CN205131689U - A carry platform for unmanned aerial vehicle - Google Patents
A carry platform for unmanned aerial vehicle Download PDFInfo
- Publication number
- CN205131689U CN205131689U CN201520909177.3U CN201520909177U CN205131689U CN 205131689 U CN205131689 U CN 205131689U CN 201520909177 U CN201520909177 U CN 201520909177U CN 205131689 U CN205131689 U CN 205131689U
- Authority
- CN
- China
- Prior art keywords
- carry
- center
- unmanned plane
- gravity
- adjusting part
- 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.)
- Expired - Fee Related
Links
Landscapes
- Vibration Prevention Devices (AREA)
Abstract
The utility model discloses a carry platform for unmanned aerial vehicle, include focus adjusting part and the carry subassembly that is used for the carry article, the focus adjusting part is connected with the fuselage, and carry subassembly carry is equipped with the horizontal position of a plurality of first carry portions in order to adjust the carry subassembly on the focus adjusting part on the focus adjusting part. The utility model has the advantages of simple structure lightly is suitable for unmanned aerial vehicle to use, can the quick adjustment focus satisfies different article carries, the shock attenuation is strained and is shaken effectual, the big quality carry of specially adapted.
Description
Technical field
The utility model is mainly concerned with unmanned plane field, is specifically related to a kind of carry platform for unmanned plane.
Background technology
Society, the purposes of unmanned plane is more and more wider, and unmanned plane is no longer only used for amusement by people, also utilizes unmanned plane to carry out a lot of Job Operations, as agricultural chemicals sow, make a video recording in the air, aerial broadcast, object transport, topographic mapping etc.When operating more than realizing, all need the operation article (equipment) that carry is relevant on unmanned plane, as carry medicine bucket, pick up camera, public address equipment, laser mapping equipment etc., especially when for realize some special operation need time, often need the article (equipment) of the large quality of carry on unmanned plane.
There is following technical matters in this:
(1) because the volume of each article (equipment), quality, attachment point are different, cause the center of gravity of each article self also different, if take unified position carry on unmanned plane, this will certainly cause the center of flying gravity of unmanned plane non-constant in center, directly affects stability and the safety of unmanned plane; Especially, when the article of the large quality of carry, impact is larger, even may cause time serious can not take off, danger such as falling machine of dropping in the air.
(2) unmanned plane can cause certain vibration environment in flight course, and this vibrations impact for stationarity exigent unmanned plane carry thing is very large; Especially the high-power unmanned plane of heavy－duty inherently produces larger flight vibrations, if do not carried out damping filter shake to these vibrations, the normal operation (operation is unstable as caused, fuzzy, the light shake of making a video recording, device failure etc.) of large quality carry thing will certainly be had a strong impact on.
Therefore, how to make a carry platform for unmanned plane, enable its not only simple and light be suitable for unmanned plane use and also can according to different carry thing come quick adjusting center of flying gravity, can also to unmanned plane produce vibrations carry out effective damping filter shake, make unmanned plane be applicable to different carry thing, especially can be suitable for different large quality carry things, this has become a problem demanding prompt solution.
Utility model content
The technical matters that the utility model solves is: for prior art Problems existing, provides a kind of simple and light unmanned plane that is suitable for use, quick adjustment center of gravity can meet that different article carry, damping filter shake are effective, the carry platform for unmanned plane that is specially adapted to large quality carry.
For solving the problems of the technologies described above, the utility model by the following technical solutions:
A kind of carry platform for unmanned plane, comprise center of gravity adjusting part and the carry assembly for carry article, described center of gravity adjusting part is connected with fuselage, described carry assembly carry is on center of gravity adjusting part, and described center of gravity adjusting part is provided with multiple first carry portion to regulate the level attitude of carry assembly.
As further improvement of the utility model, described center of gravity adjusting part comprises more than the one center of gravity adjust bar be arranged at bottom unmanned plane, and described carry assembly is connected with center of gravity adjust bar and can adjusts level attitude along the axial direction of center of gravity adjust bar.
As further improvement of the utility model, described carry assembly comprises the shock-absorbing support plate, elastomeric damper member and the upper carry plate that superpose successively from bottom to up, described shock-absorbing support plate is connected with center of gravity adjust bar, and described upper carry plate is carried in elastomeric damper member to be filtered out the vibrations that unmanned plane produces by elastomeric damper member.
