CN205396528U - Horn detachable unmanned aerial vehicle - Google Patents
Horn detachable unmanned aerial vehicle Download PDFInfo
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- CN205396528U CN205396528U CN201620179378.7U CN201620179378U CN205396528U CN 205396528 U CN205396528 U CN 205396528U CN 201620179378 U CN201620179378 U CN 201620179378U CN 205396528 U CN205396528 U CN 205396528U
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- horn
- loop bar
- groove
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- unmanned plane
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Abstract
The utility model provides a horn detachable unmanned aerial vehicle belongs to the aircraft field, including fuselage and horn, be provided with the installation department on the fuselage, be provided with drive arrangement on the horn, drive arrangement was kept away from to the horn one end is passed through the connecting piece and can be dismantled with the installation department and be connected. This unmanned aerial vehicle's horn and the installation department of fuselage pass through the connecting piece can be dismantled and be connected, has both guaranteed the joint strength of horn with the fuselage, enable the horn again and can follow the fuselage and pull down, the maintenance of being convenient for, but horn or fuselage reuse have practiced thrift the cost, have also strengthened this unmanned aerial vehicle's portability, can the horn dismantle put into the slightly little knapsack of volume in.
Description
Technical field
This utility model relates to aircraft field, in particular to a kind of dismountable unmanned plane of horn.
Background technology
UAV is called for short " unmanned plane ", and english abbreviation is " UAV ", is the not manned aircraft of the presetting apparatus manipulation utilizing radio robot with providing for oneself.Unmanned plane is actually the general designation of unmanned vehicle.The horn of existing unmanned plane is usually and fuselage one, this is to ensure that the bonding strength between horn and fuselage, but the horn of this unmanned plane and fuselage are non-removable, once horn is damaged, not only being difficult to keep in repair, even whole fuselage is required for scrapping, and causes the wasting of resources, and this unmanned plane can only entirety carry, and portability is poor.
Utility model content
This utility model provides a kind of dismountable unmanned plane of horn, it is intended to improve the problems referred to above.
This utility model is achieved in that
A kind of dismountable unmanned plane of horn, including fuselage and horn, described fuselage is provided with installation portion, described horn is provided with driving device, and described horn is removably connected by connector and described installation portion away from one end of described driving device.
Further, described connector includes the first connector, described first connector is arranged in described horn, described first connector includes the first loop bar and the second loop bar, described first loop bar is connected with described horn, described second loop bar is connected with described installation portion, and described first loop bar and described second loop bar are connected with each other.
Adopt the first loop bar and the second loop bar, it is possible to horn and installation portion are connected securely, it is ensured that bonding strength.
Further, described first connector also includes the first fixture block and the second fixture block；
One end of described first loop bar is provided with the first draw-in groove, and described first fixture block embeds in described first draw-in groove, described first loop bar and described horn clamping；
One end of described second loop bar is provided with the second draw-in groove, and described second fixture block embeds in described second draw-in groove, described second loop bar and described installation portion clamping, described first fixture block and described second fixture block clamping.
By arranging the first fixture block and the second fixture block, it is possible to the first loop bar and the second loop bar are connected together securely, improve bonding strength.
Further, described first fixture block is multi-edge column-shaped, and the second fixture block is and the multi-edge column-shaped of described first card Block-matching, and the cell wall of described first draw-in groove mates with the outer wall of described first fixture block, and the cell wall of described second draw-in groove mates with the outer wall of described second fixture block.
First fixture block and the second fixture block adopt identical multi-edge column-shaped, can either ensure that clamping is firm, are more prevented from reversing, improve the bonding strength of horn and installation portion further, strengthen connecting portion transverse strength.
Further, first groove being circumferentially provided with multiple strip of described first loop bar, described first groove is arranged along the direction being parallel to described first set rod axis, and described first groove connects with described first draw-in groove；
Second groove being circumferentially provided with multiple strip of described second loop bar, described second groove extends along the direction being parallel to described second set rod axis, and described second groove connects with described second draw-in groove.
Horn is if it occur that reverse, the cell wall of the first groove can prop up the first projection, then produce between the first loop bar and the first projection to stop the active force reversed, in like manner, the cell wall of the second groove can prop up the second projection, then produce between the second loop bar and the second projection to stop the active force reversed, thus stoping horn to reverse, make the connection between horn and fuselage more firm, it is ensured that the bonding strength of junction.
