CN205418056U - Unmanned aerial vehicle of unmanned aerial vehicle shell and applied this unmanned aerial vehicle shell - Google Patents
Unmanned aerial vehicle of unmanned aerial vehicle shell and applied this unmanned aerial vehicle shell Download PDFInfo
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- CN205418056U CN205418056U CN201620251774.6U CN201620251774U CN205418056U CN 205418056 U CN205418056 U CN 205418056U CN 201620251774 U CN201620251774 U CN 201620251774U CN 205418056 U CN205418056 U CN 205418056U
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- upper cover
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- 229910052751 metal Inorganic materials 0.000 claims description 15
- 239000002184 metal Substances 0.000 claims description 15
- 235000019994 cava Nutrition 0.000 claims description 3
- 238000009434 installation Methods 0.000 abstract description 4
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 4
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 description 4
- 238000010521 absorption reaction Methods 0.000 description 3
- PWHULOQIROXLJO-UHFFFAOYSA-N Manganese Chemical compound [Mn] PWHULOQIROXLJO-UHFFFAOYSA-N 0.000 description 2
- 229910017052 cobalt Inorganic materials 0.000 description 2
- 239000010941 cobalt Substances 0.000 description 2
- GUTLYIVDDKVIGB-UHFFFAOYSA-N cobalt atom Chemical compound [Co] GUTLYIVDDKVIGB-UHFFFAOYSA-N 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 238000005194 fractionation Methods 0.000 description 2
- 229910052742 iron Inorganic materials 0.000 description 2
- 229910052748 manganese Inorganic materials 0.000 description 2
- 239000011572 manganese Substances 0.000 description 2
- 238000004519 manufacturing process Methods 0.000 description 2
- 230000013011 mating Effects 0.000 description 2
- 239000007769 metal material Substances 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 229910052759 nickel Inorganic materials 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
- 230000000007 visual effect Effects 0.000 description 1
- 239000002699 waste material Substances 0.000 description 1
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Abstract
The utility model provides an unmanned aerial vehicle of unmanned aerial vehicle shell and applied this unmanned aerial vehicle shell relates to unmanned airborne vehicle field. This unmanned aerial vehicle shell includes fuselage casing and upper cover, and the upper cover sets up first fitting piece, the fuselage casing be provided with with first fitting piece complex second fitting piece, upper cover and fuselage casing adsorb through first fitting piece and second fitting piece and/or the mode of lock combines. Adopt magnet to adsorb or the buckle carries out the lock, has improved the installation rate of unmanned aerial vehicle's upper cover yu fuselage casing, when setting up a set of magnet and a set of buckle and carrying out being connected of upper cover and fuselage casing, convenience that can also be better, firmly makes upper cover and the combination of fuselage casing. The equipment of unmanned aerial vehicle shell is inconvenient in having improved prior art to reach the problem that causes unmanned aerial vehicle mass addition easily.
Description
Technical field
The utility model relates to unmanned airborne vehicle technical field, in particular to a kind of unmanned plane shell and the unmanned plane of applying this unmanned plane shell.
Background technology
At present, small-sized many rotor wing unmanned aerial vehicles taking photo by plane, rescue, forest fire protection, a lot of fields such as security protection are widely used.Urgent special occasions or client that the time is taken notice of very much, it is desirable to unmanned plane is capable of quickly assembling, with time-consuming.Common unmanned plane upper cover and the assembling mode of body, have screw fixed, lace-type etc., and these fixed forms easily cause the increase of the quality of unmanned plane, installs simultaneously and typically requires instrument, brings unnecessary trouble to client, and waste valuable time.
Utility model content
In view of this, the utility model provides a kind of unmanned plane shell and applies the unmanned plane of this unmanned plane shell, to improve unmanned plane shell assembling inconvenience in prior art, and easily causes the problem that unmanned plane quality increases.
