CN206569281U - Unmanned vehicle - Google Patents
Unmanned vehicle Download PDFInfo
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- CN206569281U CN206569281U CN201720235792.XU CN201720235792U CN206569281U CN 206569281 U CN206569281 U CN 206569281U CN 201720235792 U CN201720235792 U CN 201720235792U CN 206569281 U CN206569281 U CN 206569281U
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- fixing device
- component
- unmanned vehicle
- head assembly
- aircraft body
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Abstract
The utility model discloses a kind of unmanned vehicle, wherein the unmanned vehicle includes aircraft body and head assembly, the top of the aircraft body is provided with fixing device, the bottom of the aircraft body passes component provided with figure, and the head assembly is connected to the fixing device or the figure is passed on component.Unmanned vehicle of the present utility model can be easy to detect top target, increase the scope of detection and use scope.
Description
Technical field
The utility model is related to vehicle technology field, more particularly to a kind of unmanned vehicle.
Background technology
The head of current unmanned vehicle is placed in fuselage bottom, and the detection carried out to the target below fuselage can be achieved,
But also detected for the target above unmanned vehicle without proper method.Such as detected for bridge bottom, and its
He is needed at the application of detection top target, causes that top target can not be detected with this, and detection has limitation.
Utility model content
Main purpose of the present utility model is to provide a kind of unmanned vehicle, it is intended to can be easy to visit top target
Survey, increase the scope of detection and use scope.
To achieve the above object, the utility model proposes a kind of unmanned vehicle, the unmanned vehicle includes aircraft sheet
Body and head assembly, the top of the aircraft body are provided with fixing device, and the bottom of the aircraft body is provided with figure biography group
Part, the head assembly is connected to the fixing device or the figure is passed on component.
Preferably, in addition at least one locking member, the locking member and the fixing device and the aircraft body
Connection.
Preferably, the fixing device includes at least one extension abutted against with the aircraft body, the lock
Tight part connects the extension.
Preferably, in addition to connecting wire, the figure, which passes component, includes the connector located at the aircraft body, described
One end of connecting wire is electrically connected with the connector, when the head assembly connects the fixing device, the connecting wire
The other end electrically connected with the head assembly.
Preferably, in addition to it is respectively arranged at the top of the fixing device and the figure passes the latch assembly of component bottom, institute
Head assembly is stated to be detachably connected with the fixing device or figure biography component by the latch assembly.
Preferably, the latch assembly includes fastener and locating part, fixed dress described in the fastener slidable connection
Put or the figure passes one end of component, the locating part is fixedly connected at the top of the fixing device or the figure passes component bottom
The other end, forms a holding area between the fastener and the locating part, the head assembly is fastened on the accommodating area
In domain.
Preferably, the fastener includes Flexible Connector and holding section, and described Flexible Connector one end connects the card
Conjunction portion, the other end connects the fixing device or figure passes component, and an accommodating area is formed between the holding section and the locating part
Domain.
Preferably, the locating part is plate washer, snap fit or elastic card component.
Technical solutions of the utility model are by the fixing device at the top of aircraft body and located at aircraft body bottom
The figure in portion passes component, and head assembly is fixedly arranged on fixing device or figure passes component, make head assembly may be selected located at fixing device or
Figure is passed on component, is made the structure of the aircraft body simpler with this, can be easy to detect top target, increase detection
Scope and use scope.
Brief description of the drawings
, below will be to embodiment in order to illustrate more clearly of the utility model embodiment or technical scheme of the prior art
Or the accompanying drawing used required in description of the prior art is briefly described, it should be apparent that, drawings in the following description are only
It is some embodiments of the present utility model, for those of ordinary skill in the art, is not paying the premise of creative work
Under, other accompanying drawings can also be obtained according to the structure shown in these accompanying drawings.
Fig. 1 is the main structure diagram of the embodiment of the utility model unmanned vehicle one；
Fig. 2 is the left view structural representation of Fig. 1 unmanned vehicles；
Fig. 3 is the decomposition texture schematic diagram of Fig. 2 unmanned vehicles；
Fig. 4 is the overlooking the structure diagram of Fig. 1 unmanned vehicles；
Fig. 5 is the main structure diagram of another embodiment of the utility model unmanned vehicle；
Fig. 6 is the part section structural representation of Fig. 5 unmanned vehicles.