Further, described first fixture block is provided with boss, described second fixture block is provided with link slot, described boss is provided with bar-shaped trough, being provided with bar blocks on the cell wall of described link slot, described boss coordinates with described link slot, and described bar blocks coordinates with described bar-shaped trough.
When first fixture block and the second fixture block coordinate, boss is inserted in link slot, and bar blocks is inserted in bar-shaped trough simultaneously, and the first fixture block and the second fixture block plug together mutually, it is possible to the connection making the first fixture block and the second fixture block is more tight, prevents torsional deflection further simultaneously.
Further, described connector includes the second connector, and described second connector includes block, and described block is set in the junction of described installation portion and described horn and props up the end of described first loop bar.
By arranging block, a block part can prop up the end of the first loop bar, and a part can be enclosed within outside installation portion and horn so that block encases the junction of installation portion and horn, makes connection more firm, and makes inner connecting structure more safe and reliable.
Further, it is provided with ball between the outer wall of described block and described installation portion.By arranging ball, it is possible to anti-stop block, with installation portion, axially opposing movement occurs, and it is more firm to connect.
Further, described second connector also includes sleeve, and described sleeve is set in outside described block.Block and inner connecting structure can be played a protective role by sleeve.
Further, described first loop bar is provided with the first card article, described second loop bar is provided with the second card article, described first card article and described horn clamping, described second card article and described installation portion clamping.
First card article and the second card article can make the first loop bar and horn, between the second loop bar and installation portion clamping more closely firm.
The dismountable unmanned plane of horn that this utility model provides provides the benefit that: the horn of this unmanned plane and the installation portion of fuselage are removably connected by connector, both ensure that the bonding strength of horn and fuselage, horn can be made again can to pull down from fuselage, it is easy to maintenance, horn or the repeatable utilization of fuselage, save cost, also enhanced the portability of this unmanned plane, it is possible to horn dismounting has been put in the knapsack that volume is slightly smaller.
Accompanying drawing explanation
In order to be illustrated more clearly that the technical scheme of this utility model embodiment, the accompanying drawing used required in embodiment will be briefly described below, it is to be understood that, the following drawings illustrate only some embodiment of the present utility model, therefore the restriction to scope it is not construed as, for those of ordinary skill in the art, under the premise not paying creative work, it is also possible to obtain other relevant accompanying drawings according to these accompanying drawings.
The overall structure schematic diagram of the dismountable unmanned plane of horn that Fig. 1 provides for this utility model embodiment；
The horn of the dismountable unmanned plane of horn that Fig. 2 provides for this utility model embodiment and the attachment structure sectional view of installation portion；
The assembling structural representation of the first connector of the dismountable unmanned plane of horn that Fig. 3 provides for this utility model embodiment；
The decomposition texture schematic diagram of the first connector of the dismountable unmanned plane of horn that Fig. 4 provides for this utility model embodiment；
The structural representation of the first loop bar of the dismountable unmanned plane of horn that Fig. 5 provides for this utility model embodiment；
The structural representation of the first projection of the dismountable unmanned plane of horn that Fig. 6 provides for this utility model embodiment；
The structural representation of the second projection of the dismountable unmanned plane of horn that Fig. 7 provides for this utility model embodiment；
The structural representation of the second loop bar of the dismountable unmanned plane of horn that Fig. 8 provides for this utility model embodiment.
Figure acceptance of the bid note is respectively as follows:
Fuselage 101；Horn 102；Installation portion 103；Driving device 104；Annular protrusion 105；
First connector 20；First loop bar 201；Second loop bar 202；First fixture block 203；Second fixture block 204；First draw-in groove 205；Second draw-in groove 206；First groove 207；Second groove 208；Boss 209；Link slot 210；Bar blocks 211；Bar-shaped trough 212；First card article 213；Second card article 214；First annular protuberance 215；Second annular protrusion 216；
Second connector 30；Block 301；Sleeve 302；Ball 303.
Detailed description of the invention
Designer of the present utility model finds under study for action, the horn of unmanned plane and fuselage are usually one, tracing it to its cause, various power in flight course are born in the junction being because horn and fuselage, and stressing conditions is complicated, if making dismountable, junction intensity is difficult to ensure that, horn easily snaps off, and causes unmanned plane to damage, and this unmanned plane can only entirety carry, and portability is poor.
