CN205469856U - Power supply module , Unmanned vehicles and remote control mobile device - Google Patents
Power supply module , Unmanned vehicles and remote control mobile device Download PDFInfo
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- CN205469856U CN205469856U CN201620151510.3U CN201620151510U CN205469856U CN 205469856 U CN205469856 U CN 205469856U CN 201620151510 U CN201620151510 U CN 201620151510U CN 205469856 U CN205469856 U CN 205469856U
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- 238000009434 installation Methods 0.000 claims abstract description 43
- 230000003447 ipsilateral effect Effects 0.000 claims description 4
- 230000005484 gravity Effects 0.000 claims description 3
- 238000012423 maintenance Methods 0.000 description 3
- 230000000712 assembly Effects 0.000 description 2
- 238000000429 assembly Methods 0.000 description 2
- 230000005540 biological transmission Effects 0.000 description 1
- 239000000446 fuel Substances 0.000 description 1
- 239000002917 insecticide Substances 0.000 description 1
- 238000013507 mapping Methods 0.000 description 1
- 230000001737 promoting effect Effects 0.000 description 1
- 230000005855 radiation Effects 0.000 description 1
- 239000007921 spray Substances 0.000 description 1
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Abstract
The utility model relates to a power supply module, unmanned vehicles and remote control mobile device unmanned vehicles. Power supply module includes mounting bracket, energy supply device and two at least functional modules, the mounting bracket sets up on the fuselage, energy supply device set up in on the mounting bracket, the mounting bracket includes two at least installation departments, two at least functional modules set up respectively in on two at least installation departments, and respectively with energy supply device electric connection. Above -mentioned power supply module's volume is less relatively and the dismouting is comparatively convenient.
Description
Technical field
This utility model relates to a kind of power supply module and the unmanned vehicle using this power supply module and remote-controlled movement device.
Background technology
Remote-controlled movement device, such as unmanned vehicle or automatic driving vehicle etc., generally comprise main frame mounting structure and be connected to control device, power supply device and the power set on described main frame mounting structure.User controls to control described in equipment remote-control device by remote controller etc., makes described control device control described power set and drives described remote-controlled movement device entirety to advance.Described power supply device is for providing energy source for described power set.Owing to the Miniaturization Design of described remote-controlled movement device needs, above-mentioned main frame mounting structure is usually: the most functional modules is integrated on a circuit board, and is arranged at by described circuit board in the casing of described remote-controlled movement device.But, owing to being integrated with all of functional module on described circuit board, make the above-mentioned assembling of main frame mounting structure, dismounting or inconvenient maintenance profit.
Utility model content
In view of the foregoing, it is necessary to provide a kind of volume relatively small and dismount remote-controlled movement device and power supply module thereof easily.
A kind of power supply module, including installing rack, power supply device and at least two functional module, described installing rack is arranged on described fuselage, and described power supply device is arranged on described installing rack；Described installing rack includes at least two installation portion.Described at least two functional module is respectively arranged on described at least two installation portion, and is electrically connected with described power supply device respectively.
Further, described installing rack is polyhedral structure, and described at least two installation portion lays respectively at the not ipsilateral of described installing rack；
And/or, described power supply module also includes the controller being connected on described installing rack, and described controller is flight controller or travel controller.
Further, described at least two functional module is respectively the circuit board for performing difference in functionality.
Further, described at least two functional module be following several at least one: speed sensing module, gravity sensing module, vision sensing module, sensing magnetic fields module, control module.
Further, described at least two functional module includes that first circuit board and second circuit board, described first circuit board and described second circuit board are separately positioned on the opposite sides of described installing rack.
Further, described power supply device is arranged in described installing rack, on the outer surface of the opposite sides that described first circuit board and described second circuit board are stacked in described installing rack respectively.
Further, described power supply module also includes that adaptor, described adaptor are arranged on one end of described installing rack, and is electrically connected with described power supply device.
Further, described adaptor is stacked on the outer surface of described installing rack, and relative two sides of described adaptor are respectively adjacent to described first circuit board and described second circuit board；
And/or, described adaptor is provided with standard interface, described standard interface is for being electrically connected with described power supply device.
