CN205661645U - Multiaxis unmanned aerial vehicle's horn quick assembly disassembly structure - Google Patents
Multiaxis unmanned aerial vehicle's horn quick assembly disassembly structure Download PDFInfo
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- CN205661645U CN205661645U CN201620480056.6U CN201620480056U CN205661645U CN 205661645 U CN205661645 U CN 205661645U CN 201620480056 U CN201620480056 U CN 201620480056U CN 205661645 U CN205661645 U CN 205661645U
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- horn
- component
- plug
- unmanned plane
- fixing seat
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Abstract
The utility model discloses a multiaxis unmanned aerial vehicle's horn quick assembly disassembly structure, multiaxis unmanned aerial vehicle's horn quick assembly disassembly structure is provided with quick -witted arm components, plug subassembly and the fuselage member of columnar structure, and quick -witted arm components can dismantle the setting on the fuselage member, and the plug subassembly includes public head of the plug of mutual adaptation and the female head of plug, and the public head of plug mates setting respectively on quick -witted arm components or fuselage member with plug mother head, be provided with the fixing base on the fuselage member, be provided with the fixing base member of hollow columnar structure on the fixing base, public head of plug or the female head of plug set up on the fixing base member, and quick -witted arm components can dismantle the setting on the fixing base member, fuselage member and quick -witted arm components are for can dismantle connection structure, and messenger's multiaxis unmanned aerial vehicle that can be better accomplishes and dismantles and the installation.
Description
Technical field
This utility model relates to the fields such as unmanned air vehicle technique, specifically, is the horn fast assembling-disassembling knot of multiaxis unmanned plane
Structure.
Background technology
UAV is called for short " unmanned plane ", and english abbreviation is " UAV ", utilizes radio robot and provides for oneself
The most manned aircraft that presetting apparatus is handled.
Unmanned plane presses application, can be divided into military and civilian.Military aspect, unmanned plane is divided into reconnaissance plane and target drone.Nothing
Man-machine+sector application, is real just the needing of unmanned plane；At present taking photo by plane, agricultural, plant protection, auto heterodyne, express transportation, disaster relief,
Observe wild animal, monitoring infectious disease, mapping, news report, electric inspection process, the disaster relief, movies-making, manufacture romance etc. field
Application, greatly expanded the purposes of unmanned plane itself, developed country is also at actively extension sector application and development unmanned plane
Technology.
In November, 2013, Civil Aviation Administration of China (CAAC) has issued " civilian push-button aircraft system driver pipe
Reason temporary provisions ", AOPA association of China it is responsible for the related management of civilian unmanned plane.According to " regulation ", inland of China unmanned plane
Operate and can be divided into 11 kinds of situations according to type size, flying area, the most only the unmanned plane of more than 116 kilograms and 4600 cubes
Dirigible more than rice is managed by civil aviation authority in the flight of fusion spatial domain, and remaining situation, including the most popular miniature aerial photography aircraft
In other interior flights, by employer's organization's management or it is responsible for voluntarily by manipulator.
Unmanned plane correlation technique develops rapidly both at home and abroad, and UAS is of a great variety, the wide distinct characteristics of purposes, causes it
When size, quality, voyage, boat, flying height, flight speed, task dispatching many-side has larger difference.Due to unmanned plane
Multiformity, has different sorting techniques for different considering:
Classifying by flying platform configuration, unmanned plane can be divided into fixed-wing unmanned plane, rotor wing unmanned aerial vehicle, unmanned airship, the umbrella wing
Unmanned plane, flapping wing unmanned plane etc..
Classification by use, unmanned plane can be divided into military unmanned air vehicle and civilian unmanned plane.Military unmanned air vehicle can be divided into scouting nothing
Man-machine, bait unmanned plane, UAV for electronic countermeasure, communication relay unmanned plane, UCAV and target drone etc.；Civilian unmanned plane
Inspection/supervision unmanned plane, agricultural unmanned plane, meteorological unmanned plane can be divided into, explore nine machine and mapping unmanned plane etc..
By yardstick classify (civil aviaton's regulation), unmanned plane can be divided into MAV, light-duty unmanned plane, SUAV and
Large-scale unmanned plane.MAV refers to that empty weight is less than or equal to 7kg, and light-duty unmanned plane quality is more than 7kg, but is less than or equal to
The unmanned plane of 116kg, and full power is flat flies, calibrated airspeed is less than 100km/h (55nmile/h), ceiling is less than 3000m.Little
Type unmanned plane, refers to that empty weight is less than or equal to the unmanned plane of 5700kg, except miniature and light-duty unmanned plane.Large-scale unmanned plane,
Refer to that empty weight is more than the unmanned plane of 5700kg.