Given this, designer of the present utility model is by long-term exploration and trial, and experiment repeatedly and effort, constantly reform and innovation, devise a kind of dismountable unmanned plane of horn, the installation portion 103 of horn 102 and fuselage 101 is removably connected by connector, both ensure that the bonding strength of horn 102 and fuselage 101, horn 102 can be made again can to pull down from fuselage 101.
For making the purpose of this utility model embodiment, technical scheme and advantage clearly, below in conjunction with the accompanying drawing in this utility model embodiment, technical scheme in this utility model embodiment is clearly and completely described, obviously, described embodiment is a part of embodiment of this utility model, rather than whole embodiments.Generally can with various different configurations arrange and design with the assembly of this utility model embodiment that illustrate described in accompanying drawing herein.Therefore, below the detailed description of the embodiment of the present utility model provided in the accompanying drawings is not intended to limit claimed scope of the present utility model, but is merely representative of selected embodiment of the present utility model.Based on the embodiment in this utility model, the every other embodiment that those of ordinary skill in the art obtain under not making creative work premise, broadly fall into the scope of this utility model protection.
Embodiment
Refer to Fig. 1, present embodiments provide a kind of dismountable unmanned plane of horn, this unmanned plane includes fuselage 101 and horn 102, fuselage 101 is provided with installation portion 103, being provided with driving device 104 on horn 102, horn 102 is removably connected by connector and installation portion 103 away from one end of driving device 104.
Wherein, installation portion 103 is part outwardly on fuselage 101, and it is designed as cylindrical shape away from one end of fuselage 101, and horn 102 is circular tube shaped.In the present embodiment, horn 102 is four, and installation portion 103 phase should be four, and the circumference along fuselage 101 is uniformly distributed.Driving device 104 adopts motor, is installed on the free end of horn 102, and motor is connected with rotor, can produce the lift that flight is required.
It addition, connector can adopt various structures, convenient dismounting.The present embodiment preferably employs the internal attachment structure connecting and combining with external connection, to ensure the bonding strength of the junction of horn 102 and installation portion 103, it is ensured that flight safety.
Referring to Fig. 1 and Fig. 2, connector includes the first connector 20 and the second connector 30.First connector 20 is arranged in horn 102, and namely the first connector 20 is inner connecting structure.Second connector 30 is arranged at outside horn 102 and installation portion 103, and namely the second connector 30 is external connection structure.
Referring to Fig. 2～Fig. 8, specifically, the first connector 20 includes the first loop bar the 201, second loop bar the 202, first fixture block 203 and the second fixture block 204.First loop bar 201 is connected with horn 102, and the second loop bar 202 is connected with installation portion 103, and the first loop bar 201 and the second loop bar 202 are connected with each other.Adopt the first loop bar 201 and the second loop bar 202, it is possible to horn 102 and installation portion 103 are connected securely, it is ensured that bonding strength.
As preferably, the first loop bar 201 being provided with the first card article 213, the second loop bar 202 is provided with the second card article 214, the first card article 213 and horn 102 clamping, the second card article 214 and installation portion 103 clamping.First card article 213 and the second card article 214 can make clamping between the first loop bar 201 and horn the 102, second loop bar 202 and installation portion 103 more closely firm.
Being provided with first annular protuberance 215 on first loop bar 201, first annular protuberance 215 projects radially outward along the first loop bar 201；Being provided with the second annular protrusion 216 on second loop bar 202, the second annular protrusion 216 projects radially outward along the second loop bar 202.The inwall of installation portion 103 is provided with annular protrusion 105, when connecting, the end face of the end face of the first annular protuberance 215 of the first loop bar 201 and the second annular protrusion 216 of the second loop bar 202 matches, the annular protrusion 105 of installation portion 103 props up second annular protrusion 216 one end end face away from first annular protuberance 215, second connector 30 props up the first annular protuberance 215 one end end face away from the second annular protrusion 216, say, that the first loop bar 201 and the second loop bar 202 are pressed on therebetween by the second connector 30 and annular protrusion 105.
One end of first loop bar 201 is provided with the first draw-in groove 205, and the first fixture block 203 embeds in the first draw-in groove 205, the first loop bar 201 and horn 102 clamping.One end of second loop bar 202 is provided with the second draw-in groove 206, and the second fixture block 204 embeds in the second draw-in groove 206, the second loop bar 202 and installation portion 103 clamping, the first fixture block 203 and the second fixture block 204 clamping.
By arranging the first fixture block 203 and the second fixture block 204, it is possible to the first loop bar 201 and the second loop bar 202 are connected together securely, improve bonding strength.
First fixture block 203 is multi-edge column-shaped, and the second fixture block 204 is the multi-edge column-shaped mated with the first fixture block 203, and the cell wall of the first draw-in groove 205 and the outer wall of the first fixture block 203 mate, and the cell wall of the second draw-in groove 206 and the outer wall of the second fixture block 204 mate.
First fixture block 203 and the second fixture block 204 adopt identical multi-edge column-shaped, can either ensure that clamping is firm, are more prevented from reversing, improve the bonding strength of horn 102 and installation portion 103 further, strengthen connecting portion transverse strength.
As preferably, in the present embodiment, the first fixture block 203 and the second fixture block 204 are triangular prism shaped, and its cross section is equal in magnitude, naturally it is also possible to adopt the prism of other shapes, for instance quadrangular, pentagonal prism, six prisms etc..But, because the limit quantity of polygon prism is more many, its cross section is closer to circle, and when twisting, its barrier effect is more little, and therefore, the present embodiment is preferably triangular prism shaped, both ensure that connection is firm, the effect that stop twists can be made again to reach the best.
It addition, first groove 207 being circumferentially provided with multiple strip of the first loop bar 201, the first groove 207 is arranged along the direction being parallel to the first loop bar 201 axis, and the first groove 207 connects with the first draw-in groove 205.Second groove 208 being circumferentially provided with multiple strip of the second loop bar 202, the second groove 208 extends along the direction being parallel to the second loop bar 202 axis, and the second groove 208 connects with the second draw-in groove 206.The quantity of the first groove 207 is equal with the seamed edge number of the first projection, and the quantity of the second groove 208 is equal with the seamed edge number of the second projection, and in the present embodiment, the first groove 207 and the second groove 208 are three.
Horn 102 is if it occur that reverse, the cell wall of the first groove 207 can prop up the first projection, then produce between the first loop bar 201 and the first projection to stop the active force reversed, in like manner, the cell wall of the second groove 208 can prop up the second projection, then produce between the second loop bar 202 and the second projection to stop the active force reversed, thus stoping horn 102 to reverse, make the connection between horn 102 and fuselage 101 more firm, it is ensured that the bonding strength of junction.
First groove 207 connects with the first draw-in groove 205, and the second groove 208 connects with the second draw-in groove 206, then the first projection is when embedding in the first draw-in groove 205, and its edge portions stretches in the first groove 207；In like manner, the second projection is when embedding in the second draw-in groove 206, and its edge portions stretches in the second groove 208.Further enhancing torsional strength.Additionally, can stretch to the part of the first groove 207 at the first projection, the second projection stretches to and is respectively provided with hole in the part of the second groove 208, during connection, first projection and the second projection are relative, and both holes are corresponding, can arrange pin in hole, both are connected, can also set up, on horn 102 and installation portion 103, the column structure mated with hole, by column structure, horn 102 is connected further with the first projection, installation portion 103 and the second projection, strengthen the fixing of attachment structure.
First fixture block 203 is provided with boss 209, second fixture block 204 is provided with link slot 210, boss 209 is provided with bar-shaped trough 212, the cell wall of link slot 210 is provided with bar blocks 211, boss 209 coordinates with link slot 210, and bar blocks 211 coordinates with bar-shaped trough 212.
When first fixture block 203 coordinates with the second fixture block 204, boss 209 is inserted in link slot 210, bar blocks 211 is inserted in bar-shaped trough 212 simultaneously, first fixture block 203 and the second fixture block 204 plug together mutually, the connection that can make the first fixture block 203 and the second fixture block 204 is more tight, prevents torsional deflection further simultaneously.
Specifically, referring to Fig. 2, the second connector 30 includes block 301 and sleeve 302, and block 301 is set in the junction of installation portion 103 and horn 102 and props up the end of the first loop bar 201.Sleeve 302 is set in outside block 301.Block 301 and inner connecting structure can be played a protective role by sleeve 302.It is provided with elastic component, it is possible to make the connection between sleeve 302 and block 301 tightr between sleeve 302 and block 301.When horn 102 and installation portion 103 connect, the first loop bar 201 and the second loop bar 202 are pressed on therebetween by block 301 and annular protrusion 105.
