CN205098486U - Unmanned aerial vehicle - Google Patents
Unmanned aerial vehicle Download PDFInfo
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- CN205098486U CN205098486U CN201520790604.0U CN201520790604U CN205098486U CN 205098486 U CN205098486 U CN 205098486U CN 201520790604 U CN201520790604 U CN 201520790604U CN 205098486 U CN205098486 U CN 205098486U
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- fuselage
- buckle
- connect
- permanent seat
- plug
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Abstract
The utility model discloses an unmanned aerial vehicle, including the fuselage with set up in the cloud platform of fuselage below, the cloud platform has a fixing base of being connected with the fuselage, has first plug head on the fixing base, have on the fuselage with a first plug head second plug head that docks, be provided with a grafting portion on the fixing base, grafting portion extends along the direction of inserting that first plug head inserted second plug head, is provided with the slot that is used for acceping grafting portion on the fuselage, still be provided with the card portion of holding on the fixing base, the card portion of holding includes the buckle that extends towards the fuselage, sets up on the fuselage and to hold the draw -in groove of buckle. The utility model discloses an unmanned aerial vehicle sets up one a calorie of portion of holding and a grafting portion, general on the one hand on through the fixing base at the cloud platform grafting portion inserts the slot, on the other hand will the buckle card of the card portion of holding is gone into the draw -in groove is in order to incite somebody to action the cloud platform detachable be fixed in on the unmanned aerial vehicle fuselage, make the installation of cloud platform and fuselage and dismantle very convenient and fast.
Description
Technical field
The utility model relates to unmanned air vehicle technique field, particularly a kind of unmanned plane.
Background technology
Unmanned plane with its action flexibly, landing environmental requirement is lower, and has good operating characteristic etc., be widely used in take photo by plane, monitor, investigate, the numerous areas such as search and rescue.
For the ease of obtaining video or photographic intelligence, unmanned plane generally can configure The Cloud Terrace to take photo by plane, but, the The Cloud Terrace of existing unmanned plane and the connection mode of fuselage more complicated, four angles by the permanent seat of The Cloud Terrace are fixed by screws on fuselage.So, just result in the Assembly &Disassembly inconvenience of The Cloud Terrace.
Utility model content
Main purpose of the present utility model is to provide a kind of unmanned plane, is intended to promote the The Cloud Terrace of unmanned plane and the Assembly &Disassembly efficiency of fuselage.
For achieving the above object, the utility model provides a kind of unmanned plane, comprise fuselage and be arranged at the The Cloud Terrace below described fuselage, described The Cloud Terrace has a permanent seat be connected with described fuselage, described permanent seat has the first connect-disconnect plug, described fuselage has the second connect-disconnect plug docked with described first connect-disconnect plug, described The Cloud Terrace is electrically connected by described first connect-disconnect plug and the second connect-disconnect plug with described fuselage, described permanent seat being provided with a Plug Division, described fuselage being provided with the slot for accommodating described Plug Division; Described permanent seat is also provided with holding section, and described holding section comprises the buckle extended towards fuselage, described fuselage is provided with the draw-in groove that can hold described buckle; Described The Cloud Terrace inserts described slot by described Plug Division, and described buckle snaps in described draw-in groove and is fixed on described fuselage.
Preferably, described permanent seat comprises the adapter plate that faces described fuselage bottom, and described first connect-disconnect plug, Plug Division and holding section are all arranged on described adapter plate; The direction of insertion that described second connect-disconnect plug is inserted along described first connect-disconnect plug in described Plug Division extends.
Preferably, described adapter plate has the front-end and back-end in the direction of insertion of described second connect-disconnect plug of described first connect-disconnect plug insertion, the front end of described adapter plate offers two stepping down breach of extending backwards, the two partial fixing plates of stepping down between breach form described Plug Division, and breach of stepping down described in two is for stepping down to relative two cell walls of described slot.
Preferably, the one side towards described fuselage bottom of described Plug Division is provided with reinforced rib, and described reinforced rib extends at fore-and-aft direction.
Preferably, described Plug Division bends obliquely downward.
Preferably, described permanent seat has the front-end and back-end in the direction of insertion of described second connect-disconnect plug of described first connect-disconnect plug insertion, and described plugging position is in described front end, and described fastening part is in described rear end.
Preferably, described buckle comprises the projection of the side being arranged at described buckle top; Described protruding bottom is hooked on bottom described draw-in groove, is fixed on described fuselage to make described permanent seat.