By radius of action classify, unmanned plane can be divided into super short range unmanned plane, short range unmanned plane, short distance unmanned plane, intermediate range without
Man-machine and long-range unmanned aerial vehicle.Super short range unmanned plane radius of action is within 15km, and short range unmanned plane radius of action is 15～50km
Between, short distance unmanned plane radius of action is between 50～200km, and intermediate range unmanned plane radius of action is between 200～800km, far
Journey unmanned plane radius of action is more than 800km.
Classifying by task height, unmanned plane can be divided into extreme low-altitude unmanned plane, low latitude unmanned plane, hollow unmanned plane, high-altitude
Unmanned plane and superaltitude unmanned plane.Extreme low-altitude unmanned plane task height typically between 0～100m, low latitude unmanned plane task height
General between 100～1000m, hollow unmanned plane task height is typically between 1000～7000m, and High Altitude UAV task is high
Degree is general between 7000～18000m, more than 18000m as superaltitude unmanned plane task height.
Utility model content
The purpose of this utility model is to design the horn fast assembling disassembling structure of multiaxis unmanned plane, its frame member and machine
Arm member is Detachable connection structure, it is possible to preferably make multiaxis unmanned plane complete dismounting and install.
This utility model is achieved through the following technical solutions: the horn fast assembling disassembling structure of multiaxis unmanned plane, is provided with post
Horn component, plug-assembly and the frame member of shape structure, horn component is detachably arranged on frame member, plug-assembly bag
Include the plug male and plug female being mutually adapted, plug male and the pairing of plug female and be separately positioned on horn component or fuselage
On component.
Further for preferably realizing this utility model, use the following structure that arranges especially: on described frame member
It is provided with fixing seat, fixing seat is provided with the fixing seat component of open column shape structure, plug male or plug female and arranges
On fixing seat component, horn component is detachably arranged on fixing seat component.
Further for preferably realizing this utility model, use the following structure that arranges especially: at described horn component
It is provided with positioning element on outer surface, described fixing seat component and horn component connection are provided with guiding draw-in groove, guide
Draw-in groove is adaptive with positioning element.
Further for preferably realizing this utility model, use the following structure that arranges especially: described horn component is with solid
Reservation component is all open column shape body, and horn component is plugged in fixing seat component.
Further for preferably realizing this utility model, use the following structure that arranges especially: described horn component is sky
Heart cylindrical column, the inner chamber of horn component one end arranges plug male；Described fixing seat component is open circles barrel mast, fixing seat structure
On one end inner chamber that part is connected with horn component, plug female is set.
Further for preferably realizing this utility model, use the following structure that arranges especially: at described fixing seat component
It is additionally provided with spring part between female connector assembly and fixing seat.
Further for preferably realizing this utility model, use the following structure that arranges especially: described plug-assembly uses
Triangle plug assembly.
Further for preferably realizing this utility model, use the following structure that arranges especially: described guiding draw-in groove is L-type
Gathering sill.
Further for preferably realizing this utility model, the following structure that arranges of employing especially: described horn component and machine
Body component all uses carbon fibre material.
This utility model compared with prior art, has the following advantages and beneficial effect:
Its frame member of this utility model and horn component are Detachable connection structure, it is possible to preferably make multiaxis unmanned plane
Complete dismounting and install.
This utility model can assemble the horn of multiaxis unmanned plane more efficiently, and dismounting simultaneously is more conducive to carry, triangle
Plug avoids triple line being respectively connected to again, can adapt to different scenes by the different horns using different wheelbase according to demand,
In use, it is mounted directly and can use.
Accompanying drawing explanation
Fig. 1 is this utility model structural representation.
Fig. 2 is horn element structure schematic diagram described in the utility model.
Fig. 3 is frame member structural representation described in the utility model.
Fig. 4 is this utility model partial schematic diagram.
Wherein, 1-plug male, 2-positioning element, 3-horn component, 4-fixes seat, and 5-fixes seat component, and 6-plug is female
Head, 7-guides draw-in groove, 8-spring part.
Detailed description of the invention
Below in conjunction with embodiment, this utility model is described in further detail, but embodiment of the present utility model is not
It is limited to this.
Embodiment 1:
The horn fast assembling disassembling structure of multiaxis unmanned plane, frame member and horn component are Detachable connection structure, it is possible to
Preferably make multiaxis unmanned plane complete dismounting and install, as Figure 1-4, be specifically arranged to following structure: be provided with column knot
Horn component 3, plug-assembly and the frame member of structure, horn component 3 is detachably arranged on frame member, and plug-assembly includes
The plug male 1 being mutually adapted and plug female 6, plug male 1 or plug female 6 are separately positioned on horn component 3 or fuselage
On component.