Further, described at least two functional module also includes tertiary circuit plate, described tertiary circuit plate is arranged on described installing rack and is spaced with described second circuit board and described first circuit board respectively, and described tertiary circuit plate is electrically connected with described power supply device.
Further, described tertiary circuit plate is stacked on the outer surface of described installing rack, and three sides of described tertiary circuit plate are respectively adjacent to described first circuit board, described second circuit board and described adaptor.
Further, described power supply module also includes that controller, described controller are arranged at the side deviating from described installing rack of described tertiary circuit plate, and described controller is electrically connected with described power supply device.
Further, the opposite ends of the two ends the most described tertiary circuit plate of described controller is extended, and is electrically connected with described power supply device respectively；
And/or, described controller is flight controller or travel controller.
A kind of unmanned vehicle, including fuselage and as above power supply module described in any one, described power supply module is arranged on described fuselage.
Further, described fuselage is casing, and described power supply module is housed in described casing；
And/or, described unmanned vehicle also includes the motor being arranged on described fuselage and is arranged at the propeller on described motor.
Further, described fuselage includes upper casing and the lower casing mutually fastened, and described power supply module is arranged between described upper casing and described lower casing.
Further, described power supply module is fixedly installed on described upper casing, to form upper shell component with described upper casing.
Further, described unmanned vehicle also includes that at least one control piece, at least one control piece described are fixed on described lower casing, and corresponding to described installing rack.
Further, at least one control piece described includes the first control piece being stacked and placed on regularly on described lower casing, and described first control piece is circuit board.
Further, at least one control piece described also includes that the second control piece, described second control piece are stacked and placed on described first control piece, and described second control piece is circuit board.
Further, at least one control piece described is electrically connected with the load being mounted on described unmanned vehicle, and is used for controlling described loaded work piece.
Further, described unmanned vehicle also includes that radiating piece, described radiating piece are arranged on described lower casing adjacent to described control piece.
Further, at least one control piece described, described radiating piece are fixed on described lower casing respectively, to form lower shell component with described lower casing；
And/or, described lower casing includes that the first housing and the second housing, described first housing are interlocked with described upper casing and is connected, and described second housing is detachably mounted on described first housing；
And/or, described radiating piece is radiator fan.
Further, at least one control piece described, described radiating piece are fixed on described second housing respectively, in order at least one control piece described and the integrated assembling of described radiating piece.
Further, described first housing being provided with installing port, described installing port runs through described first housing the inner space with described fuselage, and described second case lid is located on described installing port.
Further, described lower casing includes that the first housing and the second housing, described first housing are interlocked with described upper casing, and described second housing is detachably mounted on described first housing.
Further, described first housing being provided with installing port, described installing port runs through described first housing the inner space with described fuselage, and described second case lid is located on described installing port；
And/or, described unmanned vehicle also includes that undercarriage, described undercarriage are arranged on described first housing of described fuselage, and extends towards the direction away from described fuselage.
Further, described unmanned vehicle being provided with image acquiring device, described image acquiring device is connected on described second housing of described fuselage.
Further, described unmanned vehicle also includes The Cloud Terrace, and described The Cloud Terrace can adjustably be arranged on described second housing, and described image acquiring device is arranged on described The Cloud Terrace.
A kind of remote-controlled movement device, including fuselage and as above power supply module described in any one, described power supply module is arranged on described fuselage.
Further, described remote-controlled movement device is automatic driving vehicle or unmanned boats and ships.
In sum, multiple described functional modules are arranged on described installing rack separated from one anotherly, enabling that the installation and debugging of multiple described functional module are separated from one another to be carried out, the debugging of the most described power supply module and maintenance, the dismounting also making described power supply module is more convenient.Meanwhile, the layout of power supply module is more rationalized, and reduces described remote-controlled movement device entirety and amasss, make the assembling of power supply module in described remote-controlled movement device, dismantle or keep in repair more convenient.