As further improvement of the utility model, described shock-absorbing support plate is provided with several through hole, described carry assembly comprises several carry bar, and one end of several described carry bar is connected with upper carry plate, and the other end of several described carry bar passes through hole and do not contact with shock-absorbing support plate.
As further improvement of the utility model, described carry assembly comprises the lower carry plate be located at below shock-absorbing support plate, and described lower carry plate is connected to make article carry on lower carry plate with the several carry bars through through hole.
As further improvement of the utility model, described lower carry plate is provided with multiple for regulating the second carry portion of article carry position.
As further improvement of the utility model, described elastomeric damper member is the multiple elastic shock absorption balls be uniformly distributed on shock-absorbing support plate, one end of each described elastic shock absorption ball contacts with shock-absorbing support plate, and the other end of each described elastic shock absorption ball contacts with upper carry plate.
As further improvement of the utility model, described shock-absorbing support plate and upper carry plate are equipped with multiple fixed orifice portion for fixing elastic shock absorption ball.
As further improvement of the utility model, described center of gravity adjusting part also comprises multiple adjustable first attaching parts, and described carry assembly is connected with center of gravity adjusting part by multiple first attaching parts.
As further improvement of the utility model, described center of gravity adjust bar is Hollow circular beam, and described carry assembly is connected with center of gravity adjust bar by multiple first pipe clamp connecting element.
As further improvement of the utility model, described center of gravity adjusting part is also provided with multiple second attaching parts, described center of gravity adjusting part is formed by multiple second attaching parts and unmanned plane and removably connects.
Compared with prior art, the utility model has the advantage of:
(1) the carry platform for unmanned plane of the present utility model, by arranging center of gravity adjusting part and carry assembly, make carry assembly can adjust position flexibly according to different carry things, so that the center of flying gravity of unmanned plane is adjusted to optimum regime, realize the flight usefulness that unmanned plane is splendid, enable steady, safe the taking off and operation of unmanned plane, finally make unmanned plane can the different carry thing of carry, meet multiple different job requirements, the range of use of unmanned plane is wider.
(2) the carry platform for unmanned plane of the present utility model, carry assembly not only realizes the function of carry, also by design shock-absorbing support plate, elastomeric damper member etc., carry assembly is enable to filter out the vibrations of unmanned plane generation, ensure that the vibration environment that unmanned plane causes can not impact carry thing, effectively ensure that the stationarity of carry thing, achieve good flight job requirements.
(3) the carry platform for unmanned plane of the present utility model, is provided with multiple second carry portion further on the lower carry plate of carry assembly, can realize the fine setting of center of flying gravity by adjusting different carry positions.The centre of gravity adjustment mode of lower carry plate and the centre of gravity adjustment mode of center of gravity adjusting part match, and this dual regulation design can realize the center of flying gravity adjustment of different carry thing more accurately, easily.
(4) the carry platform for unmanned plane of the present utility model, simple and light, is convenient to the use of unmanned plane.And can dismantle flexibly, be convenient to install and carry.The particular design of this series of science that multiple spot especially of the present utility model is fixedly connected with, the even formula of flat overlaying structure, shock-absorbing ball distributes, makes this carry platform can ensure stable, the safe carry of large quality carry thing.
Accompanying drawing explanation
Fig. 1 is the structural principle schematic diagram of the unmanned plane applying the utility model carry platform.
Fig. 2 is the perspective exploded view of the unmanned plane applying the utility model carry platform.
Fig. 3 is the spatial structure principle schematic of the utility model for the carry platform of unmanned plane.
Fig. 4 is the structural principle schematic diagram of the utility model for the carry assembly of the carry platform of unmanned plane.
Marginal data:
1, center of gravity adjusting part; 11, center of gravity adjust bar; 12, the first attaching parts; 13, the second attaching parts; 2, carry assembly; 21, shock-absorbing support plate; 211, through hole; 22, elastomeric damper member; 23, upper carry plate; 24, carry bar; 25, lower carry plate.
Detailed description of the invention
Below in conjunction with specific embodiments and the drawings, the utility model is described in further detail.
As shown in Figures 1 to 4, the utility model provides a kind of carry platform for unmanned plane, comprise center of gravity adjusting part 1 and the carry assembly 2 for carry article, center of gravity adjusting part 1 is connected with fuselage, carry assembly 2 carry is on center of gravity adjusting part 1, and center of gravity adjusting part 1 is provided with multiple first carry portion to regulate the level attitude of carry assembly 2.
When different carry thing (especially large quality carry thing) carries is on carry assembly 2, because the volume of each carry thing, quality, attachment point are different, cause the center of gravity of each carry thing self also different, as being directly connected with unmanned plane by carry assembly 2, the center of flying gravity of unmanned plane will certainly be caused unstable.For this technical matters, the utility model is provided with the center of gravity adjusting part 1 be connected with fuselage, and center of gravity adjusting part 1 is provided with multiple first carry portion.Operating personal can according to the center of gravity situation of different carry thing, the level attitude of rational flexible carry assembly 2 that carry assembly 2 carry is come up in the first different carry portions, until the center of flying gravity of unmanned plane is adjusted to optimum regime, enable steady, safe the taking off and operation of unmanned plane.
Such particular design, makes certain fixed position being fixed on unmanned plane that carry assembly 2 is no longer single, but can adjust the center of flying gravity of unmanned plane flexibly according to different large quality carry things, to realize the splendid flight usefulness of unmanned plane.Finally make unmanned plane can the different large quality carry thing of carry, can meet multiple different job requirements, the range of use of unmanned plane be wider.
As shown in Figure 3, further, in the preferred embodiment, center of gravity adjusting part 1 comprises more than the one center of gravity adjust bar 11 be arranged at bottom unmanned plane, carry assembly 2 is connected with center of gravity adjust bar 11 and can adjusts level attitude along the axial direction of center of gravity adjust bar 11, and namely carry assembly 2 axially can realize the carry of multiple diverse location at whole center of gravity adjust bar 11.In the present embodiment, center of gravity adjust bar 11 is two, and be parallel to each other be horizontally placed on bottom unmanned plane, carry assembly 2 is connected with two center of gravity adjusts bar 11 respectively and axially can adjusts level attitude along center of gravity adjust bar 11.In the present embodiment, center of gravity adjust bar 11 designs for Hollow circular beam, and carry assembly 2 is connected with two center of gravity adjusts bar 11 by four the first pipe clamp fixed blocks.In other embodiments, center of gravity adjust bar 11 also can design for special pipe, and attaching parts is designed to other attaching partss of corresponding cooperation too.Center of gravity adjust bar 11 structure is simple, light, the use of very applicable unmanned plane; And carry assembly 2 along center of gravity adjust bar 11 slide axially regulate center of gravity regulative mode also simple to operate, time saving and energy saving.
It should be noted that, under the technology of said structure and embodiment inspires, those of ordinary skill in the art can also expect form center of gravity adjusting part 1 being set to other easily, as arranged a centre of gravity adjustment plate in the bottom of fuselage, multiple first carry portion is multiple hooks that centre of gravity adjustment plate is arranged, and carry assembly 2 is by linking up with carry on center of gravity regulating plate.When needs adjustment center of gravity time, can by carry assembly 2 carry on different hooks to regulate the level attitude of carry assembly 2, until the center of flying gravity of unmanned plane is adjusted to optimum regime.Certainly, the center of gravity adjust bar 11 of fuselage bottom can also being set to other forms, as being set to cross by two center of gravity adjusts bar 11, making carry assembly 2 can realize the adjustment of four direction all around; As center of gravity adjust bar 11 being set to circular or multiple circular concentric, to realize the adjustment of multiple dimensions of carry assembly 2.
Therefore under the inspiration of the said structure of the present embodiment, as long as arrange multiple first carry portion, reached the technique effect of the center of flying gravity of adjustment unmanned plane by the horizontal carry position of adjustment carry assembly 2, all should belong to protection domain of the present utility model.
As shown in Figure 3 and Figure 4, further, in the preferred embodiment, carry assembly 2 comprises the shock-absorbing support plate 21, elastomeric damper member 22 and the upper carry plate 23 that superpose successively from bottom to up, shock-absorbing support plate 21 is connected with center of gravity adjust bar 11, and upper carry plate 23 is carried in elastomeric damper member 22 to be filtered out the vibrations that unmanned plane produces by elastomeric damper member 22.When unmanned plane creates strong motion in flight course, vibrations can first be conducted to the shock-absorbing support plate 21 be attached thereto, conduct to the elastomeric damper member 22 be located on shock-absorbing support plate 21 again, elastomeric damper member 22 is owing to having elastic shock attenuation ability, therefore, it is possible to well filter out the vibrations of unmanned plane generation, make vibrations can not conduct to the upper carry plate 23 be carried in elastomeric damper member 22 again, the vibrations that unmanned plane is produced can not to the raw vibration influence of carry produce, realize between carry thing and unmanned plane flexibly connecting, well meet the flight job requirements of carry thing.
