CN207208470U - A kind of modular unmanned plane of dynamical system - Google Patents
A kind of modular unmanned plane of dynamical system Download PDFInfo
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- CN207208470U CN207208470U CN201720802416.4U CN201720802416U CN207208470U CN 207208470 U CN207208470 U CN 207208470U CN 201720802416 U CN201720802416 U CN 201720802416U CN 207208470 U CN207208470 U CN 207208470U
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Abstract
The modular unmanned plane of a kind of dynamical system provided by the utility model, including at least one modular power system being installed in the unmanned plane frame, the modular power system includes motor, electron speed regulator, electrokinetic cell and the micro control unit being installed on modular power system casing, and the motor, the electron speed regulator and micro control unit are connected on the electrokinetic cell.By by dynamical system modularization, making the assembling of unmanned plane more convenient, the assembly cost of unmanned plane is greatly reduced；Its convenience is also convenient for reusing the module, every to use the power module, still can be with versatile power system module even if aircraft form is different；Assembling is freer, and the free degree is higher.
Description
Technical field
The utility model belongs to unmanned plane dynamic field, more particularly to a kind of modular unmanned plane of dynamical system.
Background technology
Unmanned plane is a kind of unmanned vehicle manipulated by radio robot or itself presetting apparatus.Nothing
Man-machine widely used, cost is low, and efficiency-cost ratio is good；Risk that no one was injured；Survival ability is strong, and mobility is good, easy to use,
There is extremely important effect in modern war, more held out broad prospects in civil area.
The dynamical system of modern middle-size and small-size electronic unmanned plane generally has two kinds of motor and internal combustion engine, wherein using motor as
Main, electronic dynamical system mainly includes electricity mechanical, electrical tune (controlled motor rotating speed), propeller and battery.In electronic unmanned plane
In, energy storage device (such as battery) is placed in unmanned aerial vehicle body position, and then power cable is parallel in energy storage device, if flown
Machine uses multiple power set, and such as multi-rotor unmanned aerial vehicle, dynamical system will produce multiple in parallel with energy storage device.
Due to multiple dynamical systems being connected in parallel with energy storage device, unmanned aerial vehicle design and the freedom of assembling are reduced
Degree, adds the network complexity in system assembles so that traditional unmanned aerial vehicle design is once it is determined that good unmanned plane form, subsequently
Can not freely it change again；And because it is integrated design, assembling needs to carry out after in place in all devices, reduces group
Speed is filled, meanwhile, after unmanned plane damage, in view of its complicated connection, safeguards that with what is changed will be a complete machine, rather than
Individually damage mechanism, difficulty is brought for maintenance.
Utility model content
For the above-mentioned technical problem of prior art, the purpose of this utility model is to propose that a kind of dynamical system is modular
Unmanned plane, it is intended to solve in existing unmanned plane especially multi-power system unmanned plane that parallel line is more and numerous and diverse on energy storage device,
Maintenance difficult and the problem of can not freely change.
To solve the above problems, the utility model provides technical scheme：
A kind of modular unmanned plane of dynamical system, including at least one modularization being installed in the unmanned plane frame
Dynamical system, the modular power system include being installed on motor on modular power system casing, electron speed regulator, dynamic
Power battery and micro control unit, the motor, the electron speed regulator and micro control unit are connected on the electrokinetic cell.
Further, in addition to propeller, the propeller are arranged on the power transmission shaft of the motor by buckle or screw
On.
Further, the electrokinetic cell is detachably installed in the modular power system casing.
Further, the electrokinetic cell is any in lithium battery, solar cell or hydrogen fuel cell.
Further, in addition to USB interface, the USB interface be installed on the modular power system casing and with
Micro control unit connects.
Further, the USB interface is USB Type-C interfaces.
Further, in addition to propeller protective cover, the propeller protective cover are installed on the modular power system
Top on housing, for protecting propeller.
Further, the motor selects brushless electric machine, and the electron speed regulator selects brushless electronic speed regulator.
Further, the quantity for the modular power system being installed in the unmanned plane frame is any in 1-16.
Further, in addition to master controller, the modular power system pass through the wired or wireless and main control
Device communication connection.
The modular unmanned plane of a kind of dynamical system provided by the utility model, including it is at least one be installed on it is described nobody
Modular power system in machine frame, the modular power system include the electricity being installed on modular power system casing
Mechanical, electrical sub- speed regulator, electrokinetic cell and micro control unit, the motor, the electron speed regulator and micro control unit are connected on described
On electrokinetic cell.By by dynamical system modularization, making the assembling of unmanned plane more convenient, the group of unmanned plane is greatly reduced
Dress up this；Its convenience is also convenient for reusing the module, every to use the power module, even if aircraft form is different,
Still can be with versatile power system module；Assembling is freer, and the free degree is higher.
Brief description of the drawings
Fig. 1 is the composition and wiring diagram of the dynamical system module of the utility model embodiment；
Fig. 2 is the structural representation of the dynamical system of the unmanned plane of the utility model embodiment；
Fig. 3 is the dynamical system and flight line graph of the unmanned plane of the utility model embodiment.
Embodiment
The technical solution of the utility model is clearly and completely described below in conjunction with accompanying drawing, it is clear that described
Embodiment is the utility model part of the embodiment, rather than whole embodiments.Based on the embodiment in the utility model, sheet
The every other embodiment that field those of ordinary skill is obtained under the premise of creative work is not made, belongs to this practicality
Novel protected scope.
, it is necessary to explanation in description of the present utility model, term " " center ", " on ", " under ", it is "left", "right", " perpendicular
Directly ", the orientation of the instruction such as " level ", " interior ", " outer " or position relationship are based on orientation shown in the drawings or position relationship, are only
Described for the ease of description the utility model and simplifying, rather than instruction or imply signified device or element must have it is specific
Orientation, with specific azimuth configuration and operation, therefore it is not intended that to limitation of the present utility model.In addition, term " the
One ", " second ", " the 3rd " are only used for describing purpose, and it is not intended that instruction or hint relative importance.
, it is necessary to which explanation, unless otherwise clearly defined and limited, term " are pacified in description of the present utility model
Dress ", " connected ", " connection " should be interpreted broadly, for example, it may be fixedly connected or be detachably connected, or integratedly
Connection；Can be mechanical connection or electrical connection；Can be joined directly together, can also be indirectly connected by intermediary,
It can be the connection of two element internals.For the ordinary skill in the art, above-mentioned art can be understood with concrete condition
Concrete meaning of the language in the utility model.
As shown in Figure 1-2, the modular unmanned plane of a kind of dynamical system, including at least one it is installed on the unmanned plane machine
Modular power system on frame, the modular power system include the motor being installed on modular power system casing 1
5th, electron speed regulator 4, electrokinetic cell 1 and micro control unit 3, the motor, the electron speed regulator and micro control unit are connected on institute
State on electrokinetic cell.The dynamical system of unmanned plane is related to the cruising time of unmanned plane complete machine, influences unmanned plane power supply reaction speed
Rate, therefore the importance of dynamical system can not interfere.One complete unmanned plane dynamical system comprises at least motor, electronics is adjusted
Fast device, micro control unit and electrokinetic cell, wherein the micro control unit assume responsibility for electron speed regulator control, current protection, battery,
2.4g networking functions, unmanned plane are rotated by micro control unit controlled motor and drive propeller rotation production by the output shaft of motor
Raw downward motive force promotes unmanned plane lift-off, but individually motor can not directly work, it is necessary to coordinate electron speed regulator, institute
State the rotating speed that electron speed regulator is used for controlled motor；Electrokinetic cell is then powered for above-mentioned part components, it is completed various instructions.