Accompanying drawing explanation
The schematic perspective view of the unmanned vehicle that Fig. 1 provides for this utility model embodiment.
Fig. 2 is the part-structure decomposing schematic representation of unmanned vehicle shown in Fig. 1.
Fig. 3 is the perspective exploded view of unmanned vehicle shown in Fig. 1.
Main element symbol description
| Unmanned vehicle | 1 |
| Fuselage | 100 |
| Upper shell component | 20 |
| Upper casing | 21 |
| Installing rack | 23 |
| First installation portion | 231 |
| Second installation portion | 233 |
| 3rd installation portion | 235 |
| 4th installation portion | 237 |
| Receiving space | 239 |
| Power supply device | 25 |
| Functional module | 27 |
| First circuit board | 271 |
| Second circuit board | 273 |
| Tertiary circuit plate | 275 |
| Controller | 28 |
| Adaptor | 29 |
| Interface | 291 |
| Lower shell component | 40 |
| Lower casing | 41 |
| First housing | 411 |
| Installing port | 4111 |
| Second housing | 413 |
| Host cavity | 42 |
| Control piece | 43 |
| First control piece | 431 |
| Second control piece | 433 |
| Radiating piece | 45 |
| Undercarriage | 60 |
| Power set | 300 |
| Motor | 310 |
| The Cloud Terrace camera | 400 |
| The Cloud Terrace | 410 |
| Image acquiring device | 430 |
Following detailed description of the invention will further illustrate this utility model in conjunction with above-mentioned accompanying drawing.
Detailed description of the invention
Below in conjunction with the accompanying drawing in this utility model embodiment, the technical scheme in this utility model embodiment is clearly and completely described, it is clear that described embodiment is only a part of embodiment of this utility model rather than whole embodiments.Based on the embodiment in this utility model, the every other embodiment that those of ordinary skill in the art are obtained under not making creative work premise, broadly fall into the scope of this utility model protection.
It should be noted that be referred to as " being fixed on " another assembly when assembly, it can be directly on another assembly or can also there is assembly placed in the middle.When an assembly is considered as " connection " another assembly, and it can be directly to another assembly or may be simultaneously present assembly placed in the middle.When an assembly is considered as " being arranged at " another assembly, and it can be to be set directly on another assembly or may be simultaneously present assembly placed in the middle.Term as used herein " vertical ", " level ", "left", "right" and similar statement are for illustrative purposes only.
Unless otherwise defined, all of technology used herein and scientific terminology are identical with belonging to the implication that those skilled in the art of the present utility model are generally understood that.It is intended merely to describe the purpose of specific embodiment at term used in the description of the present utility model herein, it is not intended that in limiting this utility model.Term as used herein " and/or " include the arbitrary and all of combination of one or more relevant Listed Items.
Below in conjunction with the accompanying drawings, embodiments more of the present utility model are elaborated.In the case of not conflicting, the feature in following embodiment and embodiment can be mutually combined.
Refer to Fig. 1 and Fig. 2, this utility model embodiment provides a kind of remote-controlled movement device, described remote-controlled movement device can be but be not limited to as unmanned vehicle, unmanned vehicle or unmanned boat etc., and in the present embodiment, described remote-controlled movement device is as a example by unmanned vehicle 1.Described unmanned vehicle 1 includes that fuselage 100 and power set 300, described power set 300 are arranged on described fuselage 100, and for providing the power of flight for described unmanned vehicle 1.In the present embodiment, described unmanned vehicle 1 is used for carrying The Cloud Terrace camera 400 and carries out shooting operation, and described The Cloud Terrace camera 400 can include The Cloud Terrace 410 and be arranged at the image acquiring device 430 on described The Cloud Terrace 410.
Described fuselage 100 includes shell component 20, lower shell component 40 and undercarriage 60.Concrete described upper shell component 20 and described lower shell component 40 mutually fasten to be formed the casing of described unmanned vehicle 1, and described undercarriage 60 is arranged on described lower shell component 40 in the illustrated embodiment, and are used as support when described unmanned vehicle 1 lands.