When design uses, the plug male 1 in plug-assembly is arranged on horn component 3, corresponding supporting by slotting
Head female 6 is arranged on frame member；Or plug female 6 is arranged on horn component 3, the most supporting by plug male 1
Being arranged on frame member, multiaxis unmanned plane uses brushless electric machine, uses three-phase alternating current, three lines respectively with on frame member
Plug-assembly part be connected connection, three lines of concrete brushless electric machine are respectively welded on the solder joint of male 1 afterbody, and
Three output leads that electricity is adjusted then are welded on three welding holes at female rear portion.Horn and fuselage by the horn component of design and
Frame member is connected, and during use, utilizes the horn component being connected with horn and the frame member being connected with fuselage by machine
Arm and fuselage couple together, and utilize the plug-assembly being used in conjunction with each other three power lines will to be utilized to be incorporated into by power supply brushless
On motor.
Embodiment 2:
The present embodiment is to optimize further on the basis of above-described embodiment, further new for preferably realizing this practicality
Type, it is possible to preferably horn component is connected with frame member dismounting, as Figure 1-4, employing is following especially arranges structure:
Being provided with fixing seat 4 on described frame member, be provided with the fixing seat component 5 of open column shape structure on fixing seat 4, plug is public
1 or plug female 6 be arranged on fixing seat component 5, horn component 3 is detachably arranged on fixing seat component 5, makes in design
Used time, plug male 1 or the plug female 6 of plug-assembly are arranged in the cavity of fixing seat component 5, during use, horn structure
Part 3 inserts in the cavity of fixing seat component 5, and the plug-assembly part in horn component 3 and fixing seat component 5 is connected.
Embodiment 3:
The present embodiment is to optimize further on the basis of any of the above-described embodiment, further for preferably realizing this reality
With novel, it is possible to preferably by horn component and frame member with the use of, and horn component can be clamped on fuselage structure
On part, as Figure 1-4, the following structure that arranges is used especially: on the outer surface of described horn component 3, be provided with positioning element
2, at described fixing seat component 5, horn component 3 connection is provided with guiding draw-in groove 7, guides draw-in groove 7 and fit with positioning element 2
Joining, in use, horn component 3 is inserted in fixing seat component 5, and positioning element 2 is by guiding draw-in groove 7 clamping.
Embodiment 4:
The present embodiment is to optimize further on the basis of any of the above-described embodiment, further for preferably realizing this reality
With novel, facilitate the dismounting of horn component and frame member, as Figure 1-4, the following structure that arranges of employing especially: described horn
Component 3 and fixing seat component 5 are all open column shape body, and horn component 3 is plugged in fixing seat component 5, by horn component 3 with solid
Reservation component 5 is all arranged to cylindrical structure, it is possible to convenient dismounting between the two.
Embodiment 5:
The present embodiment is to optimize further on the basis of any of the above-described embodiment, further for preferably realizing this reality
With novel, it is possible to facilitate the access of power line, use the following structure that arranges especially: described horn component 3 is open circles barrel mast, machine
On the inner chamber of arm member 3 one end, plug male 1 is set；Described fixing seat component 5 is open circles barrel mast, fixing seat component 5 and machine
On one end inner chamber that arm member 3 is connected, plug female 6 is set；When design uses, the inner chamber of horn component 3 one end sets
Put plug male 1, and on the inner chamber of one end that fixing seat component 5 is connected with horn component 3, plug female 6 is set.
Embodiment 6:
The present embodiment is to optimize further on the basis of any of the above-described embodiment, further for preferably realizing this reality
With novel, it is simple to plug-assembly can shift flexibly in fixing seat component 5, as Figure 1-4, employing is following especially arranges knot
Structure: be additionally provided with spring part 8 between described fixing seat component 5 female connector assembly and fixing seat 4.
Embodiment 7:
The present embodiment is to optimize further on the basis of any of the above-described embodiment, further for preferably realizing this reality
With novel, it is possible to facilitate 3 power lines to be concurrently accessed, as Figure 1-4, the following structure that arranges is used especially: described plug group
Part uses triangle plug assembly.
Embodiment 8:
The present embodiment is to optimize further on the basis of any of the above-described embodiment, further for preferably realizing this reality
With novel, it is possible to be contained on fixing seat component by horn component, and fix further, employing is following especially arranges structure: described
Guiding draw-in groove 7 is L-type gathering sill, preferably guides draw-in groove 7 cross section and becomes half-frame structure, and the side of half frame is higher than opposite side, high
The port that is connected with horn component 3 with fixing seat component of half frame side flush.
Embodiment 9:
The present embodiment is to optimize further on the basis of any of the above-described embodiment, further for preferably realizing this reality
With novel, for reducing weight in the case of ensureing intensity, the following structure that arranges of employing especially: described horn component 3 and fuselage
Component all uses carbon fibre material.