Further, in the preferred embodiment, shock-absorbing support plate 21 is provided with several through hole 211, and carry assembly 2 comprises several carry bar 24, one end of several carry bar 24 is connected with upper carry plate 23, and the other end of several carry bar 24 passes through hole 211 and do not contact with shock-absorbing support plate 21.Several carry bar 24 can carry out fixedly contacting of multiple point with carry thing, and fixed effect is better, flies safer.And because shock-absorbing support plate 21 can not come in contact with carry bar 24, also can not by vibrations conduction to carry bar 24 when shock-absorbing support plate 21 is shaken, further ensure the vibration environment that unmanned plane causes thus to impact carry thing, effectively ensure that the stationarity of carry thing.
As shown in Figure 3 and Figure 4, further, in the preferred embodiment, carry assembly 2 comprises the lower carry plate 25 be located at below shock-absorbing support plate 21, lower carry plate 25 is connected to make article carry on lower carry plate 25 with the several carry bars 24 through through hole 211, and lower carry plate 25 is provided with multiple for regulating the second carry portion of article carry position.Such particular design has three advantages: one is by arranging lower carry plate 25, make article can with realize face between lower carry plate 25 and contact, fixing, flattening effect is better.Two is because lower carry plate 25 is provided with multiple the second carry portion for carry article, when needs adjustment center of gravity, also can realize the fine setting of center of flying gravity by adjusting different carry positions.The centre of gravity adjustment mode of lower carry plate 25 and the centre of gravity adjustment mode of center of gravity adjusting part 1 match, and this dual regulation design can realize the center of flying gravity adjustment of different heavy－duty more accurately, easily.
Further, in the preferred embodiment, elastomeric damper member 22 is for being uniformly distributed in the multiple elastic shock absorption balls on shock-absorbing support plate 21, shock-absorbing support plate 21 and upper carry plate 23 are equipped with multiple fixed orifice portion for fixing elastic shock absorption ball, one end of each elastic shock absorption ball contacts with shock-absorbing support plate 21, and the other end of each elastic shock absorption ball contacts with upper carry plate 23.By the particular design of upper carry plate 23, shock-absorbing support plate 21, this flat superposition of lower carry plate 25, one is that actv. ensure that multiple elastic shock absorption ball can maintain in one plane, and the Distributed Design of flat board can increase the distribution area of multiple elastic shock absorption ball, make stressed more even, reach best damping filter shake effect.Two is particular design of this flat superposition, can ensure the integral rigidity of whole carry assembly 2 further, can ensure stable, the safe carry of large quality carry thing.
It should be noted that; under the technology of said structure and embodiment inspires; those of ordinary skill in the art can also expect elastomeric damper member 22 to take other mode to arrange easily; as adopted sponge kind elasticity thing, the caoutchouc elasticity thing of monoblock; or adopt spring or other elastic components of multiple distribution; all can reach the technique effect of damping filter shake, all should belong to protection domain of the present utility model.
Further, in the preferred embodiment, center of gravity adjusting part 1 also comprises multiple adjustable first attaching parts 12, and carry assembly 2 is connected with center of gravity adjusting part 1 by multiple first attaching parts 12.In the present embodiment, center of gravity adjust bar 11 is Hollow circular beam, and carry assembly 2 is connected with center of gravity adjust bar 11 by multiple first pipe clamp connecting element.Hollow circular beam weight is gentlier more suitable for unmanned plane and uses, and round bar adds the bearing fit design of pipe clamp connecting element simultaneously, makes it possible to fast and carries out center of gravity adjustment easily.The corner that four the first pipe clamp connecting elements are successively set on shock-absorbing support plate 21 is connected with center of gravity adjust bar 11, makes whole carry assembly 2 held stationary.
Further, in the preferred embodiment, center of gravity adjusting part 1 is also provided with multiple second attaching parts 13, center of gravity adjusting part 1 is formed by multiple second attaching parts 13 and unmanned plane and removably connects.In the present embodiment, second attaching parts 13 is the second pipe clamp connecting element, every root center of gravity adjust bar 11 is all formed by three the second pipe clamp connecting elements and unmanned plane and removably connects, and it is more stable that this makes carry platform be connected with unmanned plane, can be applicable to the carry of large quality article.When not needing carry, by dismounting second pipe clamp connecting element, whole carry platform can be pulled down from unmanned plane, being convenient to carrying out of other working flights of unmanned plane; Meanwhile, opening of the second pipe clamp connecting element is unloaded connection mode and is also made this carry platform can realize Fast Installation and being easy to carry.
Below be only preferred implementation of the present utility model, protection domain of the present utility model be not only confined to above-described embodiment, all technical schemes belonged under the utility model thinking all belong to protection domain of the present utility model.It should be pointed out that for those skilled in the art, not departing from the some improvements and modifications under the utility model principle prerequisite, protection domain of the present utility model should be considered as.
Claims (11)
1. the carry platform for unmanned plane, it is characterized in that, comprise center of gravity adjusting part (1) and the carry assembly (2) for carry article, described center of gravity adjusting part (1) is connected with fuselage, described carry assembly (2) carry is on center of gravity adjusting part (1), and described center of gravity adjusting part (1) is provided with multiple first carry portion to regulate the level attitude of carry assembly (2).
2. the carry platform for unmanned plane according to claim 1, it is characterized in that, described center of gravity adjusting part (1) comprises more than the one center of gravity adjust bar (11) be arranged at bottom unmanned plane, and described carry assembly (2) is connected with center of gravity adjust bar (11) and can adjusts level attitude along the axial direction of center of gravity adjust bar (11).
3. the carry platform for unmanned plane according to claim 1, it is characterized in that, described carry assembly (2) comprises the shock-absorbing support plate (21), elastomeric damper member (22) and the upper carry plate (23) that superpose successively from bottom to up, described shock-absorbing support plate (21) is connected with center of gravity adjust bar (11), and described upper carry plate (23) is carried in elastomeric damper member (22) to be filtered out the vibrations that unmanned plane produces by elastomeric damper member (22).
4. the carry platform for unmanned plane according to claim 3, it is characterized in that, described shock-absorbing support plate (21) is provided with several through hole (211), described carry assembly (2) comprises several carry bar (24), one end of several described carry bar (24) is connected with upper carry plate (23), and the other end of several described carry bar (24) passes through hole (211) and do not contact with shock-absorbing support plate (21).
5. the carry platform for unmanned plane according to claim 4, it is characterized in that, described carry assembly (2) comprises the lower carry plate (25) being located at shock-absorbing support plate (21) below, and described lower carry plate (25) is connected to make article carry on lower carry plate (25) with the several carry bars (24) through through hole (211).
6. the carry platform for unmanned plane according to claim 5, is characterized in that, described lower carry plate (25) is provided with multiple for regulating the second carry portion of article carry position.
7. according to the carry platform for unmanned plane in claim 3 ~ 6 described in any one, it is characterized in that, described elastomeric damper member (22) is for being uniformly distributed in the multiple elastic shock absorption balls on shock-absorbing support plate (21), one end of each described elastic shock absorption ball contacts with shock-absorbing support plate (21), and the other end of each described elastic shock absorption ball contacts with upper carry plate (23).
8. the carry platform for unmanned plane according to claim 7, is characterized in that, described shock-absorbing support plate (21) and upper carry plate (23) are equipped with multiple fixed orifice portion for fixing elastic shock absorption ball.
9. according to the carry platform for unmanned plane in claim 1 ~ 6 described in any one, it is characterized in that, described center of gravity adjusting part (1) also comprises multiple adjustable first attaching parts (12), and described carry assembly (2) is connected with center of gravity adjusting part (1) by multiple first attaching parts (12).
10. according to the carry platform for unmanned plane in claim 2 ~ 6 described in any one, it is characterized in that, described center of gravity adjust bar (11) is Hollow circular beam, and described carry assembly (2) is connected with center of gravity adjust bar (11) by multiple first pipe clamp connecting element.
