is clamping device, the telescopic leg support is located at the lower section of assembly bench, and is connected with mounting base in telescopic leg support, and stretch
Foot support is connected with each other by mounting base and assembly bench.
Preferably, the support bracket is cyclic structure, and support bar is incline structure, and support bar is in support bracket
Side is angularly distributed.
Preferably, the support bar includes loop bar, support rod, reset spring and foot pad, and is respectively set on the inside of loop bar
There are support rod and reset spring, and reset spring is installed on support rod, support rod is mutually interconnected by reset spring with loop bar
It connects, foot pad is installed on support rod.
Preferably, the support rod constitutes stretching structure by reset spring and loop bar, and support rod and foot pad are constituted and revolved
Rotation structure, and foot pad is rubber material.
Preferably, screw thread is provided on the inside of the first adjusting ring, and the first adjusting ring is nested in the second adjusting ring
Outside, and the second adjusting ring is fixedly connected with the first track.
Preferably, first track and the second track are cyclic structure, and the first track and the second track respectively with
First link block and vertical bar constitute slide construction.
Preferably, the number of the assembly track is provided with 6, and assembles track and be made up of vertical pivot and the first link block
Rotational structure, and the connection structure assembled between track and mounting clip is identical as the connection structure between the second track and vertical bar.
Preferably, to be threadedly coupled between the adjusting rod and adjusting block, and adjusting block and vertical bar constitute slide construction, and
And adjusting rod and vertical bar constitute rotational structure.
Compared with prior art, the beneficial effects of the present invention are: the unmanned plane dynamical system is horizontally mounted debugging apparatus,
1, horizontal stable clamping conveniently is carried out to the power motor that needs assemble, so that convenient assemble motor, avoids horse
Up to occurring tilting in assembling process and the case where angle offset, improve the stability of motor assembly and improve nobody
The stability of machine flight；
2, assembly track can be slided on the first track, personnel convenient for assembly according to four wing unmanned planes or six wings nobody
The demand of machine is adjusted, and is conducive to carry out stablizing assembly to two kinds of unmanned plane, be improved to different type of machines unmanned plane
Adaptation ability；
3, it is perfused with moisture in cloche, facilitates user judges whether fixing motor is located at level in sleeve according to horizontal line observation
Position, and then user is facilitated to adjust the angle of the motor in sleeve by sleeve and bracket, be conducive to motor and be in a horizontal position
The case where being assembled, avoiding the occurrence of angle offset.
Detailed description of the invention
Fig. 1, which is that the present invention is whole, just cuts open structural schematic diagram；
Fig. 2 is present invention assembly installation structure of track schematic diagram；
Fig. 3 is support rod structure schematic diagram of the present invention；
Fig. 4 is support bar mounting structure schematic diagram of the present invention；
Fig. 5 is adjusting block mounting structure schematic diagram of the present invention；
Fig. 6 is that the present invention first adjusts ring structure schematic diagram；
Fig. 7 is enlarged structure schematic diagram at the A in Fig. 1 of the present invention.
In figure: 1, assembly bench；2, support bracket；3, support bar；301, loop bar；302, support rod；303, reset spring；304,
Foot pad；4, level meter；5, first ring is adjusted；6, second ring is adjusted；7, barre；8, the first track；9, the first link slot；10,
One link block；11, vertical pivot；12, track is assembled；13, the second link slot；14, mounting clip；15, the second link block；16, fastening bolt；
17, the second track；18, vertical bar；19, regulating tank；20, adjusting rod；21, adjusting block；22, connecting hole；23, clamping device；24, it stretches
The support of contracting foot；25, mounting base.
Specific embodiment
Following will be combined with the drawings in the embodiments of the present invention, and technical solution in the embodiment of the present invention carries out clear, complete
Site preparation description, it is clear that described embodiments are only a part of the embodiments of the present invention, instead of all the embodiments.It is based on
Embodiment in the present invention, it is obtained by those of ordinary skill in the art without making creative efforts every other
Embodiment shall fall within the protection scope of the present invention.
