CN206171808U - Modularization unmanned aerial vehicle - Google Patents
Modularization unmanned aerial vehicle Download PDFInfo
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- CN206171808U CN206171808U CN201621261680.3U CN201621261680U CN206171808U CN 206171808 U CN206171808 U CN 206171808U CN 201621261680 U CN201621261680 U CN 201621261680U CN 206171808 U CN206171808 U CN 206171808U
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Abstract
The utility model discloses a modularization unmanned aerial vehicle, including battery module, the frame module, central control module flies to control the module to and power module, connect each main module through the connector, the function of data transmission and structural connection is realized simultaneously to the plug connector, thereby realizes conveniently depositing and carrying. With traditional unmanned aerial vehicle modularized design, mitigate connections such as original loaded down with trivial details welding, bolt -up, fixed mode, remain the function maximum simplification of implementation structure simultaneously.
Description
Technical field
This utility model is related to unmanned air vehicle technique field, a kind of specifically disclosed Modularized unmanned machine.
Background technology
UAV referred to as " unmanned plane ", english abbreviation is " UAV ", using radio robot and is provided for oneself
The not manned aircraft that presetting apparatus is manipulated.With unmanned plane extensive application and progressively move towards daily life, nothing
The convenience of man-machine installation, maintenance gets growing concern for.
Patent CN 102416578A discloses a kind of wearable unmanned plane, is designed by a key folding structure, realizes nothing
Man-machine carrying convenient as wrist-watch.Patent CN204979241U discloses a kind of Novel portable unmanned plane device.
Patent CN105947210A discloses a kind of four axles folding unmanned plane, by first/second mobile jib, the first/the
Two wing components, winged control cabin component, cloud control cabin component, head assembly, four propeller components, several connectors compositions, it is special
Levy and be：First/second mobile jib is parallel；Fly the both sides of control cabin/cloud control cabin component, by connector, be mounted in first, second master
On bar；First/second wing component is set on first/second mobile jib；First/second propeller component is mounted in the second wing group
On part, the three/the quadruple screw propeller component is mounted on the first wing component；Head assembly is connected with cloud control cabin component.It has structure
Simply, it is easily manufactured, keep in repair it is convenient, foldable the features such as.Patent CN205396516U disclose a kind of unmanned plane fold with it is fast
Fast mounting structure, including main wing, dovetail type turntable, fuselage, wing-folding part, main shaft, hinge；Dovetail type turntable
Upper surface is connected with the lower surface of main wing in 90 °, and dovetail type turntable is connected with fuselage by main shaft, and the centre of main shaft sets
Have a through hole, main wing is located at body upper, wing-folding part is located at main wing top and by gemel connection, wing-folding part and
Main wing is parallel, and the burst of wing-folding part is respectively provided on two sides with bullet pin card button and bullet pin and leading edge alignment pin and leading edge is fixed
Position hole, play pin card button and bullet pin and leading edge alignment pin and leading edge location hole be used for wing-folding part outwards 180 ° of upset when
Mutual snapping simultaneously completes self-locking.It can quickly rotate wing, fold and be fixed on unmanned plane body specified location.
But above-mentioned research is still limited to easily folding storage, modular installation and removal are not carried out, so as to realize
Convenient storage and carrying.
Utility model content
The purpose of this utility model is to provide a kind of Modularized unmanned machine, its by unmanned plane be split as battery, frame, in
Five modules such as centre control, winged control and power, by plug connector physical connection and data transfer are realized, and by securing member reality
The now firm installation of each module, so as to realizing convenient storage and carrying.
This utility model provides a kind of Modularized unmanned machine, including
Battery module, for providing power supply；
Stand module, for supporting and fixing unmanned plane modules；
Central control module, in stand module, which is provided with power interface, be electrically connected with battery module；
Fly control module, the flight for unmanned plane during flying is controlled, and it passes through plug connector and is connected with central control module；With
And
Power plant module, for providing the power of unmanned plane during flying, including propeller, motor and electronic speed regulation plate, it passes through
Plug connector is connected with central control module.
Preferably, the outer end of electronic speed regulation plate is provided with motor, the inner of electronic speed regulation plate is provided with plug connector, with central control
Plug connector matches in the horizontal direction connection in module.
Preferably, flying the top that control module is arranged at central control module, the winged control plate flown in control module is provided with grafting
Part, is connected with plug connector in the vertical direction matching on central control module.
Preferably, the plug connector is pin hole plug-in plug connector.The interface of plug connector is both structural connection, is also several
According to transmission mouth.