For achieving the above object, the following technical scheme of the utility model offer:
A kind of unmanned plane shell, including body shell and upper cover, described upper cover arranges the first counterpart, described body shell is provided with the second counterpart coordinated with the first counterpart, described upper cover and described body shell and is adsorbed with described second counterpart by described first counterpart and/or combine by the way of fastening.
Use magnet to carry out adsorbing or buckle fasten, improve the upper cover of unmanned plane and the speed that is engaged of body shell, and can also preferably facilitate, the upper cover that makes that consolidates is combined with body shell.
Preferably, described first counterpart is the first magnet, and described second counterpart is the second magnet or magnetic metal.
Magnetic metal can also attract each other with magnet, and such as iron, cobalt, nickel, manganese etc., also can make upper cover be combined with body shell further.
Preferably, described first counterpart includes that the first magnet and buckle, described second counterpart include the second magnet or magnetic metal and draw-in groove, described first magnet and the second magnet or magnetic metal absorption, described buckle fastens with draw-in groove, and described buckle is " L " shape buckle.
One group of magnet is set and one group of buckle carries out the connection of upper cover and body shell, can easily, the firm upper cover that makes is combined with body shell.
Preferably, the number of described first counterpart is two, and said two the first counterpart is respectively arranged at the two ends of described upper cover.
Preferably, substantially symmetrical about its central axis along described upper cover of two described first counterparts.
Preferably, described upper cover includes inner surface and the outer surface opposed with described inner surface, and described inner surface is convexly equipped with at least one projection, and the middle part of described projection caves inward, and forms fixing groove, and described first magnet is arranged in described fixing groove.
Preferably, described body shell is provided with groove, and described second magnet or magnetic metal are arranged in described groove.
Preferably, described upper cover is additionally provided with multiple alignment pin, and described body shell is provided with the hole, location mated with described alignment pin.
Described alignment pin is to facilitate described upper cover to fasten more efficiently and described body shell with the effect in hole, described location, improves operating efficiency, reduces and fastens difficulty.Moreover, alignment pin inserts behind hole, described location and described upper cover can also be made more firm, prevent unmanned plane in flight course, the situation of upper cover landing.
Preferably, described upper cover is arc upper cover, and described upper cover includes that outer surface and inner surface, described outer surface are streamlined outer surface.So can improve the flying speed of unmanned plane, reduce air drag.
The utility model also provides for a kind of unmanned plane, and it includes above-mentioned unmanned plane shell.
Relative to prior art, the utility model includes following beneficial effect:
The unmanned plane shell that the utility model provides includes body shell and upper cover, upper cover arranges the first counterpart, body shell is provided with the second counterpart coordinated with the first counterpart, upper cover and body shell and is adsorbed by the first counterpart and the second counterpart and/or combine by the way of fastening.
Use magnet to carry out adsorbing or buckle fastens, improve the upper cover of unmanned plane and the installation rate of body shell, one group of magnet is set and time one group of buckle carries out the connection of upper cover and body shell, moreover it is possible to be the most convenient, consolidate and make upper cover be combined with body shell.Improve unmanned plane shell in prior art and assemble inconvenience, and easily cause the problem that unmanned plane quality increases.
Accompanying drawing explanation
For clearer explanation the utility model embodiment or technical scheme of the prior art, the accompanying drawing used required in embodiment or description of the prior art will be briefly described below, apparently, accompanying drawing in describing below is only embodiments more of the present utility model, for those of ordinary skill in the art, on the premise of not paying creative work, it is also possible to obtain other accompanying drawing according to these accompanying drawings.
Fig. 1 is the fractionation structural representation of the unmanned plane shell that the utility model embodiment one provides；
Fig. 2 is the structural representation of the upper cover of the unmanned plane shell that the utility model embodiment one provides；
Fig. 3 is another viewing angle constructions schematic diagram of the upper cover of the unmanned plane shell that the utility model embodiment one provides；
Fig. 4 is the structural representation at the another visual angle of the upper cover of the unmanned plane shell that the utility model embodiment one provides；
Fig. 5 is the structural representation of the body shell of the unmanned plane shell that the utility model embodiment one provides；
Fig. 6 is the structural representation of the upper cover of the unmanned plane shell that the utility model embodiment two provides；
Fig. 7 is the structural representation of the body shell of the unmanned plane shell that the utility model embodiment two provides.
