CN207631482U - Unmanned vehicle - Google Patents
Unmanned vehicle Download PDFInfo
- Publication number
- CN207631482U CN207631482U CN201720895018.1U CN201720895018U CN207631482U CN 207631482 U CN207631482 U CN 207631482U CN 201720895018 U CN201720895018 U CN 201720895018U CN 207631482 U CN207631482 U CN 207631482U
- Authority
- CN
- China
- Prior art keywords
- horn
- fuselage
- unmanned vehicle
- clamping portion
- flexural pivot
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Active
Links
Landscapes
- Toys (AREA)
Abstract
The utility model is related to vehicle technology field, a kind of unmanned vehicle is provided, including fuselage and the horn that is connected with the fuselage, the horn is articulated with the fuselage by the spherical linkage portion, and can fold or be unfolded relative to the fuselage.Pass through mode described above, horn is connected using the fuselage of spherical linkage and unmanned plane, interim card is not present during the folding and expansion of horn, meet the known operating habit of user, so that entire unmanned plane, after folding, structure becomes compact, easy to carry, it can also effectively prevent the unmanned plane when carrying simultaneously, be damaged because of collision.
Description
【Technical field】
The utility model is related to vehicle technology field more particularly to a kind of unmanned vehicles.
【Background technology】
UAV, abbreviation unmanned plane (UAV) are a kind of new concept equipments being in rapidly developing, have
Maneuverability, rapid reaction, unmanned, operation require low advantage.Unmanned plane is set by carrying multiclass sensor or camera shooting
It is standby, image real-time Transmission, high-risk areas detecting function may be implemented, be the strong supplement of satellite remote sensing and traditional air remote sensing.
At present.The use scope of unmanned plane has widened military affairs, scientific research, civilian three big field, specifically in power communication, meteorology, agriculture
Industry ocean, exploration, photographs, prevents and reduces natural disasters, Crop Estimation, enforcing the drug law the application of the fields such as anti-smuggling, border patrol, public security anti-terrorism very
Extensively.
In the process of implementing the utility model, the inventor finds that the existing technology has at least the following problems：Current rotation
The not portable problem of wing unmanned plane generally existing.Although there is some unmanned functions to accomplish simply to fold, its knot folded
Structure is still not compact enough；The folding of many unmanned planes is only that rotor arm is made simple bending, and there is no the dimensions in length, width and height
Spend the size of overall reduction unmanned plane.
【Utility model content】
In order to solve the above-mentioned technical problem, the utility model embodiment provide it is a kind of compact-sized and it is folding nobody
Aircraft.
In order to solve the above technical problems, the utility model embodiment provides following technical scheme：
A kind of unmanned vehicle, including fuselage and the horn that is connected with the fuselage, the horn pass through the spherical hinge
Chain portion is articulated with the fuselage, and can fold or be unfolded relative to the fuselage.
In some embodiments, the spherical linkage portion includes being set to the flexural pivot shell of the fuselage and being contained in described
In flexural pivot shell and the spherical linkage hinged with the fuselage, the direction that horn folds described in the flexural pivot shell upper edge also opens up
There are open slot, the horn to be slided along the open slot to fold or be unfolded.
In some embodiments, the horn further includes position limiting structure, and the position limiting structure includes being set to outside the flexural pivot
The first clamping portion on shell and on the horn ontology and with the second clamping portion of first clamping portion clamping.
In some embodiments, first clamping portion is and to be located at the open slot set on the flexural pivot shell
The card slot of both sides, second clamping portion are fixture block.
In some embodiments, the quantity of the fixture block is two.
In some embodiments, first clamping portion is set on the flexural pivot shell and positioned at the open slot both sides
Fixture block, second clamping portion are card slot.
In some embodiments, the quantity of the card slot is two.
In some embodiments, the flexural pivot shell is hemispherical.
In some embodiments, the flexural pivot shell includes first part, second part, and by the first part,
The second part and the fuselage enclose the receiving space for accommodating the spherical linkage for setting and being formed jointly；Described first
Dividing has first side, and the second part has the second side being arranged with the first side relative spacing, the opening
Slot is formed by the gap between the first side and the second side.
In some embodiments, it is additionally provided on the first side and/or the second side for avoiding described second
The arc-shaped side edges of clamping portion.
