CN206031751U - Unmanned aerial vehicle that can quick assembly disassembly - Google Patents
Unmanned aerial vehicle that can quick assembly disassembly Download PDFInfo
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- CN206031751U CN206031751U CN201620571763.6U CN201620571763U CN206031751U CN 206031751 U CN206031751 U CN 206031751U CN 201620571763 U CN201620571763 U CN 201620571763U CN 206031751 U CN206031751 U CN 206031751U
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- fuselage
- postbrachium
- forearm
- unmanned plane
- maintenance
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Abstract
The utility model discloses an unmanned aerial vehicle that can quick assembly disassembly, including fuselage and horn, the horn includes forearm and postbrachium, and the quantity of forearm and postbrachium is two, two forearms symmetry install the front end at the fuselage, battery, motor, power shaft, paddle, electronic governor, automatic pilot, global positioning system and data image sensor between forearm and the fuselage, all adopt the mode of plug to connect between postbrachium and the fuselage, are installed to the installing in the rear end of fuselage of two postbrachium symmetries in the fuselage, the camera is installed to the lateral part of fuselage. The device reasonable in design adopts the mode of plug to connect between fuselage and forearm, fuselage and the postbrachium, the dismouting of be convenient for forearm and postbrachium can reduce holistic package size, is convenient for transport, the device all adopts modular piece, only need the maintenance with the part of changing the trouble can, need not to maintain and change the single unit system, reduced the time of maintenance, reduced the cost of maintenance.
Description
Technical field
This utility model is related to a kind of unmanned plane, it is specifically a kind of can be with the unmanned plane of fast assembling-disassembling.
Background technology
Unmanned plane is the abbreviation of UAV, is using radio robot and the presetting apparatus provided for oneself behaviour
Vertical not manned aircraft.Unmanned plane presses application, can be divided into military unmanned air vehicle with civilian unmanned plane.Military aspect, unmanned plane
It is divided into reconnaissance plane and target drone.Civilian aspect, application of the unmanned plane in many industries is the real firm need of unmanned plane；At present nobody
Machine is taking photo by plane, agricultural, plant protection, auto heterodyne, express transportation, disaster relief, observation wild animal, monitoring infectious disease, mapping, Xin Wen Bao
The fields such as road, electric inspection process, the disaster relief, movies-making, manufacture romance are widely used.Due to the high-technology, loading of unmanned plane
Matter and working forms, need use compared with high power and easy to maintain, therefore the size of unmanned plane can be larger, and this results in
Require that higher therefore common on the market unmanned plane needs larger packaging in terms of unmanned plane packaging, transport and fast assembling-disassembling,
And often be difficult to be safeguarded, it is very inconvenient in links such as assembling, packing, transports；As the use of unmanned plane is changed planes respectively
Different, maintenance rate is higher, and common type overall must be changed when damaging on the market, which increases maintenance cost.
Utility model content
The purpose of this utility model be provide it is a kind of can be with the unmanned plane of fast assembling-disassembling, to solve in above-mentioned background technology
The problem of proposition.
For achieving the above object, this utility model provides following technical scheme：
It is a kind of can be with the unmanned plane of fast assembling-disassembling, including fuselage and horn, the horn includes forearm and postbrachium, forearm and
The quantity of postbrachium is two, and two forearms are symmetrically installed on the front end of fuselage, and two postbrachiums are symmetrically installed on fuselage
Rear end, between forearm and fuselage, between postbrachium and fuselage using plug by the way of connect, be provided with fuselage battery, motor,
Power shaft, blade, electron speed regulator, automatic pilot, global positioning system and data imageing sensor, the sidepiece peace of fuselage
Equipped with photographic head, electron speed regulator is connected by holding wire with automatic pilot, and photographic head is connected with data image sensor.
As further program of the utility model：Shock mitigation system is also equipped with fuselage.
As further program of the utility model：Battery adopts charged lithium cells.
Compared with prior art, the beneficial effects of the utility model are：The device is reasonable in design, fuselage and forearm, fuselage
Connected by the way of plug and postbrachium between, be easy to the dismounting of forearm and postbrachium, overall Package size can be reduced, be easy to
Transport；The device adopts modular member, need to only keep in repair and change the part of failure, without the need for tieing up to single unit system
Repair and change, reduce the time of maintenance, reduce the cost of maintenance.
Description of the drawings
Fig. 1 is can be with the structural representation of the unmanned plane of fast assembling-disassembling.