Horn component 3 is provided with positioning element, frame member is provided with L-type gathering sill 7, sets in frame member
There are spring 8, spring 8 to prop up plug female (triangle plug female) 6 extrapolated, the positioning element 2 on horn component 3 is directed at
Inserting the guiding draw-in groove 7 of frame member, triangle plug is to connecting, and makes horn component 3 rotate with guiding draw-in groove 7 direction, works as rotation
To when rotating motionless, 8 horn components 3 of spring are extrapolated, be just stuck in guide draw-in groove 7 long limit groove in, make horn with
Fuselage perfection is connected.
The above, be only preferred embodiment of the present utility model, and this utility model not does any pro forma limit
System, every according to technical spirit of the present utility model, above example is made any simple modification, equivalent variations, each fall within
Within protection domain of the present utility model.
Claims (9)
1. the horn fast assembling disassembling structure of multiaxis unmanned plane, it is characterised in that: it is provided with the horn component (3) of column structure, inserts
Head assembly and frame member, horn component (3) is detachably arranged on frame member, and plug-assembly includes the plug being mutually adapted
Male (1) and plug female (6), plug male (1) or plug female (6) pairing are separately positioned on horn component (3) or fuselage
On component.
The horn fast assembling disassembling structure of multiaxis unmanned plane the most according to claim 1, it is characterised in that: at described fuselage structure
It is provided with fixing seat (4) on part, fixing seat (4) is provided with the fixing seat component (5) of open column shape structure, plug male
(1) or plug female (6) is arranged on fixing seat component (5), horn component (3) is detachably arranged on fixing seat component (5).
The horn fast assembling disassembling structure of multiaxis unmanned plane the most according to claim 2, it is characterised in that: at described horn structure
It is provided with positioning element (2) on the outer surface of part (3), arranges with horn component (3) connection described fixing seat component (5)
There is guiding draw-in groove (7), guide draw-in groove (7) adaptive with positioning element (2).
The horn fast assembling disassembling structure of multiaxis unmanned plane the most according to claim 2, it is characterised in that: described horn component
(3) in and fixing seat component (5) is all open column shape body, horn component (3) is plugged on fixing seat component (5).
The horn fast assembling disassembling structure of multiaxis unmanned plane the most according to claim 4, it is characterised in that: described horn component
(3) it is open circles barrel mast, the inner chamber of horn component (3) one end arranges plug male (1)；Described fixing seat component (5) is empty
Heart cylindrical column, one end inner chamber that fixing seat component (5) is connected with horn component (3) arranges plug female (6).
6. according to the horn fast assembling disassembling structure of the multiaxis unmanned plane described in claim 4 or 5, it is characterised in that: described solid
Spring part (8) it is additionally provided with between reservation component (5) female connector assembly and fixing seat (4).
7. according to the horn fast assembling disassembling structure of the multiaxis unmanned plane described in any one of claim 1-5, it is characterised in that: described
Plug-assembly uses triangle plug assembly.
The horn fast assembling disassembling structure of multiaxis unmanned plane the most according to claim 3, it is characterised in that: described guiding draw-in groove
(7) it is L-type gathering sill.
9. according to the horn fast assembling disassembling structure of the multiaxis unmanned plane described in any one of claim 1-5, it is characterised in that: described
Horn component (3) and frame member all use carbon fibre material.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620480056.6U CN205661645U (en) | 2016-05-24 | 2016-05-24 | Multiaxis unmanned aerial vehicle's horn quick assembly disassembly structure |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620480056.6U CN205661645U (en) | 2016-05-24 | 2016-05-24 | Multiaxis unmanned aerial vehicle's horn quick assembly disassembly structure |
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| Publication Number | Publication Date |
|---|---|
| CN205661645U true CN205661645U (en) | 2016-10-26 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201620480056.6U Expired - Fee Related CN205661645U (en) | 2016-05-24 | 2016-05-24 | Multiaxis unmanned aerial vehicle's horn quick assembly disassembly structure |
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Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107512390A (en) * | 2017-08-22 | 2017-12-26 | 北京航宇测通电子科技有限公司 | A kind of disc-shaped unmanned machine |
| CN109305362A (en) * | 2017-07-26 | 2019-02-05 | 昊翔电能运动科技(昆山)有限公司 | Unmanned vehicle |
-
2016
- 2016-05-24 CN CN201620480056.6U patent/CN205661645U/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109305362A (en) * | 2017-07-26 | 2019-02-05 | 昊翔电能运动科技(昆山)有限公司 | Unmanned vehicle |
| CN107512390A (en) * | 2017-08-22 | 2017-12-26 | 北京航宇测通电子科技有限公司 | A kind of disc-shaped unmanned machine |
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Legal Events
| 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 |
Granted publication date: 20161026 Termination date: 20210524 |
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| CF01 | Termination of patent right due to non-payment of annual fee |