Please refer to Fig. 1-7, the present invention provides a kind of technical solution: a kind of unmanned plane dynamical system is horizontally mounted debugging dress
It sets, including assembly bench 1, assembly track 12, the second track 17 and telescopic leg support 24, the top of assembly bench 1 is equipped with support bracket
2, and support bar 3 is equipped on support bracket 2, support bracket 2 is cyclic structure, and support bar 3 is incline structure, and support bar 3
It is angularly distributed in the inside of support bracket 2, convenient to carry out adaptability fitting support to unmanned plane main body, support bar 3 includes loop bar
301, support rod 302, reset spring 303 and foot pad 304, and the inside of loop bar 301 is respectively arranged with support rod 302 and resets bullet
Spring 303, and reset spring 303 is installed on support rod 302, support rod 302 is made up of reset spring 303 and loop bar 301
Stretching structure, and support rod 302 and foot pad 304 constitute rotational structure, and foot pad 304 is rubber material, facilitates support rod 302
It drives foot pad 304 to carry out automatic attaching support to unmanned plane main body, is conducive to adapt to uav bottom shape, support rod 302 is logical
It crosses reset spring 303 and loop bar 301 is connected with each other, foot pad 304 is installed on support rod 302, is conducive to support bar 3 and carries out flexibly
Movement, the lower section of assembly bench 1 is equipped with level meter 4, and the top of assembly bench 1 is provided with the first adjusting ring 5, and first adjusts ring 5
Inside be provided with screw thread, and the first adjusting ring 5 is nested in the outside of the second adjusting ring 6, and second adjusts ring 6 and the first rail
Road 8 is fixedly connected, and is conducive to the second adjusting ring 6 first and is adjusted adjustable diameter and screw adjusting height on ring 5；
The inside of first adjusting ring 5 is connected with the second adjusting ring 6, and is fixed with barre 7 on the second adjusting ring 6, and second adjusts ring 6
Top the first track 8 is installed, and the first link slot 9 is offered on the first track 8, the first track 8 and the second track 17 are
For cyclic structure, and the first track 8 and the second track 17 constitute slide construction with the first link block 10 and vertical bar 18 respectively, convenient
Corresponding assembly track 12 and vertical bar 18 carry out slide displacement adjusting, and the inside of the first link slot 9 is provided with the first link block 10,
And first link block 10 be connected with each other by the first link slot 9 and the first track 8, assemble track 12 and be located at the upper of the first track 8
Side, and the lower section for assembling track 12 is equipped with vertical pivot 11, and it is mutual by vertical pivot 11 and the first link block 10 to assemble track 12
Connection, the number of assembly track 12 are provided with 6, and assemble track 12 and constitute rotation knot by vertical pivot 11 and the first link block 10
Structure, and assemble the connection structure between track 12 and mounting clip 14 and the connection structure phase between the second track 17 and vertical bar 18
Together, be conducive to the unmanned plane horn being fixed on mounting clip 14 and carry out angular adjustment and displacement adjusting, assemble track 12
On be provided with the second link slot 13, and the top for assembling track 12 is equipped with mounting clip 14；
The lower section of mounting clip 14 is provided with the second link block 15, and mounting clip 14 passes through the second link block 15 and the second link slot 13
It is connected with each other with assembly track 12, and is provided with fastening bolt 16 on mounting clip 14, the second track 17 is located at the outer of the first track 8
Side, and vertical bar 18 is installed on the second track 17, regulating tank 19 is offered on vertical bar 18, and the inside of regulating tank 19 is equipped with tune
Pole 20 is threadedly coupled between adjusting rod 20 and adjusting block 21, and adjusting block 21 and vertical bar 18 constitute slide construction, and adjust
Pole 20 and vertical bar 18 constitute rotational structure, the cunning for facilitating adjusting rod 20 that adjusting block 21 is driven to carry out upper and lower position on vertical bar 18
It is dynamic to adjust, adjusting block 21 is installed on adjusting rod 20, and connecting hole 22 is reserved on adjusting block 21, adjusting block 21 passes through connecting hole
22 are connected with each other with adjusting rod 20, and clamping device 23 is fixed on adjusting block 21, and telescopic leg support 24 is located under assembly bench 1
Side, and mounting base 25 is connected in telescopic leg support 24, and telescopic leg support 24 is interconnected by mounting base 25 and 1 phase of assembly bench
It connects.