Wherein reference is summarized as follows:
Unmanned plane shell 10；Upper cover 100；Projection 101；Fixing groove 102；Buckle 103；Alignment pin 104；Inner surface 105；Outer surface 106；First magnet 107；Body shell 200；Groove 201；Draw-in groove 202；Hole 203, location；Second magnet 204.
Detailed description of the invention
Below in conjunction with accompanying drawing in the utility model embodiment, the technical scheme in the utility model embodiment is clearly and completely described, it is clear that described embodiment is only a part of embodiment of the utility model rather than whole embodiments.Generally can with various different configurations arrange and design with the assembly of the utility model embodiment that illustrate described in accompanying drawing herein.Therefore, the detailed description to the embodiment of the present utility model provided in the accompanying drawings is not intended to limit claimed scope of the present utility model below, but is merely representative of selected embodiment of the present utility model.Based on embodiment of the present utility model, the every other embodiment that those skilled in the art are obtained on the premise of not making creative work, broadly fall into the scope of the utility model protection.
Embodiment one
Refer to Fig. 1, be the fractionation structural representation of the unmanned plane shell 10 that the utility model embodiment provides.The unmanned plane shell that the utility model provides is applied to unmanned plane.This unmanned plane shell 10 includes that body shell 200 and upper cover 100, described body shell 200 and described upper cover 100 use the dismountable connection of mode of absorption.
Refer to the structural representation that Fig. 2 to Fig. 4, Fig. 2 to Fig. 4 are the upper covers 100 of the unmanned plane shell 10 that the present embodiment provides.The upper cover 100 of the unmanned plane shell 10 of the utility model embodiment includes inner surface 105 and the outer surface 106 relative with this inner surface 105, described inner surface 105 is convexly equipped with two projections 101, the middle part of described projection 101 caves inward, form fixing groove 102, in described fixing groove 102, be provided with the first magnet 107.
Concrete, upper cover 100 includes two ends, and said two projection 101 is respectively arranged at two ends of the inner surface 105 of upper cover 100, and substantially symmetrical about its central axis approximately along upper cover 100, and the upper cover 100 that makes that so can more consolidate is connected with body shell 200.Certainly, the position that said two projection 101 is not limited solely to about upper cover 100 is substantially symmetrical about its central axis is arranged.The projection 101 of the present embodiment and the number of the first magnet 107 are two, and in other detailed description of the invention, the number of projection 101 and the first magnet 107 can also be other, such as 1,3,4 etc..
Refer to the structural representation that Fig. 1 and Fig. 5, Fig. 5 are the body shells 200 of the unmanned plane shell 10 that the present embodiment provides.Described body shell 200 is provided with two grooves 201, and the position of said two groove 201 is the most corresponding with the position of said two projection 101, and this groove 201 is used for accommodating described projection 101.Can arrange the second magnet 204 in the bottom of described groove 201, there is a natural attraction between the sexes with the first magnet 107, makes upper cover 100 be adsorbed on described body shell 200.
Can also arrange magnetic metal in the bottom of groove 201, such as iron, cobalt, nickel, manganese etc., can also make upper cover 100 be combined with body shell 200 equally.Certainly, the material of described groove 201 can also use magnetic metal or magnet.So, it may not be necessary in groove 201, increase by the second magnet 204 or magnetic metal again, reduce manufacture craft, reduce production cost.
Moreover, in other detailed description of the invention, can be to place magnetic metal in described fixing groove 102, or fixing groove 102 uses magnetic metal material.Relative, magnet can be placed bottom groove 201.Combine this manner it is also possible to realize described upper cover 100 with described body shell 200.
