CN206766345U - A kind of four rotor wing unmanned aerial vehicles with crawl function - Google Patents
A kind of four rotor wing unmanned aerial vehicles with crawl function Download PDFInfo
- Publication number
- CN206766345U CN206766345U CN201720418325.0U CN201720418325U CN206766345U CN 206766345 U CN206766345 U CN 206766345U CN 201720418325 U CN201720418325 U CN 201720418325U CN 206766345 U CN206766345 U CN 206766345U
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- China
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- mainboard
- unmanned aerial
- aerial vehicles
- horn
- rotor wing
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Abstract
A kind of four rotor wing unmanned aerial vehicles with crawl function disclosed in the utility model, including main machine body, are evenly distributed with some cantilevers for one week along main machine body, horn are respectively connected with each cantilever, each horn end is respectively provided with power plant module；Main machine body includes the mainboard a and mainboard b by reinforcing plate Joint, is provided with inertial measuring unit, battery and receiver in the cavity between mainboard a and mainboard b, one group of undercarriage and placement unit are also connected with mainboard b.The utility model unmanned plane significantly reduces total quality by using the main machine body of engraved structure；The cantilever with rotary buckle is employed, enables horn and main machine body relative motion, reduces storage space, it is easy to carry；It can realize that the flat of unmanned plane flies and VTOL using the gripper of easy folding and unfolding, while using the four outstanding wings, landing during operation in the wild can be advantageous to, be easy to positioning and crawl to object, there is good use value.
Description
Technical field
The utility model belongs to unmanned plane equipment technical field, and in particular to it is a kind of have crawl function four rotors nobody
Machine.
Background technology
UAV referred to as " unmanned plane ", is manipulated using radio robot and the presetting apparatus provided for oneself
Not manned vehicle, from technical standpoint definition can be divided into：Depopulated helicopter, unmanned fixed-wing aircraft, nobody more rotor flyings
Device, unmanned airship, several major classes of unmanned parasol.Compared with manned aircraft, it have small volume, low cost, it is easy to use, to make
The advantages that war environmental requirement is low, battlefield survival is stronger.
Existing unmanned multi-rotor unmanned aerial vehicle is all confined to take photo by plane mostly, aerial survey, agricultural plant protection, the field such as power-line patrolling；
And for some dangerous fields, for example high-altitude crawl etc., in use due to reasons such as position inaccurates, deposit
Capturing the problem of function is inaccurate.
Utility model content
The purpose of this utility model is to provide a kind of four rotor wing unmanned aerial vehicles with crawl function, solves existing unmanned plane
The problem of target crawl function is inaccurate.
The utility model is the technical scheme adopted is that a kind of have four rotor wing unmanned aerial vehicles for capturing function, including main frame
Body, some cantilevers are evenly distributed with one week along main machine body, horn is respectively connected with each cantilever, each horn end is respectively provided with dynamic
Power module；
Main machine body includes the mainboard a and mainboard b by reinforcing plate Joint, is set in the cavity between mainboard a and mainboard b
There are the inertial measuring unit being sequentially connected by wire, battery and receiver, one group of undercarriage and crawl are also connected with mainboard b
Unit.
It is of the present utility model to be further characterized in that,
Each cantilever surfaces are connected with rotary buckle, and rotary buckle is engaged with the buckle on each horn.
The quantity of cantilever is no less than 4, and identical with the quantity of horn.
Power plant module includes the motor cabinet being arranged on each horn, and motor, Mei Ge electricity are connected with each motor cabinet
Propeller is socketed with the main shaft of machine, each motor is connected with battery.
The angle of each undercarriage and mainboard b is 30 ° -40 °.
Placement unit includes pull bar, and pull bar one end is connected with the base being fixed on mainboard b, and the pull bar other end is provided with circle
The tension board of plate-like, several buckles are evenly distributed with one week along tension board, mechanical calvus is respectively connected with each buckle；
Sleeve is also socketed with pull bar, is evenly distributed with one week some fixed mounts along sleeve bottom, each fixed mount is logical
Cross the vertical corresponding mechanical calvus of linkage connection；
Steering wheel a and steering wheel b are also connected with base, steering wheel a and steering wheel b are connected by wire with receiver.
Mechanical calvus and linkage, the quantity all same of fixed mount.
The beneficial effects of the utility model are：A kind of four rotor wing unmanned aerial vehicles with crawl function of the utility model are by adopting
With the main machine body of engraved structure, total quality is significantly reduced；The cantilever with rotary buckle is employed, makes horn and main machine body
Energy relative motion, reduces storage space, easy to carry；Nothing can be realized using the gripper of easy folding and unfolding, while using the four outstanding wings
Man-machine flat winged and VTOL, can be advantageous to landing during operation in the wild, be easy to positioning and crawl to object, have
Good use value.