Working principle: according to Fig. 1, the position of assembly bench 1 will be adjusted by telescopic leg support 24 first, until assembly
Level meter 4 on platform 1 is in a horizontal position, and is at this time placed into unmanned plane main body on the support bar 3 of 2 inside of support bracket, support
Extruding of the support rod 302 by unmanned plane main body on bar 3, the support rod 302 being squeezed is by reset spring 303 in loop bar
301 inside carries out self-adapting stretching adjusting, so that support rod 302 drives foot pad 304 to carry out fitting support to unmanned plane main body,
The stability being supported to unmanned plane main body is improved, while facilitating the unmanned plane main body for adapting to different type of machines；
According to Fig. 1-7, after unmanned plane main body, which completes support, places, unmanned plane horn is placed on mounting clip 14,
The fastening bolt 16 reused on mounting clip 14 carries out stable holding to unmanned plane horn, is just completed in this way to unmanned plane horn
It grips, then unmanned plane motor base is installed on clamping device 23, clamping device 23 at this time then drives unmanned plane
Motor base maintains horizontal position, and unmanned plane motor is facilitated to be installed；
According to Fig. 1-7, after the related unmanned plane motor of unmanned plane motor base completes the placement of horizontal position, revolve manually
Modulation pole 20, adjusting rod 20 drives regulating tank 19 of the adjusting block 21 on vertical bar 18 to carry out sliding position by connecting hole 22 at this time
It moves, until adjusting block 21 drives unmanned plane motor to be adjusted to suitable height by clamping device 23, then passes through vertical bar 18
Second track 17 carry out slidable adjustment, until vertical bar 18 by clamping device 23 drive unmanned plane motor slide displacement to nobody
The corresponding position of machine horn then continues to the height that unmanned plane motor is adjusted by adjusting rod 20, until facilitating unmanned plane horse
Match up in the enterprising luggage of unmanned plane horn, after unmanned plane motor completes assembly on unmanned plane horn, unscrews clamping device
23, then clamping device 23 is withdrawn from unmanned plane motor and pedestal；
According to Fig. 1-7, after unmanned plane motor completes assembly, mounting clip 14 is pushed to exist by the second link block 15 manually
It is slided on assembly track 12, until mounting clip 14 slides the unmanned plane main body on support bracket 2 with unmanned plane horn,
At the same time can vertical pivot 11 angle rotation carried out to mounting clip 14 and unmanned plane horn adjust, while mounting clip 14 can lead to
It crosses the first link block 10 and the first link slot 9 and sets adjusting in the enterprising line position of the first track 8, and user can also pass through barre 7
It drives the second adjusting ring 6 to carry out rotation adjusting second in the inside of the first adjusting ring 5 and adjusts the height of ring 6, and then facilitate drive
Unmanned plane horn in mounting clip 14 adjusts height, until unmanned plane horn is carried out with installation site corresponding in unmanned plane main body
To it, thus the case where facilitating unmanned plane horn alignment unmanned plane main body accurately to be installed, avoid the occurrence of loading error, in this way
A kind of unmanned plane dynamical system be horizontally mounted debugging apparatus facilitate user carry out using.
It although an embodiment of the present invention has been shown and described, for the ordinary skill in the art, can be with
A variety of variations, modification, replacement can be carried out to these embodiments without departing from the principles and spirit of the present invention by understanding
And modification, the scope of the present invention is defined by the appended.
Claims (8)
1. a kind of unmanned plane dynamical system is horizontally mounted debugging apparatus, including assembly bench (1), assembly track (12), the second track
(17) and telescopic leg supports (24), it is characterised in that: is equipped with support bracket (2) above the assembly bench (1), and support bracket
(2) it is equipped on support bar (3), is equipped with level meter (4) below the assembly bench (1), and the top setting of assembly bench (1)
There is the first adjusting ring (5), is connected with the second adjusting ring (6) on the inside of first adjusting ring (5), and second is adjusted on ring (6)
It is fixed with barre (7), is equipped with the first track (8) above second adjusting ring (6), and offered on the first track (8)
First link slot (9) is provided with the first link block (10) on the inside of first link slot (9), and the first link block (10) is logical
The first link slot (9) and the first track (8) to be crossed to be connected with each other, assembly track (12) is located at the top of the first track (8), and
Vertical pivot (11) are installed below assembly track (12), and assembles track (12) and passes through vertical pivot (11) and the first link block (10)
It is connected with each other, is provided with the second link slot (13) on the assembly track (12), and assemble and dress is installed above track (12)
It with folder (14), is provided with the second link block (15) below the mounting clip (14), and mounting clip (14) passes through the second link block
(15) it is connected with each other with the second link slot (13) with assembly track (12), and is provided with fastening bolt (16) on mounting clip (14),
Second track (17) is located at the outside of the first track (8), and vertical bar (18), the vertical bar are equipped on the second track (17)
(18) it is offered on regulating tank (19), and adjusting rod (20) is installed on the inside of regulating tank (19), pacified on the adjusting rod (20)
Equipped with adjusting block (21), and connecting hole (22) are reserved on adjusting block (21), the adjusting block (21) by connecting hole (22) with
Adjusting rod (20) is connected with each other, and clamping device (23) are fixed on adjusting block (21), and the telescopic leg support (24) is located at dress
Lower section with platform (1), and be connected with mounting base (25) in telescopic leg support (24), and telescopic leg support (24) passes through mounting base
(25) it is connected with each other with assembly bench (1).