It should be noted that, the first above-mentioned magnet 107 or the fixing groove 102 using magnetic metal material to make may be collectively referred to as the first counterpart, the second above-mentioned magnet 204, the groove 201 using magnetic metal or magnet to make or the magnetic metal being arranged in groove 201 and may be collectively referred to as the second counterpart.
Described upper cover 100 is additionally provided with alignment pin 104, and in the present embodiment, alignment pin 104 is arranged at described inner surface 105.Corresponding, described body shell 200 is provided with hole 203, location, is used for accommodating described alignment pin 104, and number, the size in described alignment pin 104 and hole, described location 203 match.
In the present embodiment, described alignment pin 104 be shaped as cylindrical, hole, described location 203 is manhole or blind round hole.The number of described alignment pin 104 is 4, and in other detailed description of the invention, the number of described alignment pin 104 can also be other, such as 1,2,3,5 etc..
Described alignment pin 104 is to facilitate described upper cover 100 to fasten more efficiently and described body shell 200 with the effect in hole, described location 203, improves operating efficiency, reduces and fasten difficulty.Moreover, alignment pin 104 can also make described upper cover 100 more firm after inserting hole, described location 203, prevent unmanned plane in flight course, the situation of upper cover 100 landing.
In order to improve the flying speed of unmanned plane, reducing air drag, described upper cover 100 is arc upper cover 100, and its outer surface 106 uses streamlined.
Embodiment two
Refer to the structural representation that Fig. 6 and Fig. 7, Fig. 6 are the upper covers 100 of the unmanned plane shell 10 that the utility model embodiment two provides；Fig. 7 is the structural representation of the body shell 200 of the unmanned plane shell 10 that the utility model embodiment two provides.The unmanned plane shell 10 that the present embodiment provides is with the difference of embodiment one, and the upper cover 100 of the utility model embodiment is connected with the mode not only through absorption of body shell 200, but also connects by the way of buckle.
In the present embodiment, it is respectively provided with a projection 101 at the two ends of upper cover 100, fixing groove 102 is set in projection 101, in fixing groove 102, be provided with the first magnet 107.Further, being additionally provided with buckle 103 in wherein one end of upper cover 100, in the present embodiment, the number of described buckle 103 is two, and certainly, in other detailed description of the invention, the number of buckle 103 can also be other, such as 1,3 etc..Said two buckle 103 is disposed therein the both sides of a projection 101.
The corresponding of described body shell 200 is provided with two grooves 201, the second magnet 204 it is provided with in groove 201, the position of said two groove 201 is corresponding with the position of described projection 101, the both sides of one of them groove 201 are provided with two draw-in grooves 202, for being connected with described buckle 103, after making described upper cover 100 fixing with described body shell 200, consolidate further.
The buckle 103 of the present embodiment is " L " shape buckle, corresponding, include the catch making described " L " shape buckle fixing in draw-in groove 202.
It should be noted that above-mentioned buckle 103 can be also referred to as the first counterpart, above-mentioned draw-in groove 202 is referred to as the second counterpart.
In other detailed description of the invention, it is also possible to arrange projection 101 in one end of upper cover 100, the other end arranges buckle 103.Corresponding, in one end of the correspondence position of body shell 200, groove 201 is set, the other end arranges draw-in groove 202.During use, first buckle 103 is snapped in draw-in groove 202, then projection 101 is put into groove 201, make the first magnet 107 in projection 101 attract each other with the second magnet 204 in groove 201, be connected so that upper cover 100 is dismountable with body shell 200.So, upper cover 100 and body shell 200 not only can be made quickly to fasten, and fasten more closely, firmly.
It is possible that, it being respectively provided with buckle 103 at the two ends of upper cover 100, the position corresponding at the two ends of body shell 200 arranges two draw-in grooves 202, by mating of buckle 103 and draw-in groove 202, makes upper cover 100 be combined with described body shell 200.