Please refer to Fig. 3, described lower shell component 40 includes lower casing 41, control piece 43 and radiating piece 45.It is concrete that the most described control piece 43 and described radiating piece 45 are arranged on described lower casing 41, and described lower casing 41 and described between shell component 20.
The housing shape that described lower casing 41 is the most concave, it is formed host cavity 42.Described lower casing 41 houses the parts of described unmanned vehicle 1 for matching with described upper shell component 20.In the present embodiment, described lower casing 41 includes the first housing 411 and the second housing 413 being connected with described first housing 411.The approximate mid-section position of described first housing 411 offers installing port 4111, and described installing port 4111 is connected with described host cavity 42.Described second housing 413 is arranged on described installing port 4111, and closes described installing port 4111.By dismantling and installing described second housing 413, described installing port 4111 can be turned on and off easily, allow users to check or safeguard the parts within described fuselage 100 easily.
In the present embodiment, described second housing 413 is additionally operable to install described The Cloud Terrace camera 400.Specifically, described The Cloud Terrace 410 is arranged on described second housing 413 and deviates from the side of described host cavity 42, and described image acquiring device 430 is arranged on described The Cloud Terrace 410.It is appreciated that described The Cloud Terrace 410 can omit, and directly described image acquiring device 430 is connected on described second housing 413.
Described control piece 43 is arranged on the side on described second housing 413 towards described host cavity 42.Described control piece 43 is electrically connected with described The Cloud Terrace camera 400, and is used for controlling described The Cloud Terrace camera 400 and moves, to be adjusted by described image acquiring device 430 to the required angle of shooting.In the present embodiment, described control piece 43 is control circuit plate, and its quantity is two.Two described control pieces 43 are respectively the first control piece 431 and the second control piece 433, and described first control piece 431 is stacked and placed on described second housing 413 regularly, is arranged on described first control piece 431 to described second control piece 433 stacking.
Being appreciated that in other implementations, described control piece 43 can be one, three, four or multiple.Described control piece 43 is installed directly on described second housing 413 of described lower casing 41, and the installing rack of described control piece 43 it is exclusively used in without extra setting, make described fuselage 100 internal structure simplify, remaining space relatively large, and make the overall weight of described fuselage 100 the lightest.
Described radiating piece 45 is arranged on the side of described control piece 43, and is fixed on described second housing 413.In the present embodiment, described radiating piece 45 is radiator fan, and it is for promoting the air circulation of the casing internal of described unmanned vehicle 1, to prevent described unmanned vehicle 1 the most overheated.
Described undercarriage 60 is arranged on described first housing 411, and is positioned at described first housing 411 and deviates from the side of described host cavity 42.In the present embodiment, the quantity of described undercarriage 60 is two, and two described undercarriages 60 are arranged at each interval.The most in the illustrated embodiment, described undercarriage 60 is fixed landing gear.Being appreciated that in other implementations, described undercarriage 60 can also be retractable landing gear, it is not limited to present embodiment.
Described upper shell component 20 is arranged on described first housing 411, and is positioned at described first housing 411 and deviates from the side of described undercarriage 60.Described upper shell component 20 includes upper casing 21, installing rack 23, power supply device 25, functional module 27 and controller 28.The most in the illustrated embodiment, described installing rack 23 is arranged between described upper casing 21 and described first housing 411, and described power supply device 25, described functional module 27 and described controller 28 are both connected in described installing rack 23.
Described upper casing 21 is substantially in housing shape, and it is covered on described lower casing 41, and for matching to house the parts of described unmanned vehicle 1 with described lower casing 41.
Described installing rack 23 is arranged between described upper casing 21 and described lower casing 41, and is connected with described upper casing 21, and described installing rack 23 and the described corresponding setting of control piece 43.Described installing rack 23 is used for installing described power supply device 25 and described functional module 27.In the present embodiment, described installing rack 23 is polyhedron installing rack.Specifically, described installing rack 23 is the frame shaped of rectangle, and it is engraved structure.