2. a kind of unmanned plane dynamical system according to claim 1 is horizontally mounted debugging apparatus, it is characterised in that: described to hold
Bracket (2) be cyclic structure, and support bar (3) be incline structure, and support bar (3) the inside of support bracket (2) angularly
Distribution.
3. a kind of unmanned plane dynamical system according to claim 1 is horizontally mounted debugging apparatus, it is characterised in that: described to hold
Pressure pin (3) includes loop bar (301), support rod (302), reset spring (303) and foot pad (304), and the inside of loop bar (301) is divided
It is not provided with support rod (302) and reset spring (303), and reset spring (303) are installed on support rod (302), supports
Bar (302) is connected with each other by reset spring (303) and loop bar (301), is equipped with foot pad (304) on support rod (302).
4. a kind of unmanned plane dynamical system according to claim 3 is horizontally mounted debugging apparatus, it is characterised in that: the branch
Strut (302) constitutes stretching structure, and support rod (302) and foot pad (304) structure by reset spring (303) and loop bar (301)
At rotational structure, and foot pad (304) is rubber material.
5. a kind of unmanned plane dynamical system according to claim 1 is horizontally mounted debugging apparatus, it is characterised in that: described
Screw thread is provided on the inside of one adjusting ring (5), and first adjusts the outside that ring (5) are nested in the second adjusting ring (6), and second
Ring (6) are adjusted to be fixedly connected with the first track (8).
6. a kind of unmanned plane dynamical system according to claim 1 is horizontally mounted debugging apparatus, it is characterised in that: described
One track (8) and the second track (17) are cyclic structure, and the first track (8) and the second track (17) are connect with first respectively
Block (10) and vertical bar (18) constitute slide construction.
7. a kind of unmanned plane dynamical system according to claim 1 is horizontally mounted debugging apparatus, it is characterised in that: the dress
Number with track (12) is provided with 6, and assembles track (12) and be made up of vertical pivot (11) and the first link block (10) and rotate
Structure, and assemble the connection structure between track (12) and mounting clip (14) and the company between the second track (17) and vertical bar (18)
Binding structure is identical.
8. a kind of unmanned plane dynamical system according to claim 1 is horizontally mounted debugging apparatus, it is characterised in that: the tune
To be threadedly coupled between pole (20) and adjusting block (21), and adjusting block (21) and vertical bar (18) constitute slide construction, and adjust
Pole (20) and vertical bar (18) constitute rotational structure.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910071643.8A CN109732515B (en) | 2019-01-25 | 2019-01-25 | Horizontal installation debugging device of unmanned aerial vehicle driving system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910071643.8A CN109732515B (en) | 2019-01-25 | 2019-01-25 | Horizontal installation debugging device of unmanned aerial vehicle driving system |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN109732515A true CN109732515A (en) | 2019-05-10 |
| CN109732515B CN109732515B (en) | 2020-08-28 |
Family
ID=66366068
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201910071643.8A Expired - Fee Related CN109732515B (en) | 2019-01-25 | 2019-01-25 | Horizontal installation debugging device of unmanned aerial vehicle driving system |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN109732515B (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111361757A (en) * | 2020-03-25 | 2020-07-03 | 西京学院 | Cantilever driving system horizontal installation device for unmanned aerial vehicle |
Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102582844A (en) * | 2011-12-30 | 2012-07-18 | 衡阳泰豪通信车辆有限公司 | Fixation and protection pulley for disassembly, assembly, transhipment and vehicle-mounted transport of wings |
| CN203578665U (en) * | 2013-10-23 | 2014-05-07 | 上海航天精密机械研究所 | Novel aircraft cabin riveting and assembly jig |
| US20150040730A1 (en) * | 2013-08-09 | 2015-02-12 | Robert Shane Violett | Clevis tool with split ends |