Compared with prior art, the horn of the utility model embodiment is connected using the fuselage of spherical linkage portion and unmanned plane
It connects, interim card is not present during the folding and expansion of horn, meets the known operating habit of user so that entire unmanned plane warp
After folding, structure becomes compact, easy to carry, while can also effectively prevent the unmanned plane when carrying, because of collision
And it is damaged.
【Description of the drawings】
One or more embodiments are illustrated by the picture in corresponding attached drawing, these exemplary theorys
The bright restriction not constituted to embodiment, the element with same reference numbers label is expressed as similar element in attached drawing, removes
Non- to have special statement, composition does not limit the figure in attached drawing.
Fig. 1 is that a kind of structural representation for unmanned vehicle that the embodiments of the present invention 1 shown in simplification provide is three-dimensional
Figure, wherein the horn of unmanned plane is in unfolded state；
Fig. 2 is the structural representation stereogram of horn shown in FIG. 1；
Fig. 3 is that the structural representation of horn ontology and spherical linkage in the horn that the embodiments of the present invention provide is three-dimensional
Figure；
Fig. 4 is the structural representation stereogram of spherical housing in the horn that the embodiments of the present invention provide；
Fig. 5 is the structural representation front view of spherical housing in the horn that the embodiments of the present invention provide.
【Specific implementation mode】
For the ease of understanding the utility model, in the following with reference to the drawings and specific embodiments, the utility model is carried out more detailed
Thin explanation.It should be noted that when element is expressed " being fixed on " another element, it can be directly in another element
Upper or placed in the middle there may be one or more therebetween elements.When an element is expressed " connection " another element, it can
To be directly to another element or may exist one or more elements placed in the middle therebetween.This specification is used
Term "upper", "lower", "inner", "outside", the instructions such as " bottom " orientation or positional relationship be orientation based on ... shown in the drawings or
Position relationship is merely for convenience of describing the present invention and simplifying the description, and does not indicate or imply the indicated device or member
Part must have a particular orientation, with specific azimuth configuration and operation, therefore should not be understood as limiting the present invention.
In addition, term " first ", " second " " third " etc. are used for description purposes only, it is not understood to indicate or imply relatively important
Property.
Unless otherwise defined, technical and scientific term all used in this specification and the skill for belonging to the utility model
The normally understood meaning of technical staff in art field is identical.Art used in the description of the utility model in this specification
Language, which is only for the purpose of describing specific embodiments, is not intended to limitation the utility model.Term used in this specification
"and/or" includes any and all combinations of one or more relevant Listed Items.
In addition, as long as technical characteristic involved in the utility model difference embodiment disclosed below is each other not
Constituting conflict can be combined with each other.
Also referring to Fig. 1-2, the utility model embodiment provides a kind of unmanned vehicle 100, including Power Component 10
With fuselage 20.The Power Component 10 is installed on the fuselage 20, for providing power, and band for the unmanned vehicle 100
The dynamic unmanned vehicle 100 flies.The Power Component 10 can be also used for flight type toy etc..
Include the control circuit component being made of electronic components such as MCU in the fuselage 20, the control circuit component packet
Multiple control modules are included, e.g., for controlling the flight control modules of unmanned vehicle flight attitude, for the unmanned vehicle that navigates
Big dipper module and data processing module etc. for handling the environmental information acquired in related airborne equipment.
In the present embodiment, the Power Component 10 includes 12 and of driving device that horn 11, one is set to 11 one end of horn
It is installed on the propeller (not shown) of driving device 12.As shown in Fig. 2, the horn 11 includes horn ontology 111, set on described
The spherical linkage portion 112 of 111 other end of horn ontology, the horn 11 are articulated with the machine by the spherical linkage portion 112
Body 20, and can fold or be unfolded relative to the fuselage 20.It should be understood that spherical linkage portion 112 can also be arranged in fuselage
On 20.
Also referring to Fig. 3 and Fig. 4, spherical linkage portion 112 include set on the fuselage 20 flexural pivot shell 1121 and
It is contained in the flexural pivot shell 1121 and the spherical linkage 1122 hinged with the fuselage 20.