Plug connector is a kind of plug-in electrical connection device, general sub-plug and socket two parts.By the profile of plug connector
And purposes, plug connector can be divided into circular plug seat, blue-ribbon connector, printed circuit board connector assembly, source jack-socket, headset plug
Seat, bananajack and tape cable connector etc..
Preferably, central control module is provided with the functions expanding interface of plug-in.Multi-function extension interface is using plug
Mode, is managed collectively by central control module, and Intelligent Recognition can be adapted to the application module of difference in functionality.
Preferably, stand module includes carbon fiber base plate, the electronic speed regulation plate of power plant module, the central authorities of central control module
Panel is removably connected on the carbon fiber base plate by securing member.
Preferably, offering vertical through hole on electronic speed regulation plate, electronic speed regulation plate is opened up in the horizontal both sides of lead to the hole site
The both sides for having the breach for accommodating tightening buckle, tightening buckle are placed in the breach, and are led to described in the top clamping of tightening buckle
Hole, securing member is connected from via bottoms through through hole and with tightening buckle.
Preferably, the securing member is offered and screw for the top bottom side of handss the turn of the screw, the through hole and tightening buckle
The screw thread of matching.
Preferably, it is the cylinder with vertical stricture of vagina that the handss of handss the turn of the screw twist end, and handss twist end with diameter greater than screw rod
Diameter.
Preferably, it is the font structure of falling T that the handss of handss the turn of the screw twist end, is easy to handss the turn of the screw also to have both the work of unmanned plane foot rest
With.
Fastened using handss the turn of the screw, installation process without the need for any instrument, additionally, unmanned plane foot rest is also had both in handss the turn of the screw
Effect.
The beneficial effects of the utility model have：
1st, the overall modularity of unmanned plane, is split as five modules such as battery, frame, central authorities' control, winged control and power, leads to
Cross connector and connect each main modular, plug connector realizes the function of data transfer and structure connection simultaneously, so as to realize conveniently
Storage and carrying.
2nd, traditional electron speed regulator, flight panel are integrated on circuit board, become module independent one by one, subtracted
Exempt from connection, the fixed forms such as original loaded down with trivial details welding, bolt fastening, reservation function realizes that structure farthest simplifies simultaneously.
3rd, fastened using handss the turn of the screw, installation process without the need for any instrument, additionally, unmanned plane foot rest is also had both in handss the turn of the screw
Effect.
This utility model is described further below in conjunction with the drawings and specific embodiments.
Description of the drawings
Fig. 1 is this utility model Modularized unmanned machine overall structure diagram.
Fig. 2 is this utility model Modularized unmanned machine overall structure decomposing schematic representation.
Fig. 3 is the structural representation of this utility model Modularized unmanned machine battery module.
Fig. 4 is the structural representation of this utility model Modularized unmanned machine stand module.
Fig. 5 is the structural representation of this utility model Modularized unmanned machine central control module.
Fig. 6 is that this utility model Modularized unmanned machine flies to control the structural representation of module.
Fig. 7 is the structural representation of this utility model Modularized unmanned mechanomotive force module.
Fig. 8 is that this utility model Modularized unmanned machine fastens the schematic diagram installed.
Fig. 9 is the socket connection schematic diagram of this utility model Modularized unmanned machine central control module and winged control module.
Figure 10 is the socket connection schematic diagram of this utility model Modularized unmanned machine central control module and power plant module.
In figure, 1- battery modules, 2- stand module, 3- central control modules, 4- flies control module, and 5- power plant modules, 6- is inserted
Fitting, 7- functions expanding interfaces；11- batteries, 12- battery supporting plates, 13- connection-pegs, 21- carbon fiber base plates, 22- handss twist spiral shell
Silk, 23- tightening buckles, 24- through holes, 25- breach, 31- power interfaces, 32- central control boards, the winged control plates of 41-, 50- trouserss,
51- propellers, 52- motors, 53- electronic speed regulation plates.
Specific embodiment
This utility model can be further well understood to by specific embodiment of the utility model given below, but
They are not to restriction of the present utility model.Part without detailed narration in specific embodiment is using prior art, known
What technological means and industry standard were obtained.
Embodiment 1
Incorporated by reference to referring to accompanying drawing 1 to 10, this utility model provides a kind of Modularized unmanned machine, including
Battery module 1, for providing power supply；
Stand module 2, for supporting and fixing unmanned plane modules；
Central control module 3, in stand module 2, which is provided with power interface 31, be electrically connected with battery module 1；
Fly control module 4, the flight for unmanned plane during flying is controlled, and it passes through plug connector 6 and is connected with central control module 3
Connect；And
Power plant module 5, for providing the power of unmanned plane during flying, including trouserss 50, propeller 51, motor 52 and electronics
Speed adjusting plate 53, it passes through plug connector 6 and is connected with central control module 3；
Wherein, battery module 1 includes battery 11, battery supporting plate 12 and connection-peg 13, connection-peg 13 and central authorities' control mould
The power interface 31 of block 3 is mutually inserted to realize being electrically connected with.
Wherein, the outer end of electronic speed regulation plate 53 is provided with motor 52, and the inner of electronic speed regulation plate 53 is provided with plug connector 6, with
Plug connector 6 matches in the horizontal direction connection in the control module 3 of centre；
Fly the top that control module 4 is arranged at central control module 3, the winged control plate 41 flown in control module 4 is provided with plug connector
6, it is connected with the in the vertical direction of plug connector 6 matching on central control module 3.
Plug connector is a kind of plug-in electrical connection device, general sub-plug and socket two parts.By the profile of plug connector
And purposes, plug connector can be divided into circular plug seat, blue-ribbon connector, printed circuit board connector assembly, source jack-socket, headset plug
Seat, bananajack and tape cable connector etc..This utility model adopts the interface of plug connector, is both structural connection,
It is data transmission mouth.Used as the preferred scheme of the present embodiment, the plug connector is pin hole plug-in plug connector.
Specifically, the inner of electronic speed regulation plate 53 is provided with plug connector 6 and plug connector 6 on central control module 3, can select
One of them is plug portion, then another is socket part, you can realizes matching connection, is both structural connection, is also several
According to transmission mouth.
Specifically, trouserss 50, propeller 51, motor 52 are motor of the prior art suit, by advance welding
Or be connected with electronic speed regulation plate 53 using inserting mode.
Wherein, stand module 2 includes carbon fiber base plate 21, the electronic speed regulation plate 53 of power plant module 5, central control module 3
Central control board 32 on the carbon fiber base plate 21, and removably connected by handss the turn of the screw 22.Handss the turn of the screw is only
It is one of fixed form that the present embodiment shows, can also be fixed by other securing members certainly.
The present embodiment is using the concrete reinforcing mode of handss the turn of the screw 22：
Vertical through hole 24 is offered on electronic speed regulation plate 53, electronic speed regulation plate 53 is opened up in the horizontal both sides of the position of through hole 24
The both sides for having the breach 25 for accommodating tightening buckle 23, tightening buckle 23 are placed in the breach 25, and the top of tightening buckle 23
Through hole 24 described in clamping, handss the turn of the screw 22 is connected from the bottom of through hole 24 through through hole 24 and with tightening buckle 23, the through hole 24
The screw thread matched with handss the turn of the screw 22 is offered with the top bottom side of tightening buckle 23；
In the present embodiment, it is the cylinder with vertical stricture of vagina that the handss of handss the turn of the screw 22 twist end, and handss twist end with diameter greater than
The diameter of screw rod.Fastened using handss the turn of the screw, installation process without the need for any instrument, additionally, unmanned under-chassis is also had both in handss the turn of the screw
The effect of frame.
The installation process of Modularized unmanned machine of the present utility model is：The carbon fiber base plate 21 of expansion stand module 2, and
The central control board 32 of central control module 3 is placed thereon.By the plug connector 6 on the electronic speed regulation plate 53 of power plant module 5 with
The matching of plug connector 6 grafting in the control module 3 of centre, that is, the grafting completed in horizontal direction is installed；Again by the winged control in winged control module 4
Plug connector 6 on plate 41 matches grafting with plug connector 6 on central control module 3, that is, the grafting completed in vertical direction is installed.
Finally, battery module 1 is positioned over and flies control module 4 top, and battery module 1 is plugged in into the power supply on central control module 3
In interface 31.Thereafter, tightening buckle 23 is fastened on electronic speed regulation plate 53, then is adjusted through electronics from bottom using handss the turn of the screw 22
Through hole 24 on fast plate 53 is simultaneously mutually threadedly coupled with tightening buckle 23.The He of power plant module 5 is made by tightening buckle 23 and handss the turn of the screw 22
The carbon fiber base plate 21 of stand module 2 is locked, and power plant module 5 and central control module 3 are completely fixed, overall without relative displacement
Structure becomes more to consolidate.