Brief description of the drawings
Fig. 1 is a kind of structural representation of four rotor wing unmanned aerial vehicles with crawl function of the utility model；
Fig. 2 is the structural representation of main machine body in a kind of four rotor wing unmanned aerial vehicles with crawl function of the utility model；
Fig. 3 is the structural representation of placement unit in a kind of four rotor wing unmanned aerial vehicles with crawl function of the utility model；
Fig. 4 is the decomposition texture signal of placement unit in a kind of four rotor wing unmanned aerial vehicles with crawl function of the utility model
Figure.
In figure, 1. main machine bodies, 1-1. mainboards a, 1-2. mainboard b, 1-3. inertial measuring unit, 1-4. batteries, 1-5. receptions
Machine, 1-6. reinforcing plates, 2. cantilevers, 2-1. rotary buckles, 3. horns, 3-1. buckles, 4. undercarriages, 5. motor cabinets, 6. motors, 7.
Propeller, 8. pull bars, 9. bases, 10. tension boards, 11. buckles, 12. mechanical calvus, 13. sleeves, 14. fixed mounts, 15. steering wheels
A, 16. steering wheel b, 17. bar a, 18. bar b.
Embodiment
The utility model is described in detail with reference to the accompanying drawings and detailed description.
A kind of four rotor wing unmanned aerial vehicles with crawl function of the utility model, as shown in figure 1, including main machine body 1, along main frame
Body is evenly distributed with some cantilevers 2 for 1 one weeks, and horn 3 is respectively connected with each cantilever 2, and each end of horn 3 is respectively provided with power mould
Block；
As shown in Fig. 2 main machine body 1 includes the mainboard a1-1 and mainboard b1-2 by reinforcing plate 1-6 Joints, mainboard a1-1
Inertial measuring unit 1-3, battery 1-4 and receiver that wire is sequentially connected are provided with cavity between mainboard b1-2
One group of undercarriage 4 and placement unit are also connected with 1-5, mainboard b1-2.
Each surface of cantilever 2 is connected with rotary buckle 2-1, rotary buckle 2-1 and the buckle 3- on each horn 3
1 is engaged, and rotary buckle 2-1 and buckle 3-1 make to relatively rotate between cantilever 2 and horn 3, and it is empty can not only to save storage
Between, and it is easy to carry.
The quantity of cantilever 2 is no less than 4, and identical with the quantity of horn 3, can realize that the flat of unmanned plane flies using the four outstanding wings
With VTOL, be advantageous to landing during operation in the wild, be easy to positioning and crawl to object.
Power plant module includes the motor cabinet 5 being arranged on each horn 3, is connected with motor 6 on each motor cabinet 5, often
Propeller 7 is socketed with the main shaft of individual motor 6, each motor 6 is connected with battery 1-4, and propeller is driven by motor 6
7 are rotated, and driving source is provided to unmanned plane.
Each undercarriage 4 and mainboard b1-2 angle is 30 ° -40 °, can effectively mitigate unmanned aerial vehicle body load-bearing, be easy to
The stability of landing.
As shown in Figure 3 and Figure 4, placement unit includes pull bar 8, and the one end of pull bar 8 connects with the base 9 being fixed on mainboard b1-2
Connect, the other end of pull bar 8 is provided with discoid tension board 10, is evenly distributed with 10 1 weeks several buckles 11 along tension board, often
Mechanical calvus 12 is respectively connected with individual buckle 11；Tension ring is provided with pull bar 8, bolt connects drawing with tension ring through base 9
Bar 8 and base 9, buckle 11 are flexibly connected mechanical calvus 12 by bearing pin；
Sleeve 13 is also socketed with pull bar 8, some fixed mounts 14 are evenly distributed with one week along 13 bottom of sleeve, it is each fixed
Frame 14 connects vertical corresponding mechanical calvus 12 by linkage, and sleeve 13 is protected to the pull bar 8 in it；Connecting rod machine
Structure includes movable connecting rod a17 and bar b18, and bar b18 and mechanical calvus 12 are affixed, and bar a17 is connected with fixed mount 14.
Also be connected with steering wheel a15 and steering wheel b16 on base 9, steering wheel a15 and steering wheel b16 by wire with receiver 1-5
Connection；Then steering wheel a15 and steering wheel b16 is moved by driving mechanical cat's paw 12, realized by receiving receiver 1-5 order
Mechanical cat's paw 12 is easy to effective crawl of target in three dimensions internal rotation.
Mechanical calvus 12 and linkage, the quantity all same of fixed mount 14.