Preferably, described holding section also comprises a push rod, and described push rod one end is connected to the lower end of described buckle and extends along described permanent seat, is exposed to described permanent seat rear end to the described push rod other end; Described holding section also comprises an elastic component, and described elastic component is arranged at one end that described push rod connects buckle, and its deformation direction is identical with push rod bearing of trend.
Preferably, the rear end of described permanent seat offers a blind hole extended forward, and described blind hole has at the bottom of the hole of a backward-facing, and described permanent seat one side upward also offers a through hole, and described through hole is communicated with described blind hole; The lower end of described buckle is arranged in described blind hole, and described buckle upwards extends through described through hole, and described push rod extends back from blind hole described in the lower end edge of described buckle, and described elastic component to be arranged in described blind hole and to abut with at the bottom of described hole.
Unmanned plane of the present utility model by arranging a holding section and a Plug Division on the permanent seat of The Cloud Terrace, on the one hand described slot is inserted in described Plug Division, on the other hand the buckle of described holding section is snapped in described draw-in groove, to be fixed on described unmanned aerial vehicle body by described The Cloud Terrace detouchable, make the Assembly &Disassembly of described The Cloud Terrace and fuselage very convenient and swift.
Accompanying drawing explanation
In order to be illustrated more clearly in the utility model embodiment or technical scheme of the prior art, be briefly described to the accompanying drawing used required in embodiment or description of the prior art below, apparently, accompanying drawing in the following describes is only embodiments more of the present utility model, for those of ordinary skill in the art, under the prerequisite not paying creative work, the structure according to these accompanying drawings can also obtain other accompanying drawing.
Fig. 1 be in the utility model unmanned plane one embodiment fuselage and The Cloud Terrace assemble before structural representation;
Fig. 2 is the partial enlarged drawing at A place in Fig. 1;
Fig. 3 is the structural representation of The Cloud Terrace in Fig. 1;
Fig. 4 is the front elevation of unmanned plane in Fig. 1;
Fig. 5 is the cutaway view along M-M hatching line in Fig. 4;
Fig. 6 is the partial enlarged drawing at B place in Fig. 5.
Drawing reference numeral illustrates:
| Label | Title | Label | Title |
| 10 | Fuselage | 101 | Second connect-disconnect plug |
| 102 | Slot | 103 | Draw-in groove |
| 1031 | Hold plate | 20 | The Cloud Terrace |
| 21 | Permanent seat | 210 | Adapter plate |
| 2101 | To step down breach | 2102 | Reinforced rib |
| 211 | First connect-disconnect plug | 212 | Plug Division |
| 213 | Holding section | 2131 | Buckle |
| 2131a | Support portion | 2131b | Protruding |
| 2132 | Elastic component | 2133 | Push rod |
| 2134 | Press section | 22 | Mount pad |
| 23 | Filming apparatus |
The realization of the utility model object, functional characteristics and advantage will in conjunction with the embodiments, are described further with reference to accompanying drawing.
Detailed description of the invention
Below in conjunction with the accompanying drawing in the utility model embodiment, be clearly and completely described the technical scheme in the utility model embodiment, obviously, described embodiment is only a part of embodiment of the present utility model, instead of whole embodiments.Based on the embodiment in the utility model, those of ordinary skill in the art are not making the every other embodiment obtained under creative work prerequisite, all belong to the scope of the utility model protection.
Need explanation, all directivity instruction (such as up, down, left, right, before and afters in the utility model embodiment ...) only for explaining the relative position relation, motion conditions etc. under a certain particular pose (as shown in drawings) between each parts, if when this particular pose changes, then directionality instruction also correspondingly changes thereupon.
In addition, in the utility model, relate to the description of " first ", " second " etc. only for describing object, and instruction can not be interpreted as or imply its relative importance or the implicit quantity indicating indicated technical characteristic.Thus, be limited with " first ", the feature of " second " can express or impliedly comprise at least one this feature.In addition; technical scheme between each embodiment can be combined with each other; but must be can be embodied as basis with those of ordinary skill in the art; when technical scheme combination occur conflicting maybe cannot realize time will be understood that the combination of this technical scheme does not exist, also not the utility model require protection domain within.
The utility model proposes a kind of unmanned plane.