Drawing reference numeral explanation：
Realization, functional characteristics and the advantage of the utility model purpose will be described further referring to the drawings in conjunction with the embodiments.
Embodiment
Below in conjunction with the accompanying drawing in the utility model embodiment, the technical scheme in the utility model embodiment is carried out
Clearly and completely describe, it is clear that described embodiment is only a part of embodiment of the present utility model, rather than all
Embodiment.Based on the embodiment in the utility model, those of ordinary skill in the art are not making creative work premise
Lower obtained every other embodiment, belongs to the scope of the utility model protection.
It is to be appreciated that institute is directional in the utility model embodiment indicates (such as up, down, left, right, before and after ...)
Relative position relation, motion conditions for being only used for explaining under a certain particular pose (as shown in drawings) between each part etc., such as
When really the particular pose changes, then directionality indicates also correspondingly therewith to change.
In the utility model, unless otherwise clearly defined and limited, term " connection ", " fixation " etc. should do broad sense reason
Solution, for example, " fixation " can be fixedly connected or be detachably connected, or integrally；Can mechanically connect, also may be used
Be electrical connection；Can be joined directly together, can also be indirectly connected to by intermediary, can be the connection of two element internals
Or the interaction relationship of two elements, unless otherwise clear and definite restriction.For the ordinary skill in the art, can be with
Concrete meaning of the above-mentioned term in the utility model is understood as the case may be.
In addition, and can not be managed in the utility model such as relating to the description of " first ", " second " etc. is only used for describing purpose
Solve to indicate or imply its relative importance or the implicit quantity for indicating indicated technical characteristic.Thus, define " the
One ", at least one this feature can be expressed or be implicitly included to the feature of " second ".In addition, the skill between each embodiment
Art scheme can be combined with each other, but must can be implemented as basis with those of ordinary skill in the art, when technical scheme
With reference to occur it is conflicting or when can not realize it will be understood that the combination of this technical scheme is not present, also not in the utility model
It is required that protection domain within.
The utility model proposes a kind of unmanned vehicle.
Referring to figs. 1 to Fig. 3, in the embodiment of the utility model one, the unmanned vehicle includes aircraft body 10 and cloud
Platform component 20, the top of aircraft body 10 is provided with fixing device 30, and the bottom of aircraft body 10 passes component 40, cloud provided with figure
Platform component 20 is connected to fixing device 30 or figure is passed on component 40.
Above-mentioned aircraft body 10 includes fuselage, the foot stool located at fuselage and horn component, and horn component includes multiple
Propeller.Video camera is installed on head assembly 20 therein, for monitoring objective, head assembly 20 is used to ensure video camera not
Shake, control shooting angle, such as control video camera carry out 360 ° rotation, pitching and level operation, strengthen shoot quality with
Monitor angular field of view.One embodiment is that head assembly 20 is placed in the top of aircraft body 10, for the target above detection, makes
Head assembly 20 is connected more stable with aircraft body 10, and structure is simpler；Another embodiment is that head assembly 20 is filled with fixed
Put 30 to be integrally formed, the other end of fixing device 30 can be connected by modes such as bolt, buckles with aircraft body 10, or fixed dress
Put 30 to be integrally formed with aircraft body 10, it is preferable that fixing device 30 is removably connected to aircraft body 10, with this is easy to
Fixing device 30 is changed or removed, when head assembly 20 located at figure pass component 40 detected below target in use, can will consolidate
Determine device 30 to be dismantled, mitigate the overall weight of the unmanned vehicle with this, extend the flight time.To sum up make the unmanned flight
Device single can possess the overhead of head assembly 20 in aircraft body 10, or selectable head assembly 20 is located at into fixing device 30
Or figure is passed on component 40, or head assembly 20 is two, and each head assembly 20 is equipped with a video camera, two 20 points of head assemblies
Not She Yu fixing device 30 and figure pass component 40 on, make the unmanned vehicle alternative detection above or below objective function,
Or be provided simultaneously with to lower section target and top target acquisition function, the scope of unmanned vehicle detection is increased with this and model is used
Enclose.