The flexural pivot shell 1121 includes first part 11211, second part 11212, and by the first part
11211, the second part 11212 and the fuselage 20 enclose jointly set to be formed for accommodating opening for the spherical linkage 1122
The receiving space 116 put.The first part 11211 have first side 301, the second part 11212 have with it is described
The second side of first side 301 relative spacing setting, the gap between first side 301 and the second side 302 are common
Form an open slot 113.The horn 11 can be slided along the open slot 113 to fold or be unfolded relative to fuselage 20.One
In optional embodiment, the flexural pivot shell 1121 is hemispherical, and in other possible embodiments, flexural pivot shell 1121 also may be used
To be other shapes.The horn 11 can also include position limiting structure 115, the position limiting structure 115 can be include being set to institute
Second for stating the first clamping portion on flexural pivot shell and being clamped on the horn ontology 111 and with first clamping portion
Clamping portion.In the present embodiment, first clamping portion is set on the flexural pivot shell 1121 and to be located at the open slot
The card slot 1151 of 113 both sides, second clamping portion are the fixture block 1152 being clamped with card slot 1151.In other embodiments,
One clamping portion can also be the fixture block on flexural pivot shell, and the second clamping portion mutually should be the card being clamped with fixture block on horn
Slot.When horn 11 slides into both sides in open slot 113, carried out by the clamping of fixture block 1152 Yu card slot 1151 disposed thereon
Positioning, to prevent horn 11 from carrying out unnecessary rotation.
In the present embodiment, for the fixture block 1152 on evacuation horn 11, arc-shaped side edges 303 are additionally provided on first side, therefore
When being unfolded or folding horn 11, fixture block 1152 is turned to towards first side 301 so that horn 11 can be rotated swimmingly.
It is understood that in some other embodiment, it is additionally provided on the second side 302 for avoiding described
The arc-shaped side edges 303 of two clamping portions.Alternatively, the first side 301 and second side 302 are equipped with for avoiding described second
The arc-shaped side edges 303 of clamping portion.
Further, the open slot 113 includes that the first circular open 1131, the second circular open 1132 and third are round
Opening 1133.The third circular open 1133 is described between the first circular open 1131 and the second circular open 1132
Third circular open 1133 is connected with first circular open 1131 and second circular open 1132.
The cross-sectional shape of the horn ontology 111 is circle, and the horn ontology 111 can be in the open slot 113
Sliding in opening, and can be blocked by any of the first circular open 1131 and the second circular open 1132.When described first
When circular open 1131 blocks the horn ontology 111, the fixture block 1152 is embedded in the card slot 1151, and by the card slot
1151 block.First circular open 1131 blocks the horn ontology 111, to prevent the horn ontology 111 described
Sliding in open slot 113.When second circular open 1132 blocks the horn ontology 111, the fixture block 1152 is embedded in
In another card slot 1151, and blocked by another card slot 1151.Second circular open 1132 blocks the horn
Ontology 111, to prevent the sliding of the horn ontology 111.
Equal in magnitude, the third circular open 1133 of first circular open, 1132 and second circular open 1133
Diameter be more than first circular open 1131 diameter.In folding or expansion, the horn ontology 111 is first from the first circle
Shape opening 1131 slides into the third circular open 1133, and the rotation 180 in the third circular open 1133
Degree.This is because, the diameter phase of the diameter of the horn ontology 111 and the first circular open 1131 and the second circular open 1132
Deng due to the presence of fixture block 1152, causing the horn ontology 111 round in first circular open 1131 or second
Rotation in opening 1132.Postrotational horn ontology 111 can smoothly enter into second circular open 1132, and the fixture block
1152 are embedded in another card slot 1151.
It is understood that in some other embodiment, first clamping portion is set on the flexural pivot shell and position
Fixture block in the open slot both sides, second clamping portion are card slot.The fixture block 1152 is no longer set to the horn sheet
On body 111, the fixture block 1152 altogether there are two, may be contained within the side of described 111 one end of horn ontology, two fixture blocks 1152
Line intersects with the axis of the horn ontology 111.Two fixture blocks 1152 are respectively arranged at two in embodiment as shown in Figure 5
The position of a card slot 1151.Two card slots 1151 are respectively equipped on the horn ontology 111.That is, the card slot 1151 is set
It is placed in the position of fixture block 1152 described in embodiment as shown in Figure 3.
It is understood that in some other embodiment, the flexural pivot shell no longer can individually become one zero
Part, and it is installed on the fuselage 20.The shell of the flexural pivot shell and the fuselage 20 is an integral structure.