Being provided with multiple installation portion on described installing rack 23, multiple described installation portions include but not limited to the first installation portion the 231, second installation portion the 233, the 3rd installation portion 235 and the 4th installation portion 237.The most in the illustrated embodiment, described first installation portion 231 is intervally installed with described second installation portion 233, and is substantially parallel to each other.Described 3rd installation portion 235 is arranged on described first installation portion 231 and described second installation portion 233 near the side of described lower casing 41, and relative two sides of described 3rd installation portion 235 are connected with described first installation portion 231 and described second installation portion 233 respectively.Described 4th installation portion 237 is arranged on described 3rd installation portion 235 near the side of described upper casing 21, and three sides of described 4th installation portion 237 are connected with described first installation portion 231, described second installation portion 233 and described 3rd installation portion 235 respectively.The setting that connects of described first installation portion 231, described second installation portion 233, described 3rd installation portion 235 and described 4th installation portion 237 makes the described installing rack 23 structure in drawer shape, and four described installation portions are collectively forming a receiving space (figure does not marks), described receiving space is used for housing described power supply device 25.
In the present embodiment, described power supply device 25 is battery component.Described power supply device 25 is arranged in the described receiving space of described installing rack 23.
Described functional module 27 is multiple, and multiple described functional modules 27 are arranged on the periphery of described installing rack 23 separated from one anotherly.Multiple described functional modules 27 are electrically connected with described power supply device 25 respectively, and are electrically connected with each other between multiple described functional module 27.The most in the present embodiment, described functional module 27 is circuit board, and its quantity is three, and three described functional modules 27 are respectively as follows: first circuit board 271, second circuit board 273 and tertiary circuit plate 275.First circuit board 271, described second circuit board 273 and described tertiary circuit plate 275 are respectively installed on described first installation portion 231, described second installation portion 233 and described 3rd installation portion 235.Concrete the most in the illustrated embodiment, on the outer surface of the opposite sides being arranged on described installing rack 23 to described first circuit board 271 and described second circuit board 273 stacking respectively.Described tertiary circuit plate 275 is arranged on described installing rack 23, and is spaced with described first circuit board 271 and described second circuit board 273 respectively.The relative side of described tertiary circuit plate 275 is respectively adjacent to described first circuit board 271 and described second circuit board 273.
Further, multiple described functional modules 27 are respectively the circuit board for performing difference in functionality.Being appreciated that in other implementations, described functional module 27 can be two, three, five, seven or more；And described functional module 27 can also be following any two or the combination of two or more functional module: speed sensing module, gravity sensing module, vision sensing module, sensing magnetic fields module, control module.
Described controller 28 is arranged on described tertiary circuit plate 275 and deviates from the side of described installing rack 23, and fixing with described installing rack 23 is connected.The most in the illustrated embodiment, the length of described controller 28 is more than the length of described tertiary circuit plate 275.The opposite ends of the two ends the most described tertiary circuit plate 275 of described controller 28 is extended, and is electrically connected with described power supply device 25 respectively.In the present embodiment, described controller 28 is flight controller, and it is used for controlling described unmanned vehicle 1 and performs aerial mission.
Described upper shell component 20 includes that adaptor 29, described adaptor 29 are arranged at one end of described installing rack 23 further.Described adaptor 29 is for being electrically connected with described power supply device 25.Specifically, described adaptor 29 is stacked on described 4th installation portion 237, and is positioned at the outside of described installing rack 23.Being provided with interface 291 on described adaptor 29, described interface 291 is for being electrically connected with described power supply device 25.In the present embodiment, described interface 291 is standard data interface, and it is used for transmitting electric power and/or transmission data.Relative two sides on described adaptor 29 are respectively adjacent to described first circuit board 271 and described second circuit board 273.
Described power set 300 are arranged on described fuselage 100.In the present embodiment, described power set 300 are rotor assemblies.The most in the illustrated embodiment, described unmanned vehicle 1 is quadrotor, i.e. has the aircraft of four rotor assemblies.Described power set 300 include motor 310 and the propeller (not shown) being connected with described motor 310.The most in the illustrated embodiment, the propeller of described power set 300 does not shows that, it is not intended that described power set 300 can save described propeller.Described motor 310 can drive described propeller rotational, thinks that described unmanned vehicle 1 provides the power of flight.Being appreciated that described unmanned vehicle 1 can also be for six rotorcraft, eight-rotary wing aircraft, 12 rotor crafts etc., even, described unmanned vehicle 1 can be single rotor craft；It addition, in other embodiments, described unmanned vehicle 1 can be Fixed Wing AirVehicle, or the aircraft of fixed-wing-rotor mixing.
Described installing rack 23, described power supply device 25 and the described functional module 27 that this utility model embodiment provides, collectively forms the power supply module of described unmanned vehicle 1.In described power supply module, described installing rack 23 is polyhedron installing rack, multiple described functional modules 27 are arranged on the not ipsilateral of described installing rack 23 separated from one anotherly, enable that the installation and debugging of multiple described functional module 27 are separated from one another to be carried out, being conducive to debugging and the maintenance of described power supply module, the dismounting also making described power supply module is more convenient.Simultaneously, the set-up mode of the functional module 27 of above-mentioned separate type, the Appropriate application intracavity space of described fuselage 100, while making the structure of described power supply module the compactest, inner chamber for described fuselage 100 has reserved more remaining space, flowing for air provides effective passage, the heat radiation of the most described unmanned vehicle 1.
Additionally, described power supply module forms described upper shell component 20 in being detachably mounted on described upper casing 21, described control piece 43 and described radiating piece 45 are installed on described lower casing 41 and form described lower shell component 40, the structure making described unmanned vehicle 1 is the compactest, it is simple to the modularization assembling of described unmanned vehicle 1 and dismounting debugging.
In sum, described controller, described power supply device and multiple described functional module are separately designed and are installed on described installing rack for separate module by described unmanned vehicle 1, the layout making described power supply module is more rationalized, reduce described unmanned vehicle 1 overall volume, make the assembling of power supply module in described unmanned vehicle 1, dismantle or keep in repair more convenient.
Being appreciated that the structure of described installing rack 23 is not limited to rectangular frame structure as described above, it can also be other polyhedral structure.Such as, described installing rack 23 can be tetrahedron mounting structure, hexahedron mounting structure, octahedra mounting structure etc., and by separated from one another for multiple described functional modules 27 the not ipsilateral being arranged on described installing rack 23.
It is appreciated that, described unmanned vehicle 1 can apply to take photo by plane beyond other field, such as ground mapping, the condition of a disaster are patrolled, are sprayed insecticide, correspondingly, load on described unmanned vehicle 1 can be other loads in addition to above-mentioned The Cloud Terrace camera 400, such as detector, spray appliance etc..
It is appreciated that described remote-controlled movement device can be the mobile device in addition to unmanned vehicle.Such as, described remote-controlled movement device can be automatic driving vehicle, and now, controller 28 is travel controller, and power supply device 25 can be battery component or fuel assembly etc., and power set 300 are vehicle wheel component.Or, described remote-controlled movement device can be unmanned boats and ships, unmanned submarine etc..
Embodiment of above is only in order to illustrate the technical solution of the utility model and unrestricted, although this utility model being described in detail with reference to embodiment of above, it will be understood by those within the art that, the technical solution of the utility model can be modified or equivalent the most should not depart from the spirit and scope of technical solutions of the utility model.
Claims (31)
1. a power supply module, it is characterised in that: including installing rack, power supply device and at least two functional module, described installing rack is used for being arranged on a fuselage, and described power supply device is arranged on described installing rack；Described installing rack includes at least two installation portion；Described at least two functional module is respectively arranged on described at least two installation portion, and is electrically connected with described power supply device respectively.
2. power supply module as claimed in claim 1, it is characterised in that: described installing rack is polyhedral structure, and described at least two installation portion lays respectively at the not ipsilateral of described installing rack；
And/or, described power supply module also includes the controller being connected on described installing rack, and described controller is flight controller or travel controller.
3. power supply module as claimed in claim 1, it is characterised in that: described at least two functional module is respectively the circuit board for performing difference in functionality.
4. power supply module as claimed in claim 3, it is characterised in that: described at least two functional module be following several at least one: speed sensing module, gravity sensing module, vision sensing module, sensing magnetic fields module, control module.
5. power supply module as claimed in claim 3, it is characterised in that: described at least two functional module includes that first circuit board and second circuit board, described first circuit board and described second circuit board are separately positioned on the opposite sides of described installing rack.
6. power supply module as claimed in claim 5, it is characterised in that: described power supply device is arranged in described installing rack, on the outer surface of the opposite sides that described first circuit board and described second circuit board are stacked in described installing rack respectively.
7. power supply module as claimed in claim 6, it is characterised in that: described power supply module also includes that adaptor, described adaptor are arranged on one end of described installing rack, and is electrically connected with described power supply device.
8. power supply module as claimed in claim 7, it is characterised in that: described adaptor is stacked on the outer surface of described installing rack, and relative two sides of described adaptor are respectively adjacent to described first circuit board and described second circuit board；
And/or, described adaptor is provided with standard interface, described standard interface is for being electrically connected with described power supply device.
9. power supply module as claimed in claim 7, it is characterized in that: described at least two functional module also includes tertiary circuit plate, described tertiary circuit plate is arranged on described installing rack and is spaced with described second circuit board and described first circuit board respectively, and described tertiary circuit plate is electrically connected with described power supply device.
10. power supply module as claimed in claim 9, it is characterized in that: described tertiary circuit plate is stacked on the outer surface of described installing rack, and three sides of described tertiary circuit plate are respectively adjacent to described first circuit board, described second circuit board and described adaptor.
11. power supply modules as claimed in claim 10, it is characterised in that: described power supply module also includes that controller, described controller are arranged at the side deviating from described installing rack of described tertiary circuit plate, and described controller is electrically connected with described power supply device.
12. power supply modules as claimed in claim 11, it is characterised in that: the opposite ends of the two ends the most described tertiary circuit plate of described controller is extended, and is electrically connected with described power supply device respectively；
And/or, described controller is flight controller or travel controller.
13. 1 kinds of unmanned vehicles, including fuselage, it is characterised in that: described unmanned vehicle also includes the power supply module according to any one of claim 1～12, and described power supply module is arranged on described fuselage.
14. unmanned vehicles as claimed in claim 13, it is characterised in that: described fuselage is casing, and described power supply module is housed in described casing；
And/or, described unmanned vehicle also includes the motor being arranged on described fuselage and is arranged at the propeller on described motor.
15. unmanned vehicles as claimed in claim 13, it is characterised in that: described fuselage includes upper casing and the lower casing mutually fastened, and described power supply module is arranged between described upper casing and described lower casing.
16. unmanned vehicles as claimed in claim 15, it is characterised in that: described power supply module is fixedly installed on described upper casing, to form upper shell component with described upper casing.
17. unmanned vehicles as claimed in claim 16, it is characterised in that: described unmanned vehicle also includes that at least one control piece, at least one control piece described are fixed on described lower casing, and corresponding to described installing rack.
18. unmanned vehicles as claimed in claim 17, it is characterised in that: at least one control piece described includes the first control piece being stacked and placed on regularly on described lower casing, and described first control piece is circuit board.
19. unmanned vehicles as claimed in claim 18, it is characterised in that: at least one control piece described also includes that the second control piece, described second control piece are stacked and placed on described first control piece, and described second control piece is circuit board.
20. unmanned vehicles as claimed in claim 17, it is characterised in that: at least one control piece described is electrically connected with the load being mounted on described unmanned vehicle, and is used for controlling described loaded work piece.
21. unmanned vehicles as claimed in claim 17, it is characterised in that: described unmanned vehicle also includes that radiating piece, described radiating piece are arranged on described lower casing adjacent to described control piece.
22. unmanned vehicles as claimed in claim 21, it is characterised in that: at least one control piece described, described radiating piece are fixed on described lower casing respectively, to form lower shell component with described lower casing；
And/or, described radiating piece is radiator fan.
23. unmanned vehicles as claimed in claim 21, it is characterised in that: described lower casing includes that the first housing and the second housing, described first housing are interlocked with described upper casing and is connected, and described second housing is detachably mounted on described first housing.
24. unmanned vehicles as claimed in claim 23, it is characterised in that: at least one control piece described, described radiating piece are fixed on described second housing respectively, in order at least one control piece described and the integrated assembling of described radiating piece.
25. unmanned vehicles as claimed in claim 23, it is characterised in that: being provided with installing port on described first housing, described installing port runs through described first housing the inner space with described fuselage, and described second case lid is located on described installing port.
26. unmanned vehicles as claimed in claim 15, it is characterised in that: described lower casing includes that the first housing and the second housing, described first housing are interlocked with described upper casing, and described second housing is detachably mounted on described first housing.
27. unmanned vehicles as claimed in claim 26, it is characterised in that: being provided with installing port on described first housing, described installing port runs through described first housing the inner space with described fuselage, and described second case lid is located on described installing port；
And/or, described unmanned vehicle also includes that undercarriage, described undercarriage are arranged on described first housing of described fuselage, and extends towards the direction away from described fuselage.
28. unmanned vehicles as claimed in claim 26, it is characterised in that: being provided with image acquiring device on described unmanned vehicle, described image acquiring device is connected on described second housing of described fuselage.
29. unmanned vehicles as claimed in claim 28, it is characterised in that: described unmanned vehicle also includes The Cloud Terrace, and described The Cloud Terrace can adjustably be arranged on described second housing, and described image acquiring device is arranged on described The Cloud Terrace.
30. 1 kinds of remote-controlled movement devices, including fuselage, it is characterised in that: described remote-controlled movement device also includes the power supply module according to any one of claim 1～12, and described power supply module is arranged on described fuselage.
31. remote-controlled movement devices as claimed in claim 30, it is characterised in that: described remote-controlled movement device is automatic driving vehicle or unmanned boats and ships.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620151510.3U CN205469856U (en) | 2016-02-29 | 2016-02-29 | Power supply module , Unmanned vehicles and remote control mobile device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620151510.3U CN205469856U (en) | 2016-02-29 | 2016-02-29 | Power supply module , Unmanned vehicles and remote control mobile device |
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| CN106275409A (en) * | 2016-11-16 | 2017-01-04 | 腾讯科技（深圳）有限公司 | A kind of unmanned plane |
| WO2017147764A1 (en) * | 2016-02-29 | 2017-09-08 | 深圳市大疆创新科技有限公司 | Power supply component, unmanned aerial vehicle and remotely controlled moving device |
| WO2018076535A1 (en) * | 2016-10-25 | 2018-05-03 | 深圳市大疆创新科技有限公司 | Unmanned aerial vehicle, battery compartment assembly, and battery compartment |
| WO2018086227A1 (en) * | 2016-11-09 | 2018-05-17 | 深圳市大疆创新科技有限公司 | Unmanned aerial vehicle |
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| WO2017147764A1 (en) * | 2016-02-29 | 2017-09-08 | 深圳市大疆创新科技有限公司 | Power supply component, unmanned aerial vehicle and remotely controlled moving device |
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| WO2018076535A1 (en) * | 2016-10-25 | 2018-05-03 | 深圳市大疆创新科技有限公司 | Unmanned aerial vehicle, battery compartment assembly, and battery compartment |
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| CN106275409A (en) * | 2016-11-16 | 2017-01-04 | 腾讯科技（深圳）有限公司 | A kind of unmanned plane |
| CN113942646A (en) * | 2017-06-27 | 2022-01-18 | 深圳市大疆创新科技有限公司 | Unmanned plane |
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| CN108248882A (en) * | 2018-01-19 | 2018-07-06 | 东莞市蓝姆光学科技有限公司 | A kind of unmanned plane optical mirror slip |
| WO2020133834A1 (en) * | 2018-12-25 | 2020-07-02 | 拓攻（南京）机器人有限公司 | Frame for unmanned aerial vehicle, and unmanned aerial vehicle |
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