Technical solutions of the utility model are by the fixing device 30 located at the top of aircraft body 10 and located at aircraft sheet
The figure of the bottom of body 10 passes component 40, and head assembly 20 is fixedly arranged on fixing device 30 or figure passes component 40, and head assembly 20 may be selected
Passed located at fixing device 30 or figure on component 40, make the structure of the aircraft body simpler with this, can be easy to top target
Detected, increase the scope of detection and use scope.
Reference picture 1 and Fig. 3, it is preferable that also including at least one locking member 50, locking member 50 and fixing device 30 and flight
Device body 10 is connected.
Above-mentioned locking member 50 can be on bolt, pin, nail etc., preferably bolt, aircraft body 10 and fixing device 30
Correspondence is equipped with mounting hole, and aircraft body 10 and fixing device 30 are each passed through both mounting holes by locking member 50 and carried out
Locking.When making the connection aircraft body 10 of fixing device 30 with this, it can closely be connected by locking member 50, be also convenient for fixing device
30 are dismantled.
Reference picture 1, further, fixing device 30 include at least one extension abutted against with aircraft body 10
31, the connection extension 31 of locking member 50.
Extension 31 therein can be two, can by extension 31 respectively symmetrically located at the both sides of aircraft body 10
Increase fixing device 30 and the contact area of aircraft body 10, strengthen the stability of the fixing device 30 installation, and lock
Part 50 connects aircraft body 10 and extension 31 simultaneously, by extension 31 locking member 50 can be easy to install, and making this, nobody flies
The attachment structure of row device is simpler, installs more stable.
Preferably, in addition to connecting wire 70, figure passes component 40 and includes (not scheming located at the connector of aircraft body 10
Show), one end of connecting wire 70 is electrically connected with connector (not shown), head assembly 20 be connected device 30 when, connection is led
The other end of line 70 is electrically connected with head assembly 20.
Above-mentioned connecting wire 70 is preferably soft row's connecting line, is easy to be distributed and arranges, in order to which head assembly 20 is carried out
Disassembly and assembly.
Reference picture 2 is to Fig. 6, it is preferable that also pass the lock of the bottom of component 40 including being respectively arranged on the top of fixing device 30 and figure
Tight component (not indicating), head assembly 20 passes component 40 with fixing device 30 or figure by latch assembly (not indicating) and detachably connected
Connect.
Above-mentioned latch assembly (not indicating) can be one, a latch assembly (not indicating) be connected to fixing device 30 or
Figure passes component 40, is passed in order to the installation of head assembly 20 or selectively located at fixing device 30 or figure on component 40.Locking
Component (not indicating) can be also two, be respectively arranged on fixing device 30 and figure passes component 40.
Preferably, latch assembly (not indicating) includes fastener 60 and locating part (not shown), and fastener 60 slidably connects
Connect fixing device 30 or figure passes one end of component 40, locating part (not shown) is fixedly connected with the top of fixing device 30 or figure passes component
The other end of 40 bottoms, forms a holding area between fastener 60 and locating part (not shown), head assembly 20, which is fastened on, to be put
In in holding area.
Above-mentioned head assembly 20 may include connecting plate and be respectively arranged on two limiting plates at connecting plate two ends, head assembly 20
When being partially disposed in holding area, each limiting plate is connected to fastener 60 or locating part (not shown) respectively.Preferably, locating part
(not shown) can be baffle plate, snap fit or elastic card component.Connecting plate and two limiting plates can be integrally formed, can by limiting plate
It is easy to head assembly 20 that the stability connected with positioning, enhancing head assembly 20 is installed.
Reference picture 6, it is preferable that fastener 60 includes Flexible Connector 62 and holding section 61, the one end of Flexible Connector 62 connects
Connect holding section 61, the other end is connected device 30 or figure passes component 40, is formed between holding section 61 and locating part (not shown)
One holding area.