By arranging block 301 and sleeve 302, block 301 part can prop up the end of the first loop bar 201, a part can be enclosed within outside installation portion 103 and horn 102, block 301 is made to encase installation portion 103 and the junction of horn 102, make connection more firm, and make inner connecting structure more safe and reliable.
Ball 303 it is provided with between the outer wall of block 301 and installation portion 103.By arranging ball 303, it is possible to anti-stop block 301, with installation portion 103, axially opposing movement occurs, and it is more firm to connect.
nullRefer to Fig. 1～Fig. 8，The unmanned plane that the present embodiment provides is when being connected horn 102 with the installation portion 103 of fuselage 101，The annular protrusion 105 of installation portion 103 and block 301 are by the first loop bar 201 and the second loop bar 202 clamping，First loop bar 201 and the second loop bar 202 are by the first fixture block 203 and the second fixture block 204 clamping，And，First fixture block 203 and the second fixture block 204 coordinate clamping again through the cooperation of boss 209 and link slot 210 and bar blocks 211 and bar-shaped trough 212，The connection making horn 102 and fuselage 101 is firm，Bonding strength is higher，And the first fixture block 203 and the second fixture block 204 are respectively triangular prism shaped，And it is respectively embedded into the first draw-in groove 205 and the second draw-in groove 206，Effectively restriction horn 102 twists，Make horn 102 and fuselage 101 junction more firm，It is hardly damaged.
In sum, the horn 102 of the unmanned plane that the present embodiment provides is removably connected by connector with the installation portion 103 of fuselage 101, both ensure that the bonding strength of horn 102 and fuselage 101, horn 102 can be made again can to pull down from fuselage 101, it is easy to maintenance, horn 102 or the repeatable utilization of fuselage 101, saves cost, also enhance the portability of this unmanned plane, it is possible to horn 102 is disassembled and puts in the knapsack that volume is slightly smaller.
In description of the present utility model, it will be appreciated that, term " on ", D score, "front", "rear", "left", "right", " interior ", the orientation of the instruction such as " outward " or position relationship be based on orientation shown in the drawings or position relationship, it is for only for ease of description this utility model and simplifies description, rather than the equipment of instruction or hint indication or element must have specific orientation, with specific azimuth configuration and operation, therefore it is not intended that to restriction of the present utility model.
Additionally, term " first ", " second " are only for descriptive purposes, and it is not intended that indicate or imply relative importance or the implicit quantity indicating indicated technical characteristic.Thus, define " first ", the feature of " second " can express or implicitly include one or more these features.In description of the present utility model, " multiple " are meant that two or more, unless otherwise expressly limited specifically.
In this utility model, unless otherwise clearly defined and limited, the term such as term " installation ", " being connected ", " connection ", " fixing " should be interpreted broadly, for instance, it is possible to it is fixing connection, it is also possible to be removably connect, or integral；Can be mechanically connected, it is also possible to be electrical connection；Can be joined directly together, it is also possible to be indirectly connected to by intermediary, it is possible to be connection or the interaction relationship of two elements of two element internals.For the ordinary skill in the art, it is possible to understand above-mentioned term concrete meaning in this utility model as the case may be.
In this utility model, unless otherwise clearly defined and limited, fisrt feature second feature it " on " or D score can include the first and second features and directly contact, it is also possible to include the first and second features and be not directly contact but by the other characterisation contact between them.And, fisrt feature second feature " on ", " top " and " above " include fisrt feature directly over second feature and oblique upper, or be merely representative of fisrt feature level height higher than second feature.Fisrt feature second feature " under ", " lower section " and " below " include fisrt feature immediately below second feature and obliquely downward, or be merely representative of fisrt feature level height less than second feature.
The foregoing is only preferred embodiment of the present utility model, be not limited to this utility model, for a person skilled in the art, this utility model can have various modifications and variations.All within spirit of the present utility model and principle, any amendment of making, equivalent replacement, improvement etc., should be included within protection domain of the present utility model.
Claims (10)
1. the dismountable unmanned plane of horn, it is characterized in that, including fuselage and horn, described fuselage is provided with installation portion, being provided with driving device on described horn, described horn is removably connected by connector and described installation portion away from one end of described driving device.
2. the dismountable unmanned plane of horn according to claim 1, it is characterized in that, described connector includes the first connector, described first connector is arranged in described horn, described first connector includes the first loop bar and the second loop bar, described first loop bar is connected with described horn, and described second loop bar is connected with described installation portion, and described first loop bar and described second loop bar are connected with each other.