Certainly, it is also possible that, it is respectively provided with buckle 103 at the two ends of upper cover 100, one end wherein arranges a projection 101 again, the position corresponding at the two ends of body shell 200 arranges two draw-in grooves 202, by mating of buckle 103 and draw-in groove 202, upper cover 100 is made to be combined with described body shell 200, one end that body shell 200 is corresponding with described projection 101 is provided with groove 201, can be attracted each other with the second magnet 204 in groove 201, so that upper cover 100 is fixed further with body shell 200 by the first magnet 107 in projection 101.
In sum, the unmanned plane shell 10 that the utility model provides includes body shell 200 and upper cover 100, use magnet to carry out adsorbing or buckle fastens, make that upper cover 100 is dismountable with body shell 200 to be connected, improve the upper cover 100 of unmanned plane and the installation rate of body shell 200, one group of magnet is set and time one group of buckle carries out the connection of upper cover 100 and body shell 200, moreover it is possible to the most convenient, firm make upper cover 100 be combined with body shell 200.Improve unmanned plane shell in prior art and assemble inconvenience, and easily cause the problem that unmanned plane quality increases.
The foregoing is only preferred embodiment of the present utility model, be not limited to the utility model, for a person skilled in the art, the utility model can have various modifications and variations.All within spirit of the present utility model and principle, any modification, equivalent substitution and improvement etc. made, within should be included in protection domain of the present utility model.It should also be noted that similar label and letter represent similar terms in following accompanying drawing, therefore, the most a certain Xiang Yi accompanying drawing is defined, then need not it be defined further and explains in accompanying drawing subsequently.
In description of the present utility model, it should be noted that, term " " center ", on " ", D score, " left ", " right ", " vertically ", " level ", " interior ", orientation or the position relationship of the instruction such as " outward " are based on orientation shown in the drawings or position relationship, or this utility model product orientation usually put or position relationship when using, it is for only for ease of description the utility model and simplifies description, rather than indicate or imply that the device of 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.
In description of the present utility model, in addition it is also necessary to explanation, unless otherwise clearly defined and limited, term " is arranged ", " installation ", " being connected ", " connection " should be interpreted broadly, and connects for example, it may be fixing, can also be to removably connect, or be integrally connected；Can be to be mechanically connected, it is also possible to be electrical connection；Can be to be joined directly together, it is also possible to be indirectly connected to by intermediary, can be the connection of two element internals.For the ordinary skill in the art, above-mentioned term concrete meaning in the utility model can be understood with concrete condition.
Claims (10)
1. a unmanned plane shell, it is characterized in that, including body shell and upper cover, described upper cover arranges the first counterpart, described body shell is provided with the second counterpart coordinated with the first counterpart, described upper cover and described body shell and is adsorbed with described second counterpart by described first counterpart and/or combine by the way of fastening.
Unmanned plane shell the most according to claim 1, it is characterised in that described first counterpart is the first magnet, described second counterpart is the second magnet or magnetic metal.
Unmanned plane shell the most according to claim 1, it is characterized in that, described first counterpart includes the first magnet and buckle, described second counterpart includes the second magnet or magnetic metal and draw-in groove, described first magnet and the second magnet or magnetic metal adsorb, described buckle fastens with draw-in groove, and described buckle is " L " shape buckle.
4., according to the unmanned plane shell described in Claims 2 or 3, it is characterised in that the number of described first counterpart is two, said two the first counterpart is respectively arranged at the two ends of described upper cover.
Unmanned plane shell the most according to claim 4, it is characterised in that substantially symmetrical about its central axis along described upper cover of two described first counterparts.
6. according to the unmanned plane shell described in Claims 2 or 3, it is characterized in that, described upper cover includes inner surface and the outer surface opposed with described inner surface, described inner surface is convexly equipped with at least one projection, the middle part of described projection caves inward, forming fixing groove, described first magnet is arranged in described fixing groove.
Unmanned plane shell the most according to claim 6, it is characterised in that described body shell is provided with groove, described second magnet or magnetic metal are arranged in described groove.
Unmanned plane shell the most according to claim 1, it is characterised in that described upper cover is additionally provided with multiple alignment pin, described body shell is provided with the hole, location mated with described alignment pin.