In the present embodiment, by avoiding motor, electron speed regulator, micro control unit and power battery module on electrokinetic cell
A plurality of power line in parallel, makes an electrokinetic cell only to a line powering, make connection more succinct, meanwhile, it is right
In the unmanned unit of more rotors, technical staff can according to needed for voluntarily selecting the demand of oneself dynamical system module quantity, give
The assembling of unmanned plane offers convenience, and greatly reduces the assembly cost of unmanned plane；Its convenience is also convenient for reusing the module,
It is every to use the power module, still can be with versatile power system module even if aircraft form is different；Assembling is freer,
The free degree is higher.
Further, in addition to propeller 6, the propeller are arranged on the power transmission shaft of the motor by buckle or screw
On.Propeller is the direct part for producing thrust, coordinates the motor, the electron speed regulator, the common liter for completing unmanned plane
Empty, advance and steering etc..
Further, in the present embodiment, the electrokinetic cell is detachably installed in the modular power system casing；
The electrokinetic cell is any in lithium battery, solar cell or hydrogen fuel cell.For the ease of to the power battery charging,
In the present embodiment, the electrokinetic cell is detachably set with the modular power system；The energy density of hydrogen fuel cell is very
Height, power density is smaller, accordingly relatively slow, is not suitable for moment high power discharge, but can be discharged for a long time under certain power；Too
Sun energy battery absorbs solar radiation by solar panels and is used as the propulsion energy, improves the time of continuation of the journey, but need enough
Surface area to absorb energy；The energy density of lithium battery is relatively low, and power density is very high, and response is fast, is adapted to changed power larger
And the situation of momentary high power electric discharge；In general, cut both ways, in the present embodiment, technical staff is according to the need of oneself
Voluntarily to select.
Further, in the present embodiment, in addition to USB interface 7, the USB interface are installed on the modular power
It is connected on system casing and with micro control unit；The USB interface is USB Type-C interfaces.In the present embodiment, the modularization
Dynamical system connects with flight controller communication, and UAV Flight Control device is to refer to stablize unmanned plane during flying posture, and energy
Control unmanned plane autonomous or the control system of semi-autonomous flight, in the present embodiment, flight controller can be moved by the modularization
Wireless module described in Force system in micro control unit realizes wireless connection, can also be controlled certainly by USB interface and the flight
Device wired connection processed, further, use USB Type-C interfaces；The characteristics of Type-C two-sided inserting interface maximums is to support
The two-sided insertion of USB interface, formally solves the global problem of " the eternal inaccurate plugs of USB ", and positive and negative is at will inserted.Match somebody with somebody simultaneously with it
Covering the USB data line used also must be thinner and lighter.
Further, in the present embodiment, in addition to propeller protective cover 8, the propeller protective cover are installed on described
Top on modular power system casing, for protecting propeller.
Further, the motor selects brushless electric machine, and the electron speed regulator selects brushless electronic speed regulator.As having
The upgrading products of brush motor, brushless electric machine are made up of motor body and driver, are a kind of typical electromechanical integrated products,
Because brushless motor is run with autocontrol, so will not turn as the synchronous motor of heavy load starting under frequency control
Another plus startup winding, will not also produce vibration and step-out in load changing on son.Compared to brush motor, brushless electric machine ratio has
Brush motor long lifespan, starting energetically power saving.Corresponding, also correspondence selects brushless electronic speed regulator to the electron speed regulator.
As shown in figure 3, further, the quantity for the modular power system being installed in the unmanned plane frame is 1-16
In it is any.In the prior art, unmanned plane has been distinguished also according to the quantity of propeller, the number of axle of multiaxis unmanned plane, is opened from two axles
Begin, have to ten axles, but it is common or based on 3,4,6,8 axles.In the utility model, the propeller and electricity are mechanical, electrical
Pond comprising modules together with electron speed regulator, therefore, according to the quantity of propeller, the module being installed in the unmanned plane frame
The quantity for changing dynamical system is any in 1-16.