3. the dismountable unmanned plane of horn according to claim 2, it is characterised in that described first connector also includes the first fixture block and the second fixture block；
One end of described first loop bar is provided with the first draw-in groove, and described first fixture block embeds in described first draw-in groove, described first loop bar and described horn clamping；
One end of described second loop bar is provided with the second draw-in groove, and described second fixture block embeds in described second draw-in groove, described second loop bar and described installation portion clamping, described first fixture block and described second fixture block clamping.
4. the dismountable unmanned plane of horn according to claim 3, it is characterized in that, described first fixture block is multi-edge column-shaped, second fixture block is and the multi-edge column-shaped of described first card Block-matching, the cell wall of described first draw-in groove mates with the outer wall of described first fixture block, and the cell wall of described second draw-in groove mates with the outer wall of described second fixture block.
5. the dismountable unmanned plane of horn according to claim 4, it is characterized in that, first groove being circumferentially provided with multiple strip of described first loop bar, described first groove is arranged along the direction being parallel to described first set rod axis, and described first groove connects with described first draw-in groove；
Second groove being circumferentially provided with multiple strip of described second loop bar, described second groove extends along the direction being parallel to described second set rod axis, and described second groove connects with described second draw-in groove.
6. the dismountable unmanned plane of horn according to claim 3, it is characterized in that, described first fixture block is provided with boss, described second fixture block is provided with link slot, described boss is provided with bar-shaped trough, being provided with bar blocks on the cell wall of described link slot, described boss coordinates with described link slot, and described bar blocks coordinates with described bar-shaped trough.
7. the dismountable unmanned plane of horn according to claim 2, it is characterized in that, described connector includes the second connector, and described second connector includes block, and described block is set in the junction of described installation portion and described horn and props up the end of described first loop bar.
8. the dismountable unmanned plane of horn according to claim 7, it is characterised in that be provided with ball between the outer wall of described block and described installation portion.
9. the dismountable unmanned plane of horn according to claim 8, it is characterised in that described second connector also includes sleeve, and described sleeve is set in outside described block.
10. the dismountable unmanned plane of horn according to claim 2, it is characterized in that, described first loop bar is provided with the first card article, described second loop bar is provided with the second card article, described first card article and described horn clamping, described second card article and described installation portion clamping.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620179378.7U CN205396528U (en) | 2016-03-09 | 2016-03-09 | Horn detachable unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620179378.7U CN205396528U (en) | 2016-03-09 | 2016-03-09 | Horn detachable unmanned aerial vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205396528U true CN205396528U (en) | 2016-07-27 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201620179378.7U Expired - Fee Related CN205396528U (en) | 2016-03-09 | 2016-03-09 | Horn detachable unmanned aerial vehicle |
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Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105691605A (en) * | 2016-03-09 | 2016-06-22 | 深圳行天者创新技术有限公司 | Unmanned aerial vehicle with detachable vehicle arms |
| CN106741821A (en) * | 2016-12-28 | 2017-05-31 | 中国航天电子技术研究院 | A kind of quick-connect mechanism |
| CN106828863A (en) * | 2017-03-28 | 2017-06-13 | 深圳市创客火科技有限公司 | The Multi-axis aircraft that can freely assemble |
| CN109804995A (en) * | 2019-01-31 | 2019-05-28 | 安徽梦之翼无人机科技有限公司 | A kind of novel agricultural plant protection drone |
-
2016
- 2016-03-09 CN CN201620179378.7U patent/CN205396528U/en not_active Expired - Fee Related
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105691605A (en) * | 2016-03-09 | 2016-06-22 | 深圳行天者创新技术有限公司 | Unmanned aerial vehicle with detachable vehicle arms |
| CN105691605B (en) * | 2016-03-09 | 2018-02-23 | 深圳潜行创新科技有限公司 | A kind of dismountable unmanned plane of horn |
| CN106741821A (en) * | 2016-12-28 | 2017-05-31 | 中国航天电子技术研究院 | A kind of quick-connect mechanism |
| CN106828863A (en) * | 2017-03-28 | 2017-06-13 | 深圳市创客火科技有限公司 | The Multi-axis aircraft that can freely assemble |
| CN109804995A (en) * | 2019-01-31 | 2019-05-28 | 安徽梦之翼无人机科技有限公司 | A kind of novel agricultural plant protection drone |
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| 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: 20160727 Termination date: 20170309 |