Unmanned plane shell the most according to claim 1, it is characterised in that described upper cover is arc upper cover, described upper cover includes that outer surface and inner surface, described outer surface are streamlined outer surface.
10. a unmanned plane, it is characterised in that include the unmanned plane shell as described in any one of claim 1-9.
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620251774.6U CN205418056U (en) | 2016-03-29 | 2016-03-29 | Unmanned aerial vehicle of unmanned aerial vehicle shell and applied this unmanned aerial vehicle shell |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620251774.6U CN205418056U (en) | 2016-03-29 | 2016-03-29 | Unmanned aerial vehicle of unmanned aerial vehicle shell and applied this unmanned aerial vehicle shell |
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| Publication Number | Publication Date |
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| CN205418056U true CN205418056U (en) | 2016-08-03 |
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| CN201620251774.6U Active CN205418056U (en) | 2016-03-29 | 2016-03-29 | Unmanned aerial vehicle of unmanned aerial vehicle shell and applied this unmanned aerial vehicle shell |
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Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2018188188A1 (en) * | 2017-04-10 | 2018-10-18 | 深圳市大疆创新科技有限公司 | Upper cover of unmanned aerial vehicle and unmanned aerial vehicle |
| CN109319085A (en) * | 2017-08-01 | 2019-02-12 | 广州极飞科技有限公司 | Based shell, rack and unmanned plane |
| CN109319104A (en) * | 2017-08-01 | 2019-02-12 | 广州极飞科技有限公司 | A kind of unmanned plane |
| WO2019041875A1 (en) * | 2017-08-30 | 2019-03-07 | 深圳市道通智能航空技术有限公司 | Foldable frame and unmanned aerial vehicle |
| WO2019205457A1 (en) * | 2018-04-24 | 2019-10-31 | 深圳市大疆创新科技有限公司 | Unmanned aerial vehicle |
| US20200156789A1 (en) * | 2017-08-01 | 2020-05-21 | Guangzhou Xaircraft Technology Co.,Ltd. | Unmanned aerial vehicle |
| CN109319104B (en) * | 2017-08-01 | 2024-07-05 | 广州极飞科技股份有限公司 | Unmanned aerial vehicle |
-
2016
- 2016-03-29 CN CN201620251774.6U patent/CN205418056U/en active Active
Cited By (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2018188188A1 (en) * | 2017-04-10 | 2018-10-18 | 深圳市大疆创新科技有限公司 | Upper cover of unmanned aerial vehicle and unmanned aerial vehicle |
| CN109789919A (en) * | 2017-04-10 | 2019-05-21 | 深圳市大疆创新科技有限公司 | The upper cover and unmanned plane of unmanned plane |
| CN109319085A (en) * | 2017-08-01 | 2019-02-12 | 广州极飞科技有限公司 | Based shell, rack and unmanned plane |
| CN109319104A (en) * | 2017-08-01 | 2019-02-12 | 广州极飞科技有限公司 | A kind of unmanned plane |
| US20200156789A1 (en) * | 2017-08-01 | 2020-05-21 | Guangzhou Xaircraft Technology Co.,Ltd. | Unmanned aerial vehicle |
| CN109319104B (en) * | 2017-08-01 | 2024-07-05 | 广州极飞科技股份有限公司 | Unmanned aerial vehicle |
| WO2019041875A1 (en) * | 2017-08-30 | 2019-03-07 | 深圳市道通智能航空技术有限公司 | Foldable frame and unmanned aerial vehicle |
| WO2019205457A1 (en) * | 2018-04-24 | 2019-10-31 | 深圳市大疆创新科技有限公司 | Unmanned aerial vehicle |
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Date of cancellation: 20221008 Granted publication date: 20160803 Pledgee: XinDa national equity investment fund (Shanghai) partnership (L.P.)|Beijing Civil Aviation Heyuan Investment Center (L.P.) Pledgor: ZEROTECH (BEIJING) INTELLIGENCE TECHNOLOGY Co.,Ltd. Registration number: 2017990000242 |
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