| CN204640101U (en) * | 2015-05-05 | 2015-09-16 | 江苏逸帆航空科技有限公司 | A kind of aircraft interior trim assembling frock |
| CN105910780A (en) * | 2016-04-06 | 2016-08-31 | 重庆大学 | Accurate controllable non-contact test piece rotary magnetic field fatigue excitation and vibration test device |
| CN106005466A (en) * | 2016-07-12 | 2016-10-12 | 福建工程学院 | Demountable minitype unmanned plane launching cradle |
| CN106741902A (en) * | 2017-01-17 | 2017-05-31 | 许建芹 | A kind of anti-terror explosive removing unmanned plane |
| KR101758780B1 (en) * | 2016-05-27 | 2017-07-17 | 한국철도공사 | a Disassembly tool for a tain of motor reducer |
-
2019
- 2019-01-25 CN CN201910071643.8A patent/CN109732515B/en not_active Expired - Fee Related
Patent Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102582844A (en) * | 2011-12-30 | 2012-07-18 | 衡阳泰豪通信车辆有限公司 | Fixation and protection pulley for disassembly, assembly, transhipment and vehicle-mounted transport of wings |
| US20150040730A1 (en) * | 2013-08-09 | 2015-02-12 | Robert Shane Violett | Clevis tool with split ends |
| CN203578665U (en) * | 2013-10-23 | 2014-05-07 | 上海航天精密机械研究所 | Novel aircraft cabin riveting and assembly jig |
| CN204640101U (en) * | 2015-05-05 | 2015-09-16 | 江苏逸帆航空科技有限公司 | A kind of aircraft interior trim assembling frock |
| CN105910780A (en) * | 2016-04-06 | 2016-08-31 | 重庆大学 | Accurate controllable non-contact test piece rotary magnetic field fatigue excitation and vibration test device |
| KR101758780B1 (en) * | 2016-05-27 | 2017-07-17 | 한국철도공사 | a Disassembly tool for a tain of motor reducer |
| CN106005466A (en) * | 2016-07-12 | 2016-10-12 | 福建工程学院 | Demountable minitype unmanned plane launching cradle |
| CN106741902A (en) * | 2017-01-17 | 2017-05-31 | 许建芹 | A kind of anti-terror explosive removing unmanned plane |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111361757A (en) * | 2020-03-25 | 2020-07-03 | 西京学院 | Cantilever driving system horizontal installation device for unmanned aerial vehicle |
| CN111361757B (en) * | 2020-03-25 | 2021-10-26 | 西京学院 | Cantilever driving system horizontal installation device for unmanned aerial vehicle |
Also Published As
| Publication number | Publication date |
|---|---|
| CN109732515B (en) | 2020-08-28 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN206789681U (en) | A kind of antenna mounting device | |
| CN107826268A (en) | Multi-rotor unmanned aerial vehicle assembly platform | |
| CN209678749U (en) | Protective device is used in a kind of fertilization of draught animal artificial semenpicking | |
| CN109732515A (en) | A kind of unmanned plane dynamical system is horizontally mounted debugging apparatus | |
| CN209379317U (en) | A kind of automation dispenser system | |
| CN205150384U (en) | Quick conveyor of carton | |
| CN110375174A (en) | A kind of bracket for electronic instrument rotation | |
| CN205896592U (en) | Multi -media adjusting device is used with automatic teaching to computer | |
| CN208760913U (en) | A kind of camera fixing device for unmanned plane | |
| CN208520382U (en) | A kind of topography mapping device of UAV flight's total station | |
| CN215111939U (en) | Agricultural machinery intelligent display terminal adjusting device | |
| CN104235568A (en) | Movable type lifting three-dimensional rotating base frame | |
| CN209532338U (en) | A kind of vertical machine of H profile steel group | |
| CN205076033U (en) | Electronic foot rest folding device | |
| CN208695469U (en) | For placing the jig of sebific duct | |
| CN207678908U (en) | Work station position adjustable clothing system | |
| CN110203122A (en) | A kind of radome of fighter dismounting unwheeling | |
| CN209224019U (en) | A kind of automotive wire bundle assembling table | |
| CN204345192U (en) | A kind of movable lifting three-dimensional rotation testing jig | |
| CN211364079U (en) | Drawing device for product design | |
| CN208951548U (en) | A kind of display screen connecting bracket | |
| CN209139054U (en) | A kind of liquid crystal display substrate side point glue equipment | |
| CN208754779U (en) | A kind of planting pergola | |
| CN208333470U (en) | A kind of engineering mapping fixes device with total station | |
| CN205317551U (en) | Cement mortar swing table |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20200828 Termination date: 20210125 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |