CN205131696U - A cloud platform device for unmanned aerial vehicle - Google Patents
A cloud platform device for unmanned aerial vehicle Download PDFInfo
- Publication number
- CN205131696U CN205131696U CN201520909254.5U CN201520909254U CN205131696U CN 205131696 U CN205131696 U CN 205131696U CN 201520909254 U CN201520909254 U CN 201520909254U CN 205131696 U CN205131696 U CN 205131696U
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- CN
- China
- Prior art keywords
- unmanned plane
- mount pad
- slide rail
- roll axle
- bayonet lock
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Abstract
The utility model discloses a cloud platform device for unmanned aerial vehicle, including cloud platform mount pad and the device installation assembly that links to each other, cloud platform mount pad includes mounting platform and slide rail formula coupling mechanism, slide rail formula coupling mechanism including connect in above slide rail of unmanned aerial vehicle bottom with install the spout on the mounting platform, when cloud platform mount pad linked to each other with the unmanned aerial vehicle bottom, the slide rail cover was located and is accomplished the connection in the spout and cooperate. The utility model has the advantages of simple structure compactness, simple operation, long service life, can realize quick installation and demolish, can adjust the focus again.
Description
Technical field
The utility model is mainly concerned with unmanned plane field, is specifically related to a kind of cradle head device for unmanned plane.
Background technology
Along with the rapid rising of unmanned plane, unmanned plane is widely used at military, police and civil area, such as mapping, investigation, electric inspection process, fire-fighting etc., but in these fields often through the various airborne equipment of lift-launch (mostly being various picture pick-up device), to obtain specific environmental information to realize.Connection between existing aircraft The Cloud Terrace and aircraft comprises and to be mechanically connected and electric wiring connects, and mechanical connection is generally detouchable fixed sturcture, carries demand in order to the difference meeting client.
There is following technical matters in existing cradle head device:
(1) existing The Cloud Terrace major part adopts screw locking mode to fix, and not only need to carry the instruments such as screwdriver at random, and loaded down with trivial details dismounting operation also has certain requirement to human users's gimmick during dismounting, and theoretical " quick detach connection " function is difficult to realize actually.In addition, because demolition, installation The Cloud Terrace needs repeatedly to lock screw, the dynamics that in addition manually locks is uncontrollable, and after repeatedly converting The Cloud Terrace operation, screw holds easy to slip teeth or is difficult to take out, thus makes troubles to client's routine use, even there is the risk that The Cloud Terrace is scrapped.Meanwhile, this mounting means comparatively bothers, length consuming time, is also unfavorable for that unmanned plane performs shooting task fast.
(2) existing clouds terrace system mostly is specificity design and cannot allocates center of gravity, and full the output by motor of The Cloud Terrace balance controls, and often causes that motor load is excessive and torsion surplus capacity is limited, causes The Cloud Terrace shake in-flight.
Utility model content
The technical matters that the utility model solves is: for prior art Problems existing, a kind of simple and compact for structure, simple operation, long service life are provided, can realize Fast Installation remove, again can the cradle head device for unmanned plane of center-of-gravity regulating.
For solving the problems of the technologies described above, the utility model by the following technical solutions:
A kind of cradle head device for unmanned plane, comprise connected The Cloud Terrace mount pad and device installation assembly, described The Cloud Terrace mount pad comprises erecting stage and slide rail type bindiny mechanism, described slide rail type bindiny mechanism comprises one or more slide rail be connected to bottom unmanned plane and the chute be installed on erecting stage, at described The Cloud Terrace mount pad with when being connected bottom unmanned plane, described slide rail is sheathed in chute to complete to connect and coordinates.
Further, in the preferred embodiment, described chute comprises grab parts more than two, and many group grab parts arrange the passage being formed and coordinate with slide rail successively, often organize grab parts and include two in grab positioned opposite.
Further, in the preferred embodiment, the extreme position of moving at described slide rail is provided with stopper section, and described stopper section is arranged on chute or slide rail.
Further, in the preferred embodiment, also comprise the locking member be installed on erecting stage, described locking member comprises bayonet lock, bayonet lock mount pad and spring assembly, described bayonet lock and spring assembly are installed in bayonet lock mount pad, and the lower end of described bayonet lock coordinates with spring assembly; Under the effect of spring assembly, described bayonet lock keeps up jack-up state, when described slide rail need to slip into chute coordinate time, described bayonet lock pressure to bounce back in bayonet lock mount pad and compression spring assembly.
Further, in the preferred embodiment, described spring assembly is at least one group, and often organize spring assembly and include registration mast and spring, described registration mast is fixed on erecting stage, and described spring is fixed by described registration mast.
Further, in the preferred embodiment, described bayonet lock is provided with non-slip operation portion towards the one side of operator.
Further, in the preferred embodiment, be detachably install between described bayonet lock mount pad and erecting stage; The bottom of described bayonet lock mount pad outer wall arranges a clamp button of the spring, described erecting stage is provided with the draw-in groove coordinated with clamp button of the spring.
Further, in the preferred embodiment, described device installation assembly comprises roll axle and pitch axis, one end of described pitch axis is used for being connected with device to be installed, the other end of described pitch axis is connected by the lower end of the second motor with roll axle, and the upper end of described roll axle is connected with described The Cloud Terrace mount pad.
Further, in the preferred embodiment, be connected by the first attaching parts between described pitch axis with the second motor, described second motor is fixed on roll axle, described first attaching parts is directly fixed on the second motor, described first attaching parts is provided with boss, one end that described pitch axis is connected with the first attaching parts offers groove, described boss is sheathed in groove and coordinates to complete slip.
Further, in the preferred embodiment, described roll axle is provided with roll axle protecgulum, described roll axle protecgulum offers the groove for installation second motor.
Further, in the preferred embodiment, described roll axle is connected with the 3rd motor by the second attaching parts, and described 3rd motor is fixed on The Cloud Terrace mount pad by attaching parts; The two side walls of described roll axle and roll axle protecgulum all offers the through hole for the second attaching parts parallel sliding, to make described roll axle can relative second attaching parts parallel sliding with roll axle protecgulum.
Compared with prior art, the utility model has the advantage of:
(1) cradle head device for unmanned plane of the present utility model, by being designed with the slide rail and chute that match, operating personal only need promote The Cloud Terrace mount pad gently, just cradle head device can be arranged on fast, easily (or being got off from quick-detachment unmanned plane by cradle head device) on unmanned plane, whole process is very quick, greatly save the time and efforts of operating personal, really reached the requirement of " quick detach connection ", be convenient to unmanned plane and be correlated with carrying out fast of operation.Meanwhile, owing to not needing to lock screw in the process of " quick detach connection ", also there will not be the situation of the sliding tooth of screw, not to causing the risk that tripod head equipment damages, tripod head equipment drops, tripod head equipment increases service life greatly.
(2) cradle head device for unmanned plane of the present utility model, erecting stage is also provided with locking member, make fixing after the The Cloud Terrace parts that are locked pin, prevent The Cloud Terrace mount pad reversing sense from sliding, further ensure that reliable, the secure connection of tripod head equipment.
(3) cradle head device for unmanned plane of the present utility model, device installation assembly is provided with the first attaching parts and the second attaching parts that can be used for center-of-gravity regulating, by this scientific design, part can be disassembled after cradle head device of the present utility model is installed, twice gravity balance can be completed to device, finally realize accurate leveling; By twice allotment center of gravity, each motor load on device installation assembly can be reduced to greatest extent, ensure the stability of The Cloud Terrace.
Accompanying drawing explanation
Fig. 1 is the decomposition texture principle schematic of the utility model for the cradle head device of unmanned plane.
Fig. 2 is the spatial structure principle schematic of the utility model for the cradle head device of unmanned plane.
Fig. 3 is the spatial structure principle schematic of the utility model for the pitch axis of the cradle head device of unmanned plane.
Fig. 4 is the spatial structure principle schematic of the utility model for the roll axle of the cradle head device of unmanned plane.
Fig. 5 is that the utility model is greatly for the structural principle schematic diagram of the locking member of the cradle head device of unmanned plane.
Marginal data:
1, The Cloud Terrace mount pad; 10, the first attaching parts; 101, boss; 11, the second attaching parts; 18, bayonet lock mount pad; 181, clamp button of the spring; 19, bayonet lock; 192, non-slip operation portion; 2, roll axle; 201, through hole; 21, spring; 22, registration mast; 3, roll axle protecgulum; 4, pitch axis; 401, groove; 51, slide rail; 52, chute; 53, grab; 54, stopper section; 6, the second motor; 7, the 3rd motor; 8, camera; 9, radiating gill.
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 5, the utility model provides a kind of cradle head device for unmanned plane, comprise connected The Cloud Terrace mount pad 1 and device installation assembly, device installation assembly is used for installing the various device needing carry on unmanned plane, as camera 8, The Cloud Terrace mount pad 1 comprises erecting stage and slide rail 51 formula bindiny mechanism, slide rail 51 formula bindiny mechanism comprises one or more slide rail 51 be connected to bottom unmanned plane and the chute 52 be installed on erecting stage, at The Cloud Terrace mount pad 1 with when being connected bottom unmanned plane, slide rail 51 is sheathed in chute 52 to complete to connect and coordinates.
When needs install related device (as camera 8) on unmanned plane, first device is fixed on the device installation assembly be connected with The Cloud Terrace mount pad 1, then the chute 52 on the erecting stage of The Cloud Terrace mount pad 1 is aimed at the slide rail 51 be fixed on bottom unmanned plane, then promoting erecting stage makes chute 52 move to slide rail 51, slide rail 51 is finally made to be sheathed in chute 52, slide rail 51 is formed with both chutes 52 and is connected cooperation, and The Cloud Terrace mount pad 1 is firmly fixed on bottom unmanned plane.Certainly, also first The Cloud Terrace mount pad 1 can be fixed on bottom unmanned plane, and then related device be fixed on the device installation assembly that is connected with The Cloud Terrace mount pad 1.When needs remove The Cloud Terrace or equipment, in like manner continue to promote erecting stage, finally make slide rail 51 and chute 52 depart from, do not come in contact between the two, and then The Cloud Terrace or the The Cloud Terrace that is provided with equipment are taken off from unmanned plane.
By design special above, the connection of slide rail 51 and chute 52 is utilized to coordinate, operating personal only need promote The Cloud Terrace mount pad 1 gently, just cradle head device can be arranged on fast, easily (or being got off from quick-detachment unmanned plane by cradle head device) on unmanned plane, whole process is very quick, do not need to go to lock screw one by one as existing installation, greatly save the time and efforts of operating personal, really reach the requirement of " quick detach connection ", be convenient to unmanned plane and be correlated with carrying out fast of operation.Meanwhile, owing to not needing to lock screw in the process of " quick detach connection ", also there will not be the situation of the sliding tooth of screw, not to causing the risk that tripod head equipment damages, tripod head equipment drops, tripod head equipment increases service life greatly.
As shown in Figure 2, further, in the preferred embodiment, chute 52 comprises grab parts more than two, and many group grab parts arrange the passage being formed and coordinate with slide rail 51 successively, often organize grab parts and include two in grab 53 positioned opposite.The erecting stage of The Cloud Terrace mount pad 1 is provided with two groups of grab parts, often organize between two of grab parts grab 53 positioned opposite and form chute 52 passage, when operating personal by chute 52 channel alignment slide rail 51 and promote The Cloud Terrace mount pad 1 slide time, slide rail 51 finally can slip in chute 52 passage, the now top crook carrying of grab 53 is fixed on slide rail 51 and forms cooperation, The Cloud Terrace mount pad 1 is draped be fixed on slide rail 51, namely cradle head device is fixedly connected with unmanned plane.
It should be noted that, grab parts just form the concrete mode of one of chute 52 in the present embodiment, under the technology of said structure and embodiment inspires, those of ordinary skill in the art can also expect concrete form slide rail 51 and chute 52 being set to other easily, as slide rail 51 is set to the slide bar that cross-sectional plane is upside down t-shape, chute 52 is set to the pipeline of top with opening, during installation, the cross bar portion, lower end of the slide bar of inverted T-shaped slips in pipeline, slide bar is formed with both chutes 52 and is connected cooperation, also the technique effect being slides quickly into be connected and fixed can be reached.
Therefore under the inspiration of the said structure of the present embodiment; as long as by arranging the sliding block joint mechanism matched respectively on cradle head device and unmanned plane; make cradle head device to be slidably mounted on unmanned plane fast, easily by sliding block joint mechanism, all should belong to protection domain of the present utility model.
As shown in Figure 2, further, in the preferred embodiment, the extreme position of moving at slide rail 51 is provided with stopper section 54, and stopper section 54 is arranged on chute 52 or slide rail 51.In the present embodiment, as shown in Figure 2, stopper section 54 is arranged on slide rail 51, a step sliding surface is equipped with at the two ends of slide rail 51, be provided with a stopper section 54 of protruding in one end of step sliding surface, when slipping into from left to right during The Cloud Terrace mount pad 1 is as figure, slide rail 51 finally can slip in chute 52 passage of grab parts formation left, when the top crook of grab 53 contacts with the stopper section 54 of protrusion, The Cloud Terrace mount pad 1 is limited by protrusion stopper section 54 and can not continue to move right.In other embodiments, stopper section 54 also can be arranged in chute 52, as protruded the side being arranged on grab 53.
As shown in Figure 2 and Figure 5, further, in the preferred embodiment, also comprise the locking member be installed on erecting stage, locking member comprises bayonet lock 19, bayonet lock mount pad 18 and spring assembly, and bayonet lock 19 and spring assembly are installed in bayonet lock mount pad 18, and spring assembly comprises registration mast 22 and spring 21, registration mast 22 is fixed on erecting stage, and spring 21 is fixed by registration mast 22.The lower end of bayonet lock 19 coordinates with spring 21, and under the action of the spring 21, and bayonet lock 19 keeps up jack-up state.When installing cradle head device, The Cloud Terrace mount pad 1 upper surface being against unmanned aerial vehicle body, coordinates direction to slide along slide rail 51, chute 52, now bayonet lock 19 certainly will be depressed and bounce back in bayonet lock mount pad 18 and compression spring assembly.In the present embodiment, the bayonet socket coordinated with bayonet lock 19 is provided with bottom unmanned plane, when slide rail 51 slips in chute 52 passage, bayonet lock 19 is just in time in below bayonet socket, bayonet lock 19 upwards jack-up insert in bayonet socket under the action of the spring 21, The Cloud Terrace mount pad 1 is fixed pinning, prevents The Cloud Terrace mount pad 1 from sliding toward reversing sense.
Further, in the preferred embodiment, bayonet lock mount pad 18 is installed on the end of erecting stage, and be positioned on the sliding trace of slide rail 51 formula bindiny mechanism, the bottom of bayonet lock mount pad 18 outer wall arranges a clamp button of the spring 181, erecting stage is provided with the draw-in groove coordinated with clamp button of the spring 181, by above design, to make between bayonet lock mount pad 18 and erecting stage, for detachably to install, to be convenient to maintenance and the replacing of locking member.The sidewall of bayonet lock mount pad 18 is provided with the notch part for operating personal operation bayonet lock 19, and the bayonet lock 19 being positioned at notch part is provided with non-slip operation portion 192 in the one side of operator.When The Cloud Terrace mount pad 1 pulled down by needs, operating personal first promotes non-slip operation portion 192 and moves downward, bayonet lock 19 is moved downward and no longer withstands in the bayonet socket bottom unmanned plane, now, oppositely promote The Cloud Terrace mount pad 1 again, slide rail 51 is skidded off in chute 52 passage, finally makes cradle head device and unmanned plane depart from.
As shown in Figures 1 to 5, further, in the preferred embodiment, device installation assembly comprises roll axle 2 and pitch axis 4, the upper end of roll axle 2 is connected with The Cloud Terrace mount pad 1, one end of pitch axis 4 is used for being connected with device (as camera 8), and the other end of pitch axis 4 is connected with the lower end of roll axle 2 by the second motor 6, and pitch axis 4 under the driving of the second motor 6, drive device (as camera 8) luffing so that relevant operation is carried out.
As shown in Figure 3, in the present embodiment, be connected by the first attaching parts 10 between pitch axis 4 with the second motor 6, the second motor 6 is fixed on roll axle 2, and the first attaching parts 10 is directly fixed on the second motor 6.First attaching parts 10 is provided with boss 101, one end that pitch axis 4 is connected with the first attaching parts 10 offers groove 401, boss 101 is sheathed in groove 401 and coordinates to complete slip, namely the first attaching parts 10 horizontally slips in groove 401 by boss 101, thus change the center-of-gravity position being provided with the pitch axis 4 of device (as camera 8), reach the object regulating counterweight, reduce horizontal stage electric machine self-balancing workload.Be provided with on pitch axis 4 fixed orifice coordinated at the first attaching parts 10, by fixed orifice and screw, the first attaching parts 10 fixed with pitch axis 4 after regulating center of gravity.Meanwhile, boss 101 and groove 401 coordinate exportable torsion, reduce check screw radial force, improve the service life of equipment.In the present embodiment, outside near installing device place on pitch axis 4 is provided with radiating gill 9, when unmanned plane carries device (as camera 8) in high-altitude flight by tripod head equipment, directly can take away the heat in the first motor 5 and device (as camera 8) by circulating air, ensure that the first motor 5 and device (as camera 8) can stable operations.Meanwhile, in the present embodiment, roll axle 2 is provided with roll axle protecgulum 3, roll axle protecgulum 3 offers the groove for installation second motor 6.
As shown in Figure 1 and Figure 4, further, in the preferred embodiment, roll axle 2 is connected with the 3rd motor 7 by the second attaching parts 11, and the 3rd motor 7 is fixed on The Cloud Terrace mount pad 1 by attaching parts, and roll axle 2 makes horizontal revolving motion under the 3rd motor 7 drives.In the two side walls of roll axle 2 and roll axle protecgulum 3, through hole 201, second attaching parts 11 two sides all offered for the second attaching parts 11 parallel sliding are screwed in the through hole 201 of roll axle 2 and roll axle protecgulum 3.When needs center-of-gravity regulating, first can unscrew screw, to make roll axle 2 second attaching parts 11 parallel sliding relative to roll axle protecgulum 3, tighten the screws again after regulating center of gravity, thus realize device (as camera 8) and move relative to the center-of-gravity position of the 3rd motor 7, thus realize the object of allotment center of gravity.
By above-mentioned special scientific design, make device (as camera 8) along with the slip of roll axle 2 thus realize mobile for the first time, complete first time gravity balance, then device (as camera 8) passes through the slip of pitch axis 4 again thus realizes mobile for the second time, complete second time gravity balance, finally realize accurate leveling.Namely cradle head device of the present utility model can be disassembled part after installing and only need realize center-of-gravity regulating by roll axle 2 and pitch axis 4, by twice allotment center of gravity, can reduce each motor load to greatest extent, ensure the stable of The Cloud Terrace.
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 cradle head device for unmanned plane, comprise connected The Cloud Terrace mount pad (1) and device installation assembly, it is characterized in that, described The Cloud Terrace mount pad (1) comprises erecting stage and slide rail type bindiny mechanism, described slide rail type bindiny mechanism comprises one or more slide rail be connected to bottom unmanned plane and the chute be installed on erecting stage, described The Cloud Terrace mount pad (1) with when being connected bottom unmanned plane, described slide rail is sheathed in chute to complete to connect and coordinates.
2. the cradle head device for unmanned plane according to claim 1, it is characterized in that, described chute comprises grab parts more than two, and many group grab parts arrange the passage being formed and coordinate with slide rail successively, often organize grab parts and include two in grab positioned opposite.
3. the cradle head device for unmanned plane according to claim 1, is characterized in that, the extreme position of moving at described slide rail is provided with stopper section, and described stopper section is arranged on chute or slide rail.
4. the cradle head device for unmanned plane according to claim 1 or 2 or 3, it is characterized in that, also comprise the locking member be installed on erecting stage, described locking member comprises bayonet lock (19), bayonet lock mount pad (18) and spring assembly, described bayonet lock (19) and spring assembly are installed in bayonet lock mount pad (18), and the lower end of described bayonet lock (19) coordinates with spring assembly; Under the effect of spring assembly, described bayonet lock (19) keeps up jack-up state, when described slide rail need to slip into chute coordinate time, described bayonet lock (19) pressure to bounce back in bayonet lock mount pad (18) and compression spring assembly.
5. the cradle head device for unmanned plane according to claim 4, it is characterized in that, described spring assembly is at least one group, often organize spring assembly and include registration mast (22) and spring (21), described registration mast (22) is fixed on erecting stage, and described spring (21) is fixed by described registration mast (22).
6. the cradle head device for unmanned plane according to claim 4, is characterized in that, described bayonet lock (19) is provided with non-slip operation portion (192) towards the one side of operator.
7. the cradle head device for unmanned plane according to claim 4, is characterized in that, is detachably install between described bayonet lock mount pad (18) and erecting stage; The bottom of described bayonet lock mount pad (18) outer wall arranges a clamp button of the spring (181), described erecting stage is provided with the draw-in groove coordinated with clamp button of the spring (181).
8. the cradle head device for unmanned plane according to claim 1 or 2 or 3, it is characterized in that, described device installation assembly comprises roll axle (2) and pitch axis (4), one end of described pitch axis (4) is used for being connected with device to be installed, the other end of described pitch axis (4) is connected with the lower end of roll axle (2) by the second motor (6), and the upper end of described roll axle (2) is connected with described The Cloud Terrace mount pad (1).
9. the cradle head device for unmanned plane according to claim 8, it is characterized in that, be connected by the first attaching parts (10) between described pitch axis (4) with the second motor (6), described second motor (6) is fixed on roll axle (2), described first attaching parts (10) is directly fixed on the second motor (6), described first attaching parts (10) is provided with boss (101), upper one end be connected with the first attaching parts (10) offers groove (401) to described pitch axis (4), described boss (101) is sheathed in groove (401) and coordinates to complete slip.
10. the cradle head device for unmanned plane according to claim 8, is characterized in that, described roll axle (2) is provided with roll axle protecgulum (3), described roll axle protecgulum (3) offers the groove for installation second motor (6).
11. cradle head devices for unmanned plane according to claim 10, it is characterized in that, described roll axle (2) is connected with the 3rd motor (7) by the second attaching parts (11), and described 3rd motor (7) is fixed on The Cloud Terrace mount pad (1) by attaching parts; The two side walls of described roll axle (2) and roll axle protecgulum (3) all offers the through hole (201) for the second attaching parts (11) parallel sliding, to make described roll axle (2) can relative second attaching parts (11) parallel sliding with roll axle protecgulum (3).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520909254.5U CN205131696U (en) | 2015-11-16 | 2015-11-16 | A cloud platform device for unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520909254.5U CN205131696U (en) | 2015-11-16 | 2015-11-16 | A cloud platform device for unmanned aerial vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205131696U true CN205131696U (en) | 2016-04-06 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201520909254.5U Expired - Fee Related CN205131696U (en) | 2015-11-16 | 2015-11-16 | A cloud platform device for unmanned aerial vehicle |
Country Status (1)
| Country | Link |
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| CN (1) | CN205131696U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105270646A (en) * | 2015-11-16 | 2016-01-27 | 湖南云顶智能科技有限公司 | Holder device of unmanned airplane |
| CN105882993A (en) * | 2016-05-16 | 2016-08-24 | 深圳市智璟科技有限公司 | Quickly-detachable holder and unmanned aerial vehicle |
-
2015
- 2015-11-16 CN CN201520909254.5U patent/CN205131696U/en not_active Expired - Fee Related
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105270646A (en) * | 2015-11-16 | 2016-01-27 | 湖南云顶智能科技有限公司 | Holder device of unmanned airplane |
| CN105270646B (en) * | 2015-11-16 | 2018-05-01 | 湖南云顶智能科技有限公司 | Cradle head device for unmanned plane |
| CN105882993A (en) * | 2016-05-16 | 2016-08-24 | 深圳市智璟科技有限公司 | Quickly-detachable holder and unmanned aerial vehicle |
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| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20160406 Termination date: 20211116 |
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| CF01 | Termination of patent right due to non-payment of annual fee |