With reference to the description in accompanying drawing 1 to 10, it shows the modularization assembling situation that frame is X-type unmanned plane.But make
It is located for of the present utility model creation, the shape of all modules is not fixed, and the change of shape can occur according to product demand,
Such as, the carbon fiber board in stand module may also be employed H type structures, or even can also be using the various shapes such as center is round.
Embodiment 2
The Modularized unmanned machine of the present embodiment is substantially the same manner as Example 1, but plug is had additional on central control module 3
The functions expanding interface 7 of formula, referring specifically to accompanying drawing 5.Multi-function extension interface adopts pluggable mode, is united by central control module
One management, Intelligent Recognition can be adapted to the application module of difference in functionality.
Embodiment 3
The Modularized unmanned machine of the present embodiment is substantially the same manner as Example 1, but the handss of handss the turn of the screw twist end for the font of falling T knot
Structure, is easy to handss the turn of the screw also to have both the effect of unmanned plane foot rest.
Modularized unmanned machine of the present utility model has following features：
1st, using five big nucleus module designs：Power plant module, winged control module, central control module, stand module and battery
Module.Different from the unmanned plane spare and accessory parts for typically starting to assemble, Modularized unmanned machine of the present utility model has deleted all connections
Line part, using unified pin hole plug-in plug connector, interface is both structural connection, is also data transmission mouth.Twist with reference to handss
Screw, can easily realize dismounting, replace any part without using any instrument and technology, greatly reduce assembling difficulty.
2nd, in addition to basic module, Modularized unmanned machine is also equipped with Multi-function extension interface, using unified pluggable mode, passes through
Central control module is managed collectively, and Intelligent Recognition can be adapted to the application module of difference in functionality.
3rd, all module open ports, can be patterned programming, and user can develop according to the needs of oneself, improve
The interest of teaching practice, enriches unmanned plane education content, lifts Creative spaces.
4th, Modularized unmanned machine is compact to design, small volume, lightweight, low cost., away from up to 220mm, whole machine is (containing electricity for arbor
Pond) weight as little as 300g, no matter assembled formation or take apart, can conveniently storage with carry.
5th, fuselage is designed as X-type structure, using high-strength carbon fiber composite and 6061 aluminum alloy junction components, very big journey
Degree improves the crash resistance of this money unmanned plane.
Above disclosed is only preferred embodiment of the present utility model, can not limit this practicality with this certainly new
The interest field of type, therefore the equivalent variations made according to this utility model claim, still belong to this utility model and are covered
Scope.
Claims (10)
1. a kind of Modularized unmanned machine, it is characterised in that：Including
Battery module, for providing power supply；
Stand module, for supporting and fixing unmanned plane modules；
Central control module, in stand module, which is provided with power interface, be electrically connected with battery module；
Fly control module, the flight for unmanned plane during flying is controlled, and it passes through plug connector and is connected with central control module；And
Power plant module, for providing the power of unmanned plane during flying, including propeller, motor and electronic speed regulation plate, it passes through grafting
Part is connected with central control module.
2. Modularized unmanned machine according to claim 1, it is characterised in that：The outer end of electronic speed regulation plate is provided with motor, electricity
The inner of sub- speed adjusting plate is provided with plug connector, matches in the horizontal direction with plug connector on central control module and is connected.
3. Modularized unmanned machine according to claim 1, it is characterised in that：Fly control module and be arranged at central control module
Top, the winged control plate flown in control module is provided with plug connector, and with plug connector in the vertical direction on central control module company is matched
Connect.
4. the Modularized unmanned machine according to Claims 2 or 3, it is characterised in that：The interface of plug connector is both structure connection
Part, is also data transmission mouth.
5. Modularized unmanned machine according to claim 1, it is characterised in that：Central control module is provided with the work(of plug-in
Interface can be expanded.
6. Modularized unmanned machine according to claim 1, it is characterised in that：Stand module includes carbon fiber base plate, power
The electronic speed regulation plate of module, the central control board of central control module are located on the carbon fiber base plate, and can by securing member
The connection of dismounting.
7. Modularized unmanned machine according to claim 6, it is characterised in that：Vertical through hole is offered on electronic speed regulation plate,
Electronic speed regulation plate offers the breach for accommodating tightening buckle in the horizontal both sides of lead to the hole site, and the both sides of tightening buckle are placed in institute
State in breach, and through hole described in the top clamping of tightening buckle, securing member is connected from via bottoms through through hole and with tightening buckle.
8. Modularized unmanned machine according to claim 7, it is characterised in that：The securing member is handss the turn of the screw, described logical
The top bottom side of hole and tightening buckle offers the screw thread matched with screw.
9. Modularized unmanned machine according to claim 8, it is characterised in that：It is with vertical stricture of vagina that the handss of handss the turn of the screw twist end
Cylinder, and handss twist the diameter with diameter greater than screw rod at end.
10. Modularized unmanned machine according to claim 8, it is characterised in that：The handss of handss the turn of the screw twist end for the font of falling T knot
Structure.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621261680.3U CN206171808U (en) | 2016-11-24 | 2016-11-24 | Modularization unmanned aerial vehicle |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621261680.3U CN206171808U (en) | 2016-11-24 | 2016-11-24 | Modularization unmanned aerial vehicle |
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| CN206171808U true CN206171808U (en) | 2017-05-17 |
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Cited By (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107264792A (en) * | 2017-07-04 | 2017-10-20 | 张洋 | A kind of modular unmanned plane of dynamical system |
| CN108216629A (en) * | 2018-02-26 | 2018-06-29 | 西北工业大学 | A kind of combination transport unmanned plane |
| CN109229349A (en) * | 2017-07-11 | 2019-01-18 | 上海伯镭智能科技有限公司 | A kind of long endurance multi-rotor unmanned aerial vehicle |
| CN109823554A (en) * | 2019-04-02 | 2019-05-31 | 福建电力职业技术学院 | A kind of winged control cabin fast-detachable modular structure of unmanned plane |
| WO2019140660A1 (en) * | 2018-01-19 | 2019-07-25 | 深圳市大疆创新科技有限公司 | Fuselage and unmanned aerial vehicle comprising same |
| WO2019233060A1 (en) * | 2018-06-04 | 2019-12-12 | 广州市华科尔科技股份有限公司 | Control system and control method for oil-electric hybrid multi-rotor unmanned aerial vehicle |
| WO2020000206A1 (en) * | 2018-06-26 | 2020-01-02 | 深圳市大疆创新科技有限公司 | Unmanned aerial vehicle |
| WO2020073798A1 (en) * | 2018-10-10 | 2020-04-16 | 深圳市道通智能航空技术有限公司 | Mounting structure for flight control module, flight control assembly and unmanned aerial vehicle |
| WO2022120796A1 (en) * | 2020-12-11 | 2022-06-16 | 深圳市大疆创新科技有限公司 | Modular unmanned aerial vehicle and operation method therefor |
| TWI812533B (en) * | 2022-11-03 | 2023-08-11 | 信邦電子股份有限公司 | Modular aircraft and its control method |
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2016
- 2016-11-24 CN CN201621261680.3U patent/CN206171808U/en active Active
Cited By (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107264792A (en) * | 2017-07-04 | 2017-10-20 | 张洋 | A kind of modular unmanned plane of dynamical system |
| CN109229349A (en) * | 2017-07-11 | 2019-01-18 | 上海伯镭智能科技有限公司 | A kind of long endurance multi-rotor unmanned aerial vehicle |
| WO2019140660A1 (en) * | 2018-01-19 | 2019-07-25 | 深圳市大疆创新科技有限公司 | Fuselage and unmanned aerial vehicle comprising same |
| CN110300705A (en) * | 2018-01-19 | 2019-10-01 | 深圳市大疆创新科技有限公司 | Fuselage and unmanned plane including the fuselage |
| CN108216629A (en) * | 2018-02-26 | 2018-06-29 | 西北工业大学 | A kind of combination transport unmanned plane |
| WO2019233060A1 (en) * | 2018-06-04 | 2019-12-12 | 广州市华科尔科技股份有限公司 | Control system and control method for oil-electric hybrid multi-rotor unmanned aerial vehicle |
| WO2020000206A1 (en) * | 2018-06-26 | 2020-01-02 | 深圳市大疆创新科技有限公司 | Unmanned aerial vehicle |
| WO2020073798A1 (en) * | 2018-10-10 | 2020-04-16 | 深圳市道通智能航空技术有限公司 | Mounting structure for flight control module, flight control assembly and unmanned aerial vehicle |
| CN109823554A (en) * | 2019-04-02 | 2019-05-31 | 福建电力职业技术学院 | A kind of winged control cabin fast-detachable modular structure of unmanned plane |
| WO2022120796A1 (en) * | 2020-12-11 | 2022-06-16 | 深圳市大疆创新科技有限公司 | Modular unmanned aerial vehicle and operation method therefor |
| TWI812533B (en) * | 2022-11-03 | 2023-08-11 | 信邦電子股份有限公司 | Modular aircraft and its control method |
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