CN207826539U - It can type recombined electronic unmanned vehicle and electronic unmanned vehicle group - Google Patents
It can type recombined electronic unmanned vehicle and electronic unmanned vehicle group Download PDFInfo
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- CN207826539U CN207826539U CN201820149077.9U CN201820149077U CN207826539U CN 207826539 U CN207826539 U CN 207826539U CN 201820149077 U CN201820149077 U CN 201820149077U CN 207826539 U CN207826539 U CN 207826539U
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- unmanned vehicle
- electronic unmanned
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Abstract
The utility model discloses can type recombined electronic unmanned vehicle and electronic unmanned vehicle group, wherein, electronic unmanned vehicle includes fuselage, girder, motor, propeller, electric magnetism absorbent strip, electromagnetic controller and flight control system, wherein, the section of fuselage is in regular hexagon, electric magnetism absorbent strip is symmetrically disposed on the middle part of each lateral surface of fuselage, girder is fixedly connected on the inside of fuselage, motor is fixed on the center of girder, for driving propeller to rotate, electromagnetic controller is connect with electric magnetism absorbent strip and flight control system respectively, for under the control of flight control system, electric magnetism absorbent strip is set to be powered or power off, flight control system is also connect with motor, working condition for controlling motor, electronic unmanned vehicle group is recombinated by the electronic unmanned vehicle of multi rack by electric magnetism absorbent strip.This can type recombined electronic unmanned vehicle electronic unmanned vehicle group can be reassembled into, according to mission requirements, loading capacity to improve cruise duration and loading capacity.
Description
Technical field
The utility model belongs to field of aerospace technology, specifically provide one kind can type recombined electronic unmanned vehicle and
Electronic unmanned vehicle group.
Background technology
Current electronic unmanned plane is being taken photo by plane, agricultural, plant protection, self-timer, express transportation, disaster relief, observation wild animal, is being supervised
Control infectious disease, mapping, news report, electric inspection process, the disaster relief, movies-making, manufacture romance etc. field have obtained widely answering
With greatly having expanded the purposes of unmanned plane itself, developed country is also in actively extension sector application and development unmanned air vehicle technique.
Cruise duration, the loading capacity for improving unmanned vehicle, are the emphasis in current unmanned vehicle R＆D process.Generally
Electronic unmanned vehicle rely solely on itself motor carry out job task, more power can not be obtained extend continuation of the journey
Time and voyage.
Utility model content
In consideration of it, the purpose of this utility model is to provide one kind type recombined electronic unmanned vehicle and to be weighed by described
The electronic unmanned vehicle group of group formula electronic unmanned vehicle composition, to solve, existing unmanned vehicle cruise duration is short, load-carrying
Measure the problems such as low.
The utility model on the one hand provide one kind can type recombined electronic unmanned vehicle, including：It is fuselage, girder, electronic
Machine, propeller, electric magnetism absorbent strip, electromagnetic controller and flight control system, wherein the section of fuselage is in regular hexagon, and electromagnetism is inhaled
Item is symmetrically disposed on the middle part of each lateral surface of fuselage, and girder is fixedly connected on the inside of fuselage, and motor is fixed on girder
Center, for driving propeller to rotate, electromagnetic controller is connect with electric magnetism absorbent strip and flight control system respectively, is used for
Under the control of flight control system, electric magnetism absorbent strip is set to be powered or power off, flight control system is also connect with motor, for controlling
The working condition of motor processed.
It is preferred that propeller includes propeller A and propeller B, propeller A and propeller B are symmetrically mounted on the upper of motor
Side and lower section form single-shaft double-propeller structure.
Further preferably, electromagnetic controller and flight control system are both secured on girder.
The utility model additionally provides a kind of electronic unmanned vehicle group, including it is multiple it is above-mentioned can it is type recombined it is electronic nobody fly
Row device, wherein it is described can type recombined electronic unmanned vehicle pass through its lateral surface in the middle part of be arranged electric magnetism absorbent strip connection.
It is preferred that it is described can type recombined electronic unmanned vehicle symmetrically connected by the electric magnetism absorbent strip being arranged in the middle part of its lateral surface
It connects.
It is provided by the utility model can the electric magnetism absorbent strip phase that can be arranged by its lateral surface of type recombined electronic unmanned vehicle
It connects, realizes that recombination, the power on/off of electric magnetism absorbent strip are controlled by electromagnetic controller, electromagnetic controller is carried out by flight control system
Control, the section of fuselage are in regular hexagon, are conducive to recombination that respectively can be between type recombined electronic unmanned vehicle.
It is provided by the utility model can type recombined electronic unmanned vehicle, electricity can be reassembled into according to mission requirements, loading capacity
Dynamic unmanned vehicle group.
Description of the drawings
Below in conjunction with the accompanying drawings and embodiment is described in further detail the utility model：
Fig. 1 be it is provided by the utility model can type recombined electronic unmanned vehicle vertical view；
Fig. 2 be it is provided by the utility model can type recombined electronic unmanned vehicle side view；
Fig. 3 is the structural schematic diagram of electronic unmanned vehicle group provided by the utility model.
Specific implementation mode
The utility model is further explained below in conjunction with specific embodiment, but does not limit to this practicality
It is novel.