11. according to the carry platform for unmanned plane in claim 1 ~ 6 described in any one, it is characterized in that, described center of gravity adjusting part (1) is also provided with multiple second attaching parts (13), and described center of gravity adjusting part (1) is formed by multiple second attaching parts (13) and unmanned plane and removably connects.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520909177.3U CN205131689U (en) | 2015-11-16 | 2015-11-16 | A carry platform for unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520909177.3U CN205131689U (en) | 2015-11-16 | 2015-11-16 | A carry platform for unmanned aerial vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205131689U true CN205131689U (en) | 2016-04-06 |
Family
ID=55617506
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201520909177.3U Expired - Fee Related CN205131689U (en) | 2015-11-16 | 2015-11-16 | A carry platform for unmanned aerial vehicle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205131689U (en) |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105270644A (en) * | 2015-11-16 | 2016-01-27 | 湖南云顶智能科技有限公司 | Mounting platform of unmanned airplane |
| CN106114814A (en) * | 2016-07-22 | 2016-11-16 | 四川克瑞斯航空科技有限公司 | A kind of many rotor wing unmanned aerial vehicles |
| CN109018393A (en) * | 2018-06-28 | 2018-12-18 | 山东建筑大学 | A kind of photogrammetric mounting platform of adjustable unmanned plane |
| WO2019071602A1 (en) * | 2017-10-13 | 2019-04-18 | Powervision Tech Inc. | Holding device with multiple mounting functions and unmanned aerial system therewith |
| WO2020253622A1 (en) * | 2019-06-18 | 2020-12-24 | 深圳高度创新技术有限公司 | Fire-fighting and disaster relief unmanned aerial vehicle |
-
2015
- 2015-11-16 CN CN201520909177.3U patent/CN205131689U/en not_active Expired - Fee Related
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105270644A (en) * | 2015-11-16 | 2016-01-27 | 湖南云顶智能科技有限公司 | Mounting platform of unmanned airplane |
| CN106114814A (en) * | 2016-07-22 | 2016-11-16 | 四川克瑞斯航空科技有限公司 | A kind of many rotor wing unmanned aerial vehicles |
| WO2019071602A1 (en) * | 2017-10-13 | 2019-04-18 | Powervision Tech Inc. | Holding device with multiple mounting functions and unmanned aerial system therewith |
| CN109018393A (en) * | 2018-06-28 | 2018-12-18 | 山东建筑大学 | A kind of photogrammetric mounting platform of adjustable unmanned plane |
| WO2020253622A1 (en) * | 2019-06-18 | 2020-12-24 | 深圳高度创新技术有限公司 | Fire-fighting and disaster relief unmanned aerial vehicle |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN105270644A (en) | Mounting platform of unmanned airplane | |
| CN205131689U (en) | A carry platform for unmanned aerial vehicle | |
| CN206476124U (en) | Head assembly and frame | |
| CN205150253U (en) | Novel helicopter joins externally pesticide spraying machine | |
| CN211107962U (en) | Mounting bracket for surveying and mapping unmanned aerial vehicle | |
| CN110979643A (en) | Landing gear and unmanned aerial vehicle | |
| CN110896631A (en) | Cloud platform shock-absorbing structure, cloud platform system and unmanned vehicles | |
| CN211336423U (en) | Unmanned aerial vehicle protection casing and take unmanned aerial vehicle of protection casing | |
| CN211167409U (en) | Anti-falling plant protection unmanned aerial vehicle | |
| CN213200087U (en) | Carbon fiber unmanned machine shell | |
| CN216546682U (en) | Unmanned aerial vehicle for collecting plant samples | |
| CN207191459U (en) | The multi-degree of freedom vibration reduction system and unmanned plane of unmanned plane flying control equipment | |
| CN207826532U (en) | A kind of power-line patrolling unmanned plane undercarriage | |
| CN108891584A (en) | A kind of stable unmanned plane that lands | |
| CN205150252U (en) | Aircraft explosive box for pesticide applying of preventing jolting | |
| CN213443093U (en) | Bird-driving unmanned aerial vehicle | |
| CN210592470U (en) | Pod damping mechanism | |
| CN207631477U (en) | A kind of support plate applied to unmanned plane | |
| CN110466791A (en) | Gondola damping | |
| CN211196604U (en) | Unmanned aerial vehicle stabilizer blade structure | |
| CN218704019U (en) | Unmanned aerial vehicle buffering undercarriage | |
| CN207283824U (en) | Airborne Emer-gency Communication | |
| CN211059607U (en) | Target drone avionics system shock absorption and fixing device | |
| CN211167437U (en) | Unmanned aerial vehicle oil tank arrangement mechanism | |
| CN214325398U (en) | Portable pesticide sprays unmanned aerial vehicle platform that rises and falls |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20160406 Termination date: 20211116 |