The course of work of unmanned plane of the present utility model is as follows：
After energization, each motor 6 drives the setting in motion of propeller 7, and propeller 7 drives whole unmanned setting in motion, when need
When carrying out target crawl, external server sends to receiver 1-5 and ordered, now, under the work compound of motor 6, nobody
Machine is begun to decline, and after undercarriage 4 contacts ground, receiver 1-5 to steering wheel a15 and steering wheel b16 by sending order, steering wheel
The crawl of target is realized in foldings of the a15 and steering wheel b16 by adjusting mechanical cat's paw 12, completes the action of crawl.
The utility model unmanned plane significantly reduces total quality by using the main machine body 1 of engraved structure；Employ band
There is rotary buckle 2-1 cantilever 2, enable horn 3 and the relative motion of main machine body 1, reduce storage space, it is easy to carry；Using
The mechanical calvus 12 of easy folding and unfolding, while can realize that the flat of unmanned plane flies and VTOL using the four outstanding wings, it can be advantageous to out of office
Landing during outer operation, it is easy to positioning and crawl to object, there is good use value.
Claims (7)
1. a kind of four rotor wing unmanned aerial vehicles with crawl function, it is characterised in that including main machine body (1), along main machine body (1) one week
Some cantilevers (2) are evenly distributed with, horn (3) is respectively connected with each cantilever (2), each horn (3) end is respectively provided with power
Module；
Described main machine body (1) includes the mainboard a (1-1) and mainboard b (1-2), mainboard a (1- by reinforcing plate (1-6) Joint
1) inertial measuring unit (1-3), the battery (1-4) that wire is sequentially connected are provided with the cavity between mainboard b (1-2)
With receiver (1-5), one group of undercarriage (4) and placement unit are also connected with described mainboard b (1-2).
A kind of 2. four rotor wing unmanned aerial vehicles with crawl function according to claim 1, it is characterised in that described in each
Cantilever (2) surface is connected with rotary buckle (2-1), rotary buckle (2-1) and the buckle (3-1) on each horn (3)
It is engaged.
A kind of 3. four rotor wing unmanned aerial vehicles with crawl function according to claim 1, it is characterised in that described cantilever
(2) quantity is no less than 4, and identical with the quantity of horn (3).
A kind of 4. four rotor wing unmanned aerial vehicles with crawl function according to claim 1, it is characterised in that described power
Module includes the motor cabinet (5) being arranged on each horn (3), and motor (6), Mei Ge electricity are connected with each motor cabinet (5)
Propeller (7) is socketed with the main shaft of machine (6), each described motor (6) is connected with battery (1-4).
A kind of 5. four rotor wing unmanned aerial vehicles with crawl function according to claim 1, it is characterised in that described in each
The angle of undercarriage (4) and mainboard b (1-2) is 30 ° -40 °.
A kind of 6. four rotor wing unmanned aerial vehicles with crawl function according to claim 1, it is characterised in that described crawl
Unit includes pull bar (8), and pull bar (8) one end is connected with the base (9) being fixed on mainboard b (1-2), and pull bar (8) other end is set
Discoid tension board (10) is equipped with, several buckles (11), each buckle (11) are evenly distributed with (10) one weeks along tension board
On be respectively connected with mechanical calvus (12)；
Sleeve (13) is also socketed with described pull bar (8), some fixed mounts are evenly distributed with one week along sleeve (13) bottom
(14), each fixed mount (14) connects vertical corresponding mechanical calvus (12) by linkage；
Steering wheel a (15) and steering wheel b (16) are also connected with described base (9), steering wheel a (15) and steering wheel b (16) pass through wire
It is connected with receiver (1-5).
A kind of 7. four rotor wing unmanned aerial vehicles with crawl function according to claim 6, it is characterised in that described machinery
Calvus (12) and linkage, the quantity all same of fixed mount (14).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720418325.0U CN206766345U (en) | 2017-04-20 | 2017-04-20 | A kind of four rotor wing unmanned aerial vehicles with crawl function |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720418325.0U CN206766345U (en) | 2017-04-20 | 2017-04-20 | A kind of four rotor wing unmanned aerial vehicles with crawl function |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206766345U true CN206766345U (en) | 2017-12-19 |
Family
ID=60635309
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201720418325.0U Expired - Fee Related CN206766345U (en) | 2017-04-20 | 2017-04-20 | A kind of four rotor wing unmanned aerial vehicles with crawl function |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206766345U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112061387A (en) * | 2020-09-10 | 2020-12-11 | 西安爱生技术集团公司 | Rotor wing mounting structure based on unmanned aerial vehicle wing |
-
2017
- 2017-04-20 CN CN201720418325.0U patent/CN206766345U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112061387A (en) * | 2020-09-10 | 2020-12-11 | 西安爱生技术集团公司 | Rotor wing mounting structure based on unmanned aerial vehicle wing |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20171219 Termination date: 20180420 |