As shown in Figure 1 and Figure 2, the utility model provide one kind can type recombined electronic unmanned vehicle, including：Fuselage 1,
Girder 2, motor 3, propeller, electric magnetism absorbent strip 5, electromagnetic controller 6 and flight control system 7, wherein the section of fuselage 1 is in
Regular hexagon, electric magnetism absorbent strip 5 are symmetrically disposed on the middle part of each lateral surface of fuselage 1, and girder 2 is fixedly connected on the interior of fuselage 1
Side, motor 3 is fixed on the center of girder 2, for driving propeller to rotate, electromagnetic controller 6 respectively with electric magnetism absorbent strip 5
It is connected with flight control system 7, under the control of flight control system 7, making electric magnetism absorbent strip 5 be powered or power-off, flight control
System 7 processed is also connect with motor 3, the working condition for controlling motor 3, wherein propeller includes propeller A41 and spiral shell
Rotation paddle B42, propeller A41 and propeller B42 are symmetrically mounted on above and below motor 3, form single-shaft double-propeller structure, excellent
Choosing, electromagnetic controller 6 and flight control system 7 are both secured on girder 2.
This can the electric magnetism absorbent strip that can be arranged by its lateral surface of type recombined electronic unmanned vehicle be connected with each other, realize weight
The power on/off of group, electric magnetism absorbent strip is controlled by electromagnetic controller, and electromagnetic controller is controlled by flight control system, and fuselage is cut
Face is in regular hexagon, utilizes recombination that respectively can be between type recombined electronic unmanned vehicle.
This can type recombined electronic unmanned vehicle operation principle it is as follows：Flight control system controls electric motor operation, into
And propeller rotation is controlled, provide the lift needed for flight for aircraft；When needing to recombinate multi rack time unmanned vehicle, flight
Control system control electromagnetic controller makes electromagnetism item be powered on, and then realizes multi rack time unmanned vehicle recombination, forms more rotations
The wing flies, and improves loading capacity and cruise duration.
As shown in figure 3, the utility model additionally provides a kind of electronic unmanned vehicle group, including it is multiple it is above-mentioned can be type recombined
Electronic unmanned vehicle, wherein it is described can type recombined electronic unmanned vehicle pass through its lateral surface in the middle part of be arranged electric magnetism absorbent strip
Connection, preferably symmetrical connection.
Wherein, the flight control mode of the electronic unmanned vehicle group includes the following two kinds：
1, respectively can type recombined electronic unmanned vehicle flight control system independent operating.
2, each flight control system that can be in type recombined electronic unmanned vehicle of electronic unmanned flight's unit is formed
For master control system, remaining flight control system is a point control system, described that control system is divided to be connect with master control system
And it works under the control of master control system.
As the improvement of technical solution, forming each of electronic unmanned flight's unit can be in type recombined electronic unmanned vehicle
Flight control system is connected with each other, and when original state, master control system is used as by a flight control system, other flight controls are
System is divides control system, and in flight course, master control system can set other flight control systems to main control system at any time
System, meanwhile, itself it is changed to a point control system.Specifically：When electronic unmanned flight's unit encounters urgent feelings in flight course
Condition, master control system can select the flight control system of other electronic unmanned vehicles as main control system as needed
System, meanwhile, the unmanned vehicle of failure can be abandoned by controlling the power-off realization of electromagnetism item or be withdrawn at random.
Specific embodiment of the present utility model is write according to progressive mode, and each embodiment party is highlighted
The difference of case, similar portion can be with cross-reference.
The embodiment of the utility model is elaborated above in conjunction with attached drawing, but the utility model is not limited to
The above embodiment can also not depart from the utility model within the knowledge of a person skilled in the art
Various changes can be made under the premise of objective.
Claims (5)
1. can type recombined electronic unmanned vehicle, which is characterized in that including：Fuselage (1), girder (2), motor (3), spiral
Paddle, electric magnetism absorbent strip (5), electromagnetic controller (6) and flight control system (7), wherein the section of fuselage (1) is in regular hexagon, electricity
Magnetism absorbent strip (5) is symmetrically disposed on the middle part of each lateral surface of fuselage (1), and girder (2) is fixedly connected on the inside of fuselage (1),
Motor (3) is fixed on the center of girder (2), and for driving propeller to rotate, electromagnetic controller (6) is inhaled with electromagnetism respectively
Item (5) and flight control system (7) connection, under the control of flight control system (7), make electric magnetism absorbent strip (5) be powered or
Power-off, flight control system (7) are also connect with motor (3), the working condition for controlling motor (3).
2. according to can type recombined electronic unmanned vehicle described in claim 1, it is characterised in that：Propeller includes propeller A
(41) it is symmetrically mounted on above and below motor (3) with propeller B (42), propeller A (41) and propeller B (42), shape
At single-shaft double-propeller structure.
3. according to can type recombined electronic unmanned vehicle described in claim 1, it is characterised in that：Electromagnetic controller (6) and flight
Control system (7) is both secured on girder (2).
4. electronic unmanned vehicle group, which is characterized in that including described in any one of multiple claims 1 to 3 can be type recombined
Electronic unmanned vehicle, wherein it is described can type recombined electronic unmanned vehicle pass through its lateral surface in the middle part of be arranged electric magnetism absorbent strip
Connection.
5. electronic unmanned vehicle group according to claim 4, it is characterised in that：It is described can type recombined electronic unmanned flight
Device is symmetrically connected by the electric magnetism absorbent strip being arranged in the middle part of its lateral surface.
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820149077.9U CN207826539U (en) | 2018-01-30 | 2018-01-30 | It can type recombined electronic unmanned vehicle and electronic unmanned vehicle group |
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| CN201820149077.9U CN207826539U (en) | 2018-01-30 | 2018-01-30 | It can type recombined electronic unmanned vehicle and electronic unmanned vehicle group |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108248844A (en) * | 2018-01-30 | 2018-07-06 | 沈阳航空航天大学 | It can type recombined electronic unmanned vehicle and electronic unmanned vehicle group |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108248844A (en) * | 2018-01-30 | 2018-07-06 | 沈阳航空航天大学 | It can type recombined electronic unmanned vehicle and electronic unmanned vehicle group |
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