In the present embodiment, the driving device 12 is motor.It is understood that described in some other embodiment
Driving device 12 can also be air pressure motor etc..
It is understood that in some other embodiment, the number of the horn 11, driving device 12 and propeller is not
It is limited to four, can be designed according to actual demand, such as two, three or four or more.
When flight, the horn 11 is in unfolded state.First circular open 1131 blocks the horn ontology 111
When, the fixture block 1152 is embedded in the card slot 1151, and is blocked by the card slot 1151.The horn 11 is completely fixed
Firmly, it is set to the driving device 12 of 11 other end of horn, power is provided, the unmanned vehicle 100 is driven to fly.
After flight, the horn 11 is in folded state.The horn ontology 111 is first from the first circular open
1131 slide into the third circular open 1133, and 180 degree of the rotation in the third circular open 1133.It is described
Horn ontology 111 slides into second circular open 1132 by the third circular open 1133.Second circular open
1132 block the horn ontology 111, and the fixture block 1152 is embedded in another card slot 1151, and by another card slot
1151 block.The horn 11 is completed to fold at this time, then propeller is folded so that the Power Component 10 is tightly attached to institute
State the two opposite sides of fuselage 20.
Based on the above structure design, compared to the folding mode of existing unmanned vehicle horn, the utility model is implemented
Horn 11 in example is connect using spherical linkage portion 112 with the fuselage 20 of unmanned vehicle 100, horn folding and be unfolded
Interim card is not present in journey, and meets the known operating habit of user so that entire unmanned vehicle 100 is after folding, structure
Become closely, it is easy to carry, while can also effectively prevent the unmanned vehicle 100 when carrying, due to collision
It is damaged.
Finally it should be noted that：Above example is only to illustrate the technical solution of the utility model, rather than its limitations；
Under the thinking of the utility model, it can also be combined between the technical characteristic in above example or different embodiments,
Step can be realized with random order, and there are many other variations of the different aspect of the utility model as described above, be
Simplicity, they do not provide in details；Although the utility model is described in detail with reference to the foregoing embodiments, this
The those of ordinary skill in field should understand that：Its still can with technical scheme described in the above embodiments is modified,
Or equivalent replacement of some of the technical features；And these modifications or replacements, do not make the sheet of corresponding technical solution
Matter is detached from the range of various embodiments of the utility model technical solution.
Claims (10)
1. a kind of unmanned vehicle (100) comprising fuselage (20) and the horn (11) being connected with the fuselage (20), feature
It is, the horn (11) is articulated with the fuselage (20) by spherical linkage portion (112), and can be relative to the fuselage (20)
It folds or is unfolded.
2. unmanned vehicle (100) according to claim 1, which is characterized in that the spherical linkage portion (112) includes setting
In the fuselage (20) flexural pivot shell (1121) and be contained in the flexural pivot shell (1121) and with the fuselage (20)
Hinged spherical linkage (1122), the direction that horn (11) described in flexural pivot shell (1121) upper edge folds are further opened with opening
Slot (113), the horn (11) are slided along the open slot (113) to fold or be unfolded.
3. unmanned vehicle (100) according to claim 2, which is characterized in that the horn (11) further includes limit knot
Structure (115), the position limiting structure (115) include the first clamping portion being set on the flexural pivot shell (1121) and are set to described
The second clamping portion being clamped on horn ontology (111) and with first clamping portion.
4. unmanned vehicle (100) according to claim 3, which is characterized in that first clamping portion is set on described
Flexural pivot shell (1121), and it is located at the card slot (1151) of the open slot (113) both sides, second clamping portion is fixture block
(1152)。
5. unmanned vehicle (100) according to claim 4, which is characterized in that the quantity of the fixture block (1152) is two
It is a.
6. unmanned vehicle (100) according to claim 3, which is characterized in that first clamping portion is set on described
Flexural pivot shell (1121) and the fixture block (1152) for being located at the open slot (113) both sides, second clamping portion are card slot
(1151)。
7. unmanned vehicle (100) according to claim 6, which is characterized in that the quantity of the card slot (1151) is two
It is a.
8. unmanned vehicle (100) according to claim 2, which is characterized in that the flexural pivot shell (1121) is in hemisphere
Shape.
