CN207417138U - Multi-rotor unmanned aerial vehicle - Google Patents
Multi-rotor unmanned aerial vehicle Download PDFInfo
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- CN207417138U CN207417138U CN201720703119.4U CN201720703119U CN207417138U CN 207417138 U CN207417138 U CN 207417138U CN 201720703119 U CN201720703119 U CN 201720703119U CN 207417138 U CN207417138 U CN 207417138U
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- aerial vehicle
- unmanned aerial
- rotor unmanned
- rotor
- armature assembly
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Abstract
The utility model proposes multi-rotor unmanned aerial vehicle, including：Middle armature assembly, attachment device and rotor group device, the middle armature assembly is located at the center of multi-rotor unmanned aerial vehicle, including power battery pack and aircraft control system；The attachment device is fixedly connected with middle armature assembly, including carbon pipe and triangle joint device；The rotor group device is fixed in attachment device, including motor and propeller.The utility model proposes multi-rotor unmanned aerial vehicle, propose a kind of simple assemble method of multi-rotor unmanned aerial vehicle, a kind of thinking can be provided for the assembling of subsequent multi-rotor unmanned aerial vehicle, simultaneously, this multi-rotor unmanned aerial vehicle has the advantages that foldable, VTOL, can hover, is low etc. to site requirements, it can carry medicine-chest, camera etc. and complete the tasks such as pesticide spraying, mapping.
Description
Technical field
The utility model belongs to aviation aircraft technical field, particularly multi-rotor unmanned aerial vehicle.
Background technology
Aviation field rises at present, and by this carrier of aircraft, many equipment can help people in extreme circumstances
Complete task.Multi-rotor unmanned aerial vehicle can also be called multiaxis unmanned plane, according to propeller quantity, and can be subdivided into quadrotor, six
Rotor, eight rotors etc..It is generally believed that propeller quantity is more, flight is more steady, and operation is easier.
But the increase of unmanned plane propeller simply directly increases merely on body at present, this increased spiral of method
Paddle limited amount, and increase the burden of body.
Therefore, there is an urgent need for finding a kind of new method, to achieve the purpose that infinitely increase propeller.
Utility model content
To solve the above-mentioned problems, the utility model provides multi-rotor unmanned aerial vehicle.
Specific technical solution is as follows：
Multi-rotor unmanned aerial vehicle, including：Middle armature assembly, attachment device and rotor group device, the middle armature assembly are located at more rotations
The center of wing unmanned plane, including power battery pack and aircraft control system；The attachment device is fixed with middle armature assembly to be connected
It connects, including carbon pipe and triangle joint device；The rotor group device is fixed in attachment device, including motor and spiral
Paddle.
Preferably, the middle armature assembly further includes fuel tank and aircraft control system.
Preferably, the rotor group device further includes engine and propeller.
Preferably, the number of the attachment device is even number.
Preferably, the number of the attachment device is 4.
Preferably, the number of the propeller is 4 (2n-1)。
Preferably, the multi-rotor unmanned aerial vehicle further includes undercarriage and carrying apparatus.
Preferably, the carrying apparatus is medicine-chest.
Preferably, the carrying apparatus is camera.
Preferably, the triangle joint device can fold.
Compared with the prior art, multi-rotor unmanned aerial vehicle described in the utility model has the advantage that：
The utility model proposes multi-rotor unmanned aerial vehicle, it is proposed that a kind of simple assemble method of multi-rotor unmanned aerial vehicle, can
A kind of thinking is provided with the assembling for subsequent multi-rotor unmanned aerial vehicle, meanwhile, this multi-rotor unmanned aerial vehicle has foldable, vertical
Landing, the advantages such as can hover, is low to site requirements, it can carry medicine-chest, camera etc. and complete the tasks such as pesticide spraying, mapping.
Description of the drawings
Fig. 1 be the utility model proposes multi-rotor unmanned aerial vehicle structure diagram；
Fig. 2 be the utility model proposes multi-rotor unmanned aerial vehicle structure diagram；
Fig. 3 is the structure chart of preferred 12 rotor of the utility model.
Reference sign：
2 attachment device of armature assembly, 3 rotor group device in 1
4 carbon pipe, 5 triangle joint device
Specific embodiment
The technical solution of the utility model is further described below in conjunction with specific embodiment.It should be appreciated that herein
The specific embodiment of description is only used to explain the utility model, is not used to limit the utility model.