In the above-described embodiments, the unmanned plane also includes flight controller, and it is to refer to stablize nobody that unmanned plane, which flies control,
Machine flight attitude, and unmanned plane can be controlled autonomous or the control system of semi-autonomous flight, the micro control unit is controlled with the flight
Device processed electrically connects, for receiving the control signal of the flight controller.Further, on the flight controller with earth station
Communication connection, the earth station are used for the airflight state of remotely pilotless machine；Dynamical system module and nothing are describe only herein
Communication annexation between man-machine flight control system and earth station, does not make improvements, here is omitted to flight control system.
Finally it should be noted that：Various embodiments above is only to illustrate the technical solution of the utility model, rather than it is limited
System；Although the utility model is described in detail with reference to foregoing embodiments, one of ordinary skill in the art should
Understand：It can still modify to the technical scheme described in foregoing embodiments, either to which part or whole
Technical characteristic carries out equivalent substitution；And these modifications or replacement, the essence of appropriate technical solution is departed from this practicality newly
The scope of each embodiment technical scheme of type.
Claims (10)
1. a kind of modular unmanned plane of dynamical system, it is characterised in that be installed on the unmanned plane frame including at least one
On modular power system, the modular power system include be installed on it is electric mechanical, electrical on modular power system casing
Sub- speed regulator, electrokinetic cell and micro control unit, the motor, the electron speed regulator and micro control unit are connected on the power electric
Chi Shang.
2. the modular unmanned plane of dynamical system according to claim 1, it is characterised in that described also including propeller
Propeller is arranged on the power transmission shaft of the motor by buckle or screw.
3. the modular unmanned plane of dynamical system according to claim 1 or 2, it is characterised in that the electrokinetic cell in
The modular power system casing is detachably installed.
4. the modular unmanned plane of dynamical system according to claim 3, it is characterised in that the electrokinetic cell is lithium electricity
It is any in pond, solar cell or hydrogen fuel cell.
5. the modular unmanned plane of dynamical system according to claim 1 or 2, it is characterised in that also including USB interface,
The USB interface is installed on the modular power system casing and is connected with micro control unit.
6. the modular unmanned plane of dynamical system according to claim 5, it is characterised in that the USB interface is USB
Type-C interfaces.
7. the modular unmanned plane of dynamical system according to claim 2, it is characterised in that also protected including propeller
Cover, the propeller protective cover is installed on the modular power system casing top, for protecting propeller.
8. the modular unmanned plane of dynamical system according to claim 1 or 2, it is characterised in that the motor selects nothing
Brush motor, the electron speed regulator select brushless electronic speed regulator.
9. the modular unmanned plane of dynamical system according to claim 1 or 2, it is characterised in that be installed on it is described nobody
The quantity of modular power system in machine frame is any in 1-16.
10. the modular unmanned plane of dynamical system according to claim 5, it is characterised in that also including master controller, institute
Modular power system is stated to connect with master controller communication by wired or wireless.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720802416.4U CN207208470U (en) | 2017-07-04 | 2017-07-04 | A kind of modular unmanned plane of dynamical system |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720802416.4U CN207208470U (en) | 2017-07-04 | 2017-07-04 | A kind of modular unmanned plane of dynamical system |
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| Publication Number | Publication Date |
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| CN207208470U true CN207208470U (en) | 2018-04-10 |
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Cited By (2)
| 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 |
| CN110383998A (en) * | 2018-04-17 | 2019-10-29 | 浙江派尼尔科技股份有限公司 | The automatic pruner of high altitude operation |
-
2017
- 2017-07-04 CN CN201720802416.4U patent/CN207208470U/en active Active
Cited By (2)
| 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 |
| CN110383998A (en) * | 2018-04-17 | 2019-10-29 | 浙江派尼尔科技股份有限公司 | The automatic pruner of high altitude operation |
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| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| TR01 | Transfer of patent right | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20191203 Address after: Room d1203, floor 11, building D, No. 9, Shangdi Third Street, Haidian District, Beijing 100036 Patentee after: BEIJING AIQI TECHNOLOGY CO., LTD. Address before: 050000 No. 501, Unit 3, Building No. 18, Chaoxia Street, Xinhua District, Shijiazhuang City, Hebei Province Patentee before: Zhang Yang |