Referring to figs. 1 through Fig. 6, in the utility model embodiment, the The Cloud Terrace 20 that this unmanned plane comprises fuselage 10 and is arranged at below described fuselage 10, described The Cloud Terrace 20 has a permanent seat 21 be connected with described fuselage 10, described permanent seat 21 has the first connect-disconnect plug 211, described fuselage 10 has the second connect-disconnect plug 101 docked with described first connect-disconnect plug 211, described The Cloud Terrace 20 is electrically connected by described first connect-disconnect plug 211 and the second connect-disconnect plug 101 with described fuselage 10, described permanent seat 21 is provided with a Plug Division 212, the direction of insertion that described second connect-disconnect plug 101 is inserted along described first connect-disconnect plug 211 in described Plug Division 212 extends, described fuselage 10 is provided with the slot 102 for accommodating described Plug Division 212, described permanent seat 21 is also provided with holding section 213, and described holding section 213 comprises the buckle 2131 extended towards fuselage 10, described fuselage 10 is provided with and can holds draw-in groove 103 corresponding to described buckle 2131 position, described The Cloud Terrace 20 inserts described slot 102 by described Plug Division 212, and described buckle 2131 snaps in described draw-in groove 103 and is fixed on described fuselage 10.
Particularly, in the present embodiment, with reference to Fig. 1, Fig. 2, Fig. 3 and Fig. 6, the The Cloud Terrace 20 of described unmanned plane comprises permanent seat 21, mount pad 22 and filming apparatus 23, and described filming apparatus 23 to be installed on described permanent seat 21 by described mount pad 22.Described camera head 23 carries three motors, and three motors can drive the camera of camera head to move, and can multi-angle rotary, thus obtains wider visual angle.When described The Cloud Terrace 20 is installed on described fuselage 10, first that described first connect-disconnect plug 211 is corresponding with the second connect-disconnect plug 102 position, then while the first connect-disconnect plug 211 is inserted the second connect-disconnect plug 101, described Plug Division 212 is inserted in described slot 102, then to the power that described The Cloud Terrace 20 applies upwards, the buckle 2131 of described holding section 213 is made to stretch in described draw-in groove 103, described buckle 2131 holds fixing by described draw-in groove 103, like this, under the effect of described buckle 2131 and described slot 212 double limitation, described The Cloud Terrace 20 can be fixed on bottom described fuselage 10.
It should be noted that, the embodiment that described buckle 2131 snaps in described draw-in groove 103 has multiple, and e.g., described buckle 2131 upper end has a projection, the width of rebate of described draw-in groove 103 is less than the width of described projection, described buckle 2131 and described draw-in groove 103 interference fit.Also can be that described buckle 2131 comprises a shell fragment and a grab, one end of described shell fragment is fixed on described permanent seat 21, the other end connects described grab, when described buckle 2131 is inserted described draw-in groove 103, the notch of described draw-in groove 103 extrudes described grab, described shell fragment generation elastic deformation, until when described grab passes completely through described draw-in groove 103, described shell fragment recovers elastic deformation, and the cell wall of described draw-in groove 103 hooks by described grab, fixing to realize holding.
In addition, when described The Cloud Terrace 20 is dismantled from described unmanned aerial vehicle body 10, only need to apply a power to described buckle 2131, make described buckle 2131 depart from described draw-in groove 103, then described Plug Division 212 is extracted out from described slot 102.
Unmanned plane of the present utility model by arranging holding section 213 and a Plug Division 212 on the permanent seat 21 of The Cloud Terrace 20, on the one hand described slot 102 is inserted in described Plug Division 212, on the other hand the buckle of described holding section 213 is snapped in described draw-in groove 103, to be removably fixed on described unmanned aerial vehicle body 10 by described The Cloud Terrace 20, make described The Cloud Terrace 20 very convenient and swift with the Assembly &Disassembly of fuselage 10.
Further, continue with reference to Fig. 2 and Fig. 3, described permanent seat 21 comprises one and faces adapter plate 210 bottom described fuselage 10, and described first connect-disconnect plug 211, Plug Division 212 and holding section 213 are all arranged on described adapter plate 210; The direction of insertion that described second connect-disconnect plug 212 is inserted along described first connect-disconnect plug 211 in described Plug Division 212 extends.
In the present embodiment, insert in described slot 102 for the ease of described Plug Division 212, the direction of insertion being set to the bearing of trend of described Plug Division 212 with described first connect-disconnect plug 211 is identical, and namely described Plug Division 212 extends back.So, when described The Cloud Terrace 20 is installed on described unmanned aerial vehicle body 10 by user, described Plug Division 212 be insert described second connect-disconnect plug 212 with described first connect-disconnect plug 211 while insert described slot 102.
Further, described adapter plate 210 has the front-end and back-end in the direction of insertion that described first connect-disconnect plug 211 inserts described second connect-disconnect plug 101, the front end of described adapter plate 210 offers two stepping down breach 2101 of extending backwards, the two partial fixing plates 210 of stepping down between breach 2101 form described Plug Division 212, and breach 2101 of stepping down described in two is for stepping down to relative two cell walls of described draw-in groove 102.
Particularly, in the present embodiment, described Plug Division 212 is a part for described adapter plate 210, and this Plug Division 212 is positioned at the front end of described adapter plate 210.When described slot 102 is inserted in described Plug Division 212, on the one hand, relative two cell walls of described slot 102 hold by breach 2101 of stepping down described in two, on the other hand, described Plug Division 212 is overlapped on the internal face of the lower wall of described draw-in groove 102, described draw-in groove 102 carries described Plug Division 212, to support described adapter plate 210.This set of described Plug Division 212 makes the structure of described permanent seat 21 more succinct, manufactures more convenient.
Further, continue with reference to Fig. 3, described Plug Division 212 the one side bottom described fuselage 10 is provided with reinforced rib 2102, described reinforced rib 2102 extends at fore-and-aft direction.
Particularly, in the present embodiment, described reinforced rib 2102 the intensity can strengthening on the one hand described Plug Division 212 is set, described Plug Division 212 can be made more stable in described slot 102 on the other hand, can not rock.
Further, continue with reference to Fig. 3, described Plug Division 212 extends obliquely downward.
If described Plug Division 212 extends in the horizontal direction, so described Plug Division 212 bending resistance is in the vertical direction poor.In the present embodiment, described Plug Division 212 extends obliquely downward, so just adds the stress of described Plug Division 212, described Plug Division 212 also not easy fracture.
In addition, this set of described Plug Division 212 also make this Plug Division 212 can with the internal face close contact of described slot 102, add the stability of Plug Division 212 in described slot 102.
Further, continue with reference to Fig. 3, described permanent seat 21 has the front-end and back-end in the direction of insertion that described first connect-disconnect plug 211 inserts described second connect-disconnect plug 101, and described Plug Division 212 is positioned at described front end, and described holding section 213 is positioned at described rear end.
In the present embodiment, described Plug Division 212 being arranged on described front end, described holding section 213 being arranged at the stationarity of described rear end mainly in order to keep described permanent seat 21 to install, make described permanent seat 21 stressed evenly.
Further, with reference to Fig. 4, Fig. 5 and Fig. 6, described buckle 2131 comprises the protruding 2131b of the side being arranged at described buckle 2131 top; Be hooked on bottom described protruding 2131b bottom described draw-in groove 102, be fixed on described fuselage 10 to make described permanent seat 21.
Particularly, described buckle 2131 comprises the support portion 2131a extended upward, the side of the upper end of described support portion 2131a is provided with a protruding 2131b, and described protruding 2131b extends back, and described protruding 2131b cross-sectional area in the horizontal direction from up to down increases gradually; The internal face of described draw-in groove 102 comprises the first wall forward, and the second wall backwards, described first wall extends one towards described second wall and holds plate 1031, described in hold and between plate 1031 and described second wall, to form a bayonet socket inserted for described buckle 2131.
The present embodiment provides a kind of embodiment of holding section 213.The lower end of described support portion 2131a can be fixedly connected with described permanent seat 21, also can be relative to described permanent seat 21 slidably.
If the lower end of described support portion 2131a is fixedly connected with described permanent seat 21, when described buckle 2131 is inserted the bayonet socket of described draw-in groove 103, the described plate 1031 that holds produces a squeese pressure forward to described protruding 2131b, described support portion 2131a bend forward, until described protruding 2131b fully pass over described in when holding plate 1031, described support portion 2131a recovers deformation, and lower surface and the described plate 1031 that holds of described protruding 2131b support.When described buckle 2131 is extracted out by needs from described draw-in groove 103, a thrust is forward applied to described support portion 2131a, to make described support portion 2131a bend forward, then twitch described buckle 2131, described protruding 2131b is deviate from from described bayonet socket.
In addition, described buckle 2131 and described permanent seat 21 sliding block joint, namely described buckle 2131 can slide in the longitudinal direction.Following content to described buckle 2131 on permanent seat 21 slidably an embodiment set forth:
Particularly, with reference to Fig. 6, the rear end of described permanent seat 21 offers a blind hole extended forward, and described blind hole has at the bottom of the hole of a backward-facing, and described permanent seat 21 one side upward also offers a through hole, and described through hole is communicated with described blind hole; Described holding section 213 comprises an elastic component 2132, and the lower end of described buckle 2131 is positioned at described blind hole, and described buckle 2131 upwards extends through described through hole, between described elastic component 2132 is arranged at the bottom of the lower end of described buckle 2131 and described hole.
So, under the elastic reaction of described elastic component 2132, described support portion 2131a can move at fore-and-aft direction.When described hold plate 1031 squeese pressure is forward applied to described protruding 2131b time, described support portion 2131a moves forward, described elastic component 2132 is compressed, when holding plate 1031 described in described protruding 2131b fully passes over, described elastic component 2132 promotes described support portion 2131a and moves backward, so far, described buckle 2131 is fastened in described draw-in groove 103.
Further, with reference to Fig. 6, described holding section 213 also comprises a push rod 2133, and described push rod 2133 one end is connected to the lower end of described buckle 2131 and extends along described permanent seat 21, is exposed to described permanent seat 21 rear end to described push rod 2133 other end; Described holding section 213 also comprises an elastic component 2132, and described elastic component 2132 is arranged at one end that described push rod 2133 connects buckle 2131, and its deformation direction is identical with push rod 2133 bearing of trend.
For the ease of the dismounting of described The Cloud Terrace 20, in the present embodiment, the setting of described push rod 2133 is convenient to user and is manually exerted a force to described buckle 2131, so that described buckle 2131 departs from described draw-in groove 103.
Exerting a force to described push rod 2133 to further facilitate user, can also also be provided with a press section 2134 in the rear end of described push rod 2133.
Further, with reference to Fig. 6, on the basis of a upper embodiment, the rear end of described permanent seat 21 offers a blind hole extended forward, described blind hole has at the bottom of the hole of a backward-facing, and described permanent seat 21 one side upward also offers a through hole, and described through hole is communicated with described blind hole; The lower end of described buckle 2131 is arranged in described blind hole, described buckle 2131 upwards extends through described through hole, described push rod 2133 extends back from blind hole described in the lower end edge of described buckle 2131, and described elastic component 2132 to be arranged in described blind hole and to abut with at the bottom of described hole.
Described blind hole plays spacing and directional tagging to the movable of described push rod 2133.Particularly, when user needs described The Cloud Terrace dismounting, user only needs in described blind hole, promote described push rod 2133, makes described buckle 2131 depart from described draw-in groove 103, is then extracted out from described slot 102 described Plug Division 212.Equally, when described The Cloud Terrace 20 is installed, only need described Plug Division 212 to insert described slot 102, then upwardly described buckle 2131, make described buckle 2131 snap in described draw-in groove 103.So, described The Cloud Terrace 20 and described fuselage 10 assembling and dismantle very convenient.
The foregoing is only preferred embodiment of the present utility model; not thereby the scope of the claims of the present utility model is limited; every under inventive concept of the present utility model; utilize the equivalent structure transformation that the utility model specification sheets and accompanying drawing content are done, or directly/be indirectly used in other relevant technical fields to include in scope of patent protection of the present utility model.
Claims (9)
1. a unmanned plane, comprise fuselage and be arranged at the The Cloud Terrace below described fuselage, described The Cloud Terrace has a permanent seat be connected with described fuselage, it is characterized in that, described permanent seat has the first connect-disconnect plug, described fuselage has the second connect-disconnect plug docked with described first connect-disconnect plug, described The Cloud Terrace is electrically connected by described first connect-disconnect plug and the second connect-disconnect plug with described fuselage, described permanent seat being provided with a Plug Division, described fuselage being provided with the slot for accommodating described Plug Division; Described permanent seat is also provided with holding section, and described holding section comprises the buckle extended towards fuselage, described fuselage is provided with the draw-in groove that can hold described buckle; Described The Cloud Terrace inserts described slot by described Plug Division, and described buckle snaps in described draw-in groove and is fixed on described fuselage.
2. unmanned plane as claimed in claim 1, it is characterized in that, described permanent seat comprises the adapter plate that faces described fuselage bottom, and described first connect-disconnect plug, Plug Division and holding section are all arranged on described adapter plate; The direction of insertion that described second connect-disconnect plug is inserted along described first connect-disconnect plug in described Plug Division extends.
3. unmanned plane as claimed in claim 2, it is characterized in that, described adapter plate has the front-end and back-end in the direction of insertion of described second connect-disconnect plug of described first connect-disconnect plug insertion, the front end of described adapter plate offers two stepping down breach of extending backwards, the two partial fixing plates of stepping down between breach form described Plug Division, and breach of stepping down described in two is for stepping down to relative two cell walls of described slot.
4. unmanned plane as claimed in claim 3, it is characterized in that, the one side towards described fuselage bottom of described Plug Division is provided with reinforced rib, and described reinforced rib extends at fore-and-aft direction.
5. the unmanned plane as described in claim 2,3 or 4, is characterized in that, described Plug Division bends obliquely downward.
6. unmanned plane as claimed in claim 1, is characterized in that, described permanent seat has the front-end and back-end in the direction of insertion of described second connect-disconnect plug of described first connect-disconnect plug insertion, and described plugging position is in described front end, and described fastening part is in described rear end.
7. unmanned plane as claimed in claim 1, it is characterized in that, described buckle comprises the projection of the side being arranged at described buckle top; Described protruding bottom is hooked on bottom described draw-in groove, is fixed on described fuselage to make described permanent seat.
8. unmanned plane as claimed in claim 7, it is characterized in that, described holding section also comprises a push rod, and described push rod one end is connected to the lower end of described buckle and extends along described permanent seat, is exposed to described permanent seat rear end to the described push rod other end; Described holding section also comprises an elastic component, and described elastic component is arranged at one end that described push rod connects buckle, and its deformation direction is identical with push rod bearing of trend.
9. unmanned plane as claimed in claim 8, it is characterized in that, the rear end of described permanent seat offers a blind hole extended forward, and described blind hole has at the bottom of the hole of a backward-facing, described permanent seat one side upward also offers a through hole, and described through hole is communicated with described blind hole; The lower end of described buckle is arranged in described blind hole, and described buckle upwards extends through described through hole, and described push rod extends back from blind hole described in the lower end edge of described buckle, and described elastic component to be arranged in described blind hole and to abut with at the bottom of described hole.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520790604.0U CN205098486U (en) | 2015-10-13 | 2015-10-13 | Unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520790604.0U CN205098486U (en) | 2015-10-13 | 2015-10-13 | Unmanned aerial vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205098486U true CN205098486U (en) | 2016-03-23 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201520790604.0U Active CN205098486U (en) | 2015-10-13 | 2015-10-13 | Unmanned aerial vehicle |
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| CN (1) | CN205098486U (en) |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| 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 |
| CN105889725A (en) * | 2016-05-25 | 2016-08-24 | 北京小米移动软件有限公司 | Holder structure, fixing frame thereof, air vehicle body and air vehicle |
| CN107344627A (en) * | 2016-05-06 | 2017-11-14 | 北京臻迪机器人有限公司 | A kind of head and control method for being installed on unmanned plane |
| CN108750132A (en) * | 2018-08-10 | 2018-11-06 | 深圳市道通智能航空技术有限公司 | Unmanned plane |
| CN111776214A (en) * | 2020-06-17 | 2020-10-16 | 广东工业大学 | Real-time imaging device for road survey |
-
2015
- 2015-10-13 CN CN201520790604.0U patent/CN205098486U/en active Active
Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107344627A (en) * | 2016-05-06 | 2017-11-14 | 北京臻迪机器人有限公司 | A kind of head and control method for being installed on 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 |
| CN105889725A (en) * | 2016-05-25 | 2016-08-24 | 北京小米移动软件有限公司 | Holder structure, fixing frame thereof, air vehicle body and air vehicle |
| CN105889725B (en) * | 2016-05-25 | 2018-06-12 | 北京小米移动软件有限公司 | Cradle head structure and its fixed frame, aircraft body and aircraft |
| CN108750132A (en) * | 2018-08-10 | 2018-11-06 | 深圳市道通智能航空技术有限公司 | Unmanned plane |
| WO2020030133A1 (en) * | 2018-08-10 | 2020-02-13 | 深圳市道通智能航空技术有限公司 | Unmanned aerial vehicle |
| CN111776214A (en) * | 2020-06-17 | 2020-10-16 | 广东工业大学 | Real-time imaging device for road survey |
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