In the description of the utility model, it is to be understood that term " " center ", " longitudinal direction ", " transverse direction ", " on ", " under ",
The orientation or position relationship of the instructions such as "front", "rear", "left", "right", " vertical ", " level ", " top ", " bottom ", " interior ", " outer " are
Based on orientation shown in the drawings or position relationship, it is for only for ease of description the utility model and simplifies description rather than instruction
Or imply that signified device or element must have specific orientation, with specific azimuth configuration and operation, therefore be not understood that
For the limitation to the utility model.
, it is necessary to which explanation, unless otherwise clearly defined and limited, term " are pacified in the description of the utility model
Dress ", " connected ", " connection " should be interpreted broadly, for example, it may be being fixedly connected or being detachably connected or integrally
Connection；Can be mechanical connection or electrical connection；Can be directly connected to, can also be indirectly connected by intermediary,
It can be the connection inside two elements.For the ordinary skill in the art, on being understood by concrete condition
State concrete meaning of the term in the utility model.
The utility model will be described in detail below with reference to the accompanying drawings and embodiments.
Fig. 1 to Fig. 2 be the utility model proposes multi-rotor unmanned aerial vehicle structure diagram, including：Middle armature assembly 1 connects
Connection device 2 and rotor group device 3, the middle armature assembly 1 are located at the center of multi-rotor unmanned aerial vehicle, including power battery pack and
Aircraft control system can also include fuel tank and aircraft control system；The attachment device 2 is fixedly connected with middle armature assembly 1, phase
For middle armature assembly 1, all attachment devices 2 are in T_Starburst, are centrosymmetric on middle armature assembly 1, attachment device 2 is wrapped
Carbon pipe 4 and triangle joint device 5 are included, carbon pipe 4 is directly connected with middle armature assembly 1, and triangle joint device 5 is mounted on carbon pipe 4,
For separating more 4 branches of Tan Guan, increasing the quantity of rotor, the number of attachment device 2 is even number, preferably 2,4,6,8
A, when the number of attachment device 2 is 4, the number of propeller is 4 (2n- 1), n is the number of plies of propeller, is with middle armature assembly 1
The distance of the center of circle, propeller and middle armature assembly 1 is radius, and the consistent propeller of radius is one layer, can also with same reason
Propeller number when the number for pushing over out attachment device 2 is 2,6,8；The rotor group device 3 is fixed at attachment device 2
On, including motor and propeller, engine and propeller, when fuel tank is placed in armature assembly 1 in the middle, rotor can also be included
Group device 3 just includes engine and propeller, and power is dynamic for oil, when power battery pack is placed in armature assembly 1 in the middle, rotor
Group device 3 just includes motor and propeller, and power is electronic.The multi-rotor unmanned aerial vehicle further includes frame and carrying apparatus, carries
Object device can be medicine-chest or camera, if the medicine-chest placed, can be used for the herbal sprinkling to crops, if phase
Machine, the tasks such as can complete to survey and draw or cruise.On the other hand, the triangle joint device 5 in the utility model is folding,
If the quantity of propeller is relatively more, occupied space is larger, is unfavorable for transporting for long-distance, this folding can be very good to solve
These problems.
Fig. 3 is the structure chart of preferred 12 rotor of the utility model, and the number of plies of propeller is 2, so the number of propeller
Mesh is 4* (22- 1)=12, fuel tank and aircraft control system can be placed in middle armature assembly 1, power electric can also be placed
Pond group and aircraft control system, when placing fuel tank, rotor group device 3 includes engine and propeller, has in attachment device 2
Oil pipe passes through, and the oil in fuel tank is sent to engine, provides power；When placing power battery pack, rotor group device 3 includes electricity
Machine and propeller have cable to pass through in attachment device 2, and the electric energy of power battery pack is sent to motor, provide power, drive spiral shell
Paddle is revolved to rotate.Triangle joint device 5, these triangle joint devices 5 are set between first layer propeller and second layer propeller
It can all fold, can be laterally folded, space is saved, while is also provided conveniently for transport.Under middle armature assembly 1
Face is provided with carrying apparatus, can carry medicine-chest, can also carry camera, can carry the article of any required carrying, and then
Complete the tasks such as pesticide spraying, mapping, cruise.Undercarriage can play the role of support when unmanned plane lands.
The utility model proposes multi-rotor unmanned aerial vehicle, can quickly adjust rotor quantity, i.e., structure finely tune in the case of
Dynamical system adjustment can be achieved, using modularized design, can conveniently motivation of adjustment system, happen suddenly even if being tackled in outfield
Job task change, also can easily configure rational dynamical system, realize efficiently easily operation.
In conclusion the utility model proposes multi-rotor unmanned aerial vehicle, it is proposed that simple group of a kind of multi-rotor unmanned aerial vehicle
Dress method can provide a kind of thinking for the assembling of subsequent multi-rotor unmanned aerial vehicle, meanwhile, this multi-rotor unmanned aerial vehicle has can
Folding, VTOL, the advantages such as can hover, is low to site requirements, it can carry medicine-chest, camera etc. and complete pesticide spraying, surveys
The tasks such as paint.
Above embodiment is the preferred embodiment of the utility model, not thereby limits the special of the utility model
Sharp protection domain.Those skilled in the art belonging to any the utility model, it is disclosed in the utility model not departing from
The equivalent structure and the conversion of equivalent step done to the content of the utility model on the premise of spirit and scope each falls within this reality
Within new claimed the scope of the claims.
Claims (10)
1. multi-rotor unmanned aerial vehicle, which is characterized in that including：Middle armature assembly (1), attachment device (2) and rotor group device (3), institute
The center that middle armature assembly (1) is located at multi-rotor unmanned aerial vehicle is stated, including power battery pack and aircraft control system；
The attachment device (2) is fixedly connected with middle armature assembly (1), including carbon pipe (4) and triangle joint device (5)；
The rotor group device (3) is fixed in attachment device (2), including motor and propeller.
2. multi-rotor unmanned aerial vehicle according to claim 1, which is characterized in that the middle armature assembly (1) further include fuel tank and
Aircraft control system.
3. multi-rotor unmanned aerial vehicle according to claim 2, which is characterized in that the rotor group device (3), which further includes, starts
Machine and propeller.
4. multi-rotor unmanned aerial vehicle according to claim 1, which is characterized in that the number of the attachment device (2) is even number.
5. multi-rotor unmanned aerial vehicle according to claim 4, which is characterized in that the number of the attachment device (2) is 4.
6. multi-rotor unmanned aerial vehicle according to claim 5, which is characterized in that the number of the propeller is 4 (2n-1)。
7. multi-rotor unmanned aerial vehicle according to claim 1, which is characterized in that the multi-rotor unmanned aerial vehicle further includes undercarriage
And carrying apparatus.
8. multi-rotor unmanned aerial vehicle according to claim 7, which is characterized in that the carrying apparatus is medicine-chest.
9. multi-rotor unmanned aerial vehicle according to claim 7, which is characterized in that the carrying apparatus is camera.
10. multi-rotor unmanned aerial vehicle according to claim 1, which is characterized in that the triangle joint device (5) can roll over
It is folded.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720703119.4U CN207417138U (en) | 2017-06-16 | 2017-06-16 | Multi-rotor unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720703119.4U CN207417138U (en) | 2017-06-16 | 2017-06-16 | Multi-rotor unmanned aerial vehicle |
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| Publication Number | Publication Date |
|---|---|
| CN207417138U true CN207417138U (en) | 2018-05-29 |
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ID=62399105
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201720703119.4U Active CN207417138U (en) | 2017-06-16 | 2017-06-16 | Multi-rotor unmanned aerial vehicle |
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| Country | Link |
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| CN (1) | CN207417138U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107097945A (en) * | 2017-06-16 | 2017-08-29 | 北京猎鹰无人机科技有限公司 | multi-rotor unmanned aerial vehicle |
-
2017
- 2017-06-16 CN CN201720703119.4U patent/CN207417138U/en active Active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107097945A (en) * | 2017-06-16 | 2017-08-29 | 北京猎鹰无人机科技有限公司 | multi-rotor unmanned aerial vehicle |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20200824 Address after: No.4 factory building, Fuyang industrial square, Fuyuan Road, Chengyang street, Xiangcheng economic and Technological Development Zone, Suzhou City, Jiangsu Province Patentee after: Aerospace Zhongxing (Jiangsu) Technology Co., Ltd Address before: Room 1003-1, building 7, No. 98, lianshihu West Road, Mentougou District, Beijing Patentee before: BEIJING FALCON UAV TECHNOLOGY Co.,Ltd. |
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| TR01 | Transfer of patent right | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20211227 Address after: 102407 466, block D, Beijing fund town building, Fangshan District, Beijing Patentee after: Aerospace Zhongxing (Beijing) Technology Co.,Ltd. Address before: 215137 plant 4, Fuyang industrial square, Fuyuan Road, Chengyang street, Xiangcheng economic and Technological Development Zone, Suzhou City, Jiangsu Province Patentee before: Aerospace Zhongxing (Jiangsu) Technology Co., Ltd |
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| TR01 | Transfer of patent right |