Above-mentioned Flexible Connector 62 is preferably spring, holding section 61 by spring can automatic rebounding, and keep holding section
61 abut the tension force at place with head assembly 20, head assembly 20 is carried out self-locking, and be not easily disconnected from holding area.One implements
Example is that Flexible Connector 62 is fixedly connected with holding section 61, and fixing device 30 or figure pass component 40 and be correspondingly arranged on one and elasticity
The groove that connector 62 fastens, Flexible Connector 62 is arranged in groove, and can be moved along groove, and holding section 61 can be with
Flexible Connector 62 to move together, further enhance the stabilization and reliability of its connection.
Preferred embodiment of the present utility model is the foregoing is only, the scope of the claims of the present utility model is not thereby limited,
It is every utility model of the present utility model design under, the equivalent structure made using the utility model specification and accompanying drawing content
Conversion, or directly/be used in other related technical fields indirectly and be included in scope of patent protection of the present utility model.
Claims (8)
1. a kind of unmanned vehicle, it is characterised in that including aircraft body and head assembly, the top of the aircraft body
Provided with fixing device, the bottom of the aircraft body passes component provided with figure, and the head assembly is connected to the fixing device
Or the figure is passed on component.
2. unmanned vehicle as claimed in claim 1, it is characterised in that also including at least one locking member, the locking member
It is connected with the fixing device and the aircraft body.
3. unmanned vehicle as claimed in claim 2, it is characterised in that the fixing device includes and the aircraft body
At least one extension abutted against, the locking member connects the extension.
4. unmanned vehicle as claimed in claim 1, it is characterised in that also including connecting wire, the figure, which passes component, to be included
Located at the connector of the aircraft body, one end of the connecting wire is electrically connected with the connector, the head assembly
When connecting the fixing device, the other end of the connecting wire is electrically connected with the head assembly.
5. the unmanned vehicle as described in claim any one of 1-4, it is characterised in that also including being respectively arranged on the fixed dress
Top set portion and the figure pass the latch assembly of component bottom, and the head assembly passes through the latch assembly and the fixing device
Or the figure passes component and is detachably connected.
6. unmanned vehicle as claimed in claim 5, it is characterised in that the latch assembly includes fastener and locating part,
Fixing device described in the fastener slidable connection or the figure pass one end of component, and the locating part is fixedly connected described solid
Determine at the top of device or the figure passes the other end of component bottom, an accommodating area is formed between the fastener and the locating part
Domain, the head assembly is fastened in the holding area.
7. unmanned vehicle as claimed in claim 6, it is characterised in that the fastener includes Flexible Connector and engaging
Portion, described Flexible Connector one end connects the holding section, and the other end connects the fixing device or figure passes component, the engaging
A holding area is formed between portion and the locating part.
8. unmanned vehicle as claimed in claim 6, it is characterised in that the locating part is baffle plate, snap fit or elastic engaging
Part.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720235792.XU CN206569281U (en) | 2017-03-10 | 2017-03-10 | Unmanned vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720235792.XU CN206569281U (en) | 2017-03-10 | 2017-03-10 | Unmanned vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206569281U true CN206569281U (en) | 2017-10-20 |
Family
ID=60056886
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201720235792.XU Active CN206569281U (en) | 2017-03-10 | 2017-03-10 | Unmanned vehicle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206569281U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110603504A (en) * | 2018-07-26 | 2019-12-20 | 深圳市大疆创新科技有限公司 | Multi-cradle-head control method and device, unmanned aerial vehicle, medium and electronic equipment |
-
2017
- 2017-03-10 CN CN201720235792.XU patent/CN206569281U/en active Active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110603504A (en) * | 2018-07-26 | 2019-12-20 | 深圳市大疆创新科技有限公司 | Multi-cradle-head control method and device, unmanned aerial vehicle, medium and electronic equipment |
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| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| PE01 | Entry into force of the registration of the contract for pledge of patent right | ||
| PE01 | Entry into force of the registration of the contract for pledge of patent right |
Denomination of utility model: Unmanned aerial vehicle Effective date of registration: 20200824 Granted publication date: 20171020 Pledgee: Shenzhen hi tech investment small loan Co.,Ltd. Pledgor: PRODRONE TECHNOLOGY Co. Registration number: Y2020980005273 |