9. according to claim 3-8 any one of them unmanned vehicle (100), which is characterized in that
The flexural pivot shell (1121) includes first part (11211), second part (11212), and by the first part
(11211), the second part (11212) and the fuselage (20) enclose jointly set to be formed for accommodating the spherical linkage
(1122) receiving space (116)；
The first part (11211) has first side (301), and the second part (11212) has and first side
The second side (302) of side (301) relative spacing setting, the open slot (113) is by the first side (301) and described the
Gap between dual side-edge (302) is formed.
10. unmanned vehicle (100) according to claim 9, which is characterized in that the first side (301) and/or institute
State the arc-shaped side edges (303) being additionally provided on second side (302) for avoiding second clamping portion.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720895018.1U CN207631482U (en) | 2017-07-21 | 2017-07-21 | Unmanned vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720895018.1U CN207631482U (en) | 2017-07-21 | 2017-07-21 | Unmanned vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN207631482U true CN207631482U (en) | 2018-07-20 |
Family
ID=62861134
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201720895018.1U Active CN207631482U (en) | 2017-07-21 | 2017-07-21 | Unmanned vehicle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN207631482U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109278993A (en) * | 2017-07-21 | 2019-01-29 | 深圳市道通智能航空技术有限公司 | Unmanned vehicle |
| CN109606662A (en) * | 2018-12-11 | 2019-04-12 | 泉州齐美电子科技有限公司 | A kind of quadrotor drone rolled over |
-
2017
- 2017-07-21 CN CN201720895018.1U patent/CN207631482U/en active Active
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109278993A (en) * | 2017-07-21 | 2019-01-29 | 深圳市道通智能航空技术有限公司 | Unmanned vehicle |
| CN109606662A (en) * | 2018-12-11 | 2019-04-12 | 泉州齐美电子科技有限公司 | A kind of quadrotor drone rolled over |
| CN109606662B (en) * | 2018-12-11 | 2021-09-21 | 南京多基观测技术研究院有限公司 | Foldable quad-rotor unmanned aerial vehicle |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| US10730619B2 (en) | Arm and unmanned aerial vehicle | |
| CN204998752U (en) | Folding unmanned aerial vehicle | |
| CN205554560U (en) | Unmanned vehicles and frame thereof | |
| CN109383739A (en) | A kind of horn and unmanned plane | |
| CN207631482U (en) | Unmanned vehicle | |
| CN107074353B (en) | UAV system | |
| CN204895844U (en) | Many rotor unmanned aerial vehicle | |
| WO2017097021A1 (en) | Wearable unmanned aerial vehicle | |
| US20200180760A1 (en) | Modular unmanned air vehicles | |
| CN109204786A (en) | A kind of undercarriage and the unmanned plane with this undercarriage | |
| CN108146618A (en) | Undercarriage and the unmanned vehicle with this undercarriage | |
| WO2018103026A1 (en) | Multi-rotor unmanned aerial vehicle | |
| CN109426298A (en) | Control bar assembly and remote controler | |
| US11583046B2 (en) | Modular utility kit | |
| CN207758999U (en) | Undercarriage and unmanned vehicle with this undercarriage | |
| CN107740847A (en) | Damping device, the head assembly and unmanned plane with this damping device | |
| US20190013578A1 (en) | Antenna and unmanned aerial vehicle | |
| CN206885330U (en) | Horn, Power Component and unmanned plane | |
| CN207141361U (en) | A kind of horn and unmanned plane | |
| CN109278993A (en) | Unmanned vehicle | |
| CN208630841U (en) | Wing folding unmanned plane | |
| CN210455176U (en) | Folding horn and unmanned vehicles | |
| CN206885336U (en) | A kind of undercarriage and the unmanned plane with this undercarriage | |
| CN207961408U (en) | Damping device, head assembly and unmanned plane with this damping device | |
| CN207352507U (en) | Control bar assembly and remote controler |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CP01 | Change in the name or title of a patent holder |
Address after: 518055 Guangdong city of Shenzhen province Nanshan District Xili Street Xueyuan Road No. 1001 Chi Yuen Building 9 layer B1 Patentee after: Shenzhen daotong intelligent Aviation Technology Co.,Ltd. Address before: 518055 Guangdong city of Shenzhen province Nanshan District Xili Street Xueyuan Road No. 1001 Chi Yuen Building 9 layer B1 Patentee before: AUTEL ROBOTICS Co.,Ltd. |
|
| CP01 | Change in the name or title of a patent holder |