Fig. 2 is can be with the structural representation of the unmanned plane middle fuselage of fast assembling-disassembling.
Fig. 3 is can be with the structural representation of forearm in the unmanned plane of fast assembling-disassembling.
Fig. 4 is can be with the structural representation of postbrachium in the unmanned plane of fast assembling-disassembling.
Wherein：1- fuselages, 2- forearms, 3- postbrachiums.
Specific embodiment
The technical scheme of this patent is described in more detail with reference to specific embodiment.
Refer to Fig. 1-4, it is a kind of can be with the unmanned plane of fast assembling-disassembling, including fuselage 1 and horn, the horn includes forearm
2 and the quantity of postbrachium 3, forearm 2 and postbrachium 3 be two, two forearms 2 are symmetrically installed on the front end of fuselage 1, two postbrachiums
3 rear ends for being symmetrically installed on fuselage 1, are connected by the way of plug between forearm 2 and fuselage 1, between postbrachium 3 and fuselage 1
Connect, be provided with fuselage 1 battery, motor, power shaft, blade, electron speed regulator, automatic pilot, global positioning system and
Data image sensor, the sidepiece of fuselage 1 are provided with photographic head, and electron speed regulator is connected by holding wire with automatic pilot,
Photographic head is connected with data image sensor.Shock mitigation system is also equipped with fuselage 1.Battery adopts charged lithium cells.
Operation principle of the present utility model is：Between fuselage 1 and forearm 2, fuselage 1 and postbrachium 3 by the way of plug
Connection, installation and removal speed are fast, when needing packaging and transporting pull forearm 2 and postbrachium 3, reduce packaging and transport
Defeated volume；When the part of device needs repairing, only need to keep in repair and change part, without the need for whole device carry out keeping in repair with
Change, reduce maintenance time, reduce maintenance cost.
The device is reasonable in design, is connected, before being easy between fuselage 1 and forearm 2, fuselage 1 and postbrachium 3 by the way of plug
The dismounting of arm 2 and postbrachium 3, can reduce overall Package size, be readily transported；The device adopts modular member, only needs
Maintenance and the part of replacing failure, without the need for being keeped in repair to single unit system and being changed, reduce the time of maintenance, reduce
The cost of maintenance.
Above the better embodiment of this patent is explained in detail, but this patent is not limited to above-mentioned embodiment party
Formula, in the ken that one skilled in the relevant art possesses, can be with the premise of without departing from this patent objective
Various changes can be made.
Claims (3)
1. a kind of can be with the unmanned plane of fast assembling-disassembling, it is characterised in that including fuselage and horn, the horn include forearm and after
The quantity of arm, forearm and postbrachium is two, and two forearms are symmetrically installed on the front end of fuselage, the symmetrical installation of two postbrachiums
In the rear end of fuselage, connected by the way of plug between forearm and fuselage, between postbrachium and fuselage, electricity is installed in fuselage
Pond, motor, power shaft, blade, electron speed regulator, automatic pilot, global positioning system and data imageing sensor, fuselage
Sidepiece photographic head is installed, electron speed regulator is connected by holding wire with automatic pilot, and photographic head and data image are sensed
Device is connected.
2. according to claim 1 can be with the unmanned plane of fast assembling-disassembling, it is characterised in that be also equipped with subtracting on the fuselage
Shake system.
3. according to claim 1 can be with the unmanned plane of fast assembling-disassembling, it is characterised in that the battery using charging lithium electricity
Pond.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620571763.6U CN206031751U (en) | 2016-06-15 | 2016-06-15 | Unmanned aerial vehicle that can quick assembly disassembly |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620571763.6U CN206031751U (en) | 2016-06-15 | 2016-06-15 | Unmanned aerial vehicle that can quick assembly disassembly |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206031751U true CN206031751U (en) | 2017-03-22 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201620571763.6U Active CN206031751U (en) | 2016-06-15 | 2016-06-15 | Unmanned aerial vehicle that can quick assembly disassembly |
Country Status (1)
| Country | Link |
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| CN (1) | CN206031751U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2020000660A1 (en) * | 2018-06-26 | 2020-01-02 | 深圳市大疆创新科技有限公司 | Unmanned aerial vehicle and arms thereof |
-
2016
- 2016-06-15 CN CN201620571763.6U patent/CN206031751U/en active Active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2020000660A1 (en) * | 2018-06-26 | 2020-01-02 | 深圳市大疆创新科技有限公司 | Unmanned aerial vehicle and arms thereof |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant |