CN211543920U - Integrated circuit board - Google Patents
Integrated circuit board Download PDFInfo
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- CN211543920U CN211543920U CN201922327962.9U CN201922327962U CN211543920U CN 211543920 U CN211543920 U CN 211543920U CN 201922327962 U CN201922327962 U CN 201922327962U CN 211543920 U CN211543920 U CN 211543920U
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Abstract
The utility model discloses an integrated circuit board, concretely relates to unmanned aerial vehicle technical field, which comprises a circuit board, the fixed first motor interface that is provided with of circuit board top one end, first motor interface one side is provided with second motor interface, the fixed third motor interface that is provided with of circuit board top one side, third motor interface one side is provided with fourth motor interface, the fixed fifth motor interface that is provided with of circuit board top one end, fifth motor interface one side is provided with sixth motor interface, the fixed first power source that is provided with of circuit board one side. The utility model discloses a to the power line, on integrated to a circuit board after the arrangement of planning such as equipment power cord and signal line, various interfaces that correspond are left to the outside again, to originally disordered various walking of line, the very orderly of arrangement improves rotor unmanned aerial vehicle security reliability, simultaneously, can improve the efficiency of production and inspection maintenance.
Description
Technical Field
The utility model relates to an unmanned air vehicle technique field, more specifically say, the utility model relates to an integrated circuit board.
Background
Unmanned aerial vehicle internal circuit, it is the branch line that walks mostly. Inside the VTOL fixed wing unmanned aerial vehicle, the circuit part is walked the line more: the power line, the signal line and the equipment power line are included.
However, the wires with different specifications and functions are mixed together, so that the wires look disordered, the power utilization safety cannot be guaranteed, and the inspection and maintenance are very complicated.
SUMMERY OF THE UTILITY MODEL
In order to overcome the above-mentioned defect of the prior art, the embodiment of the utility model provides an integrated circuit board, the utility model aims to solve the technical problem that: how to integrate lines with different specifications and functions to ensure the safety of power utilization and facilitate inspection and maintenance.
In order to achieve the above object, the utility model provides a following technical scheme: the utility model provides an integrated circuit board, includes the circuit board, the fixed first motor interface that is provided with of circuit board top one end, first motor interface one side is provided with second motor interface, the fixed third motor interface that is provided with in circuit board top one side, third motor interface one side is provided with fourth motor interface, the fixed fifth motor interface that is provided with of circuit board top one end, fifth motor interface one side is provided with sixth motor interface, the fixed first power source that is provided with in circuit board one side, first power source one side is provided with second power source, fifth motor interface one side is provided with flies the accuse interface, sixth motor interface one side is provided with the cloud platform interface, third motor interface one side is provided with the number and passes the interface.
When the device is produced or used, the battery is connected into the circuit box to supply power to the motors and the power supply modules, after the voltage is reduced by the power supply modules, the power supply is supplied to the flight control interface, the holder interface and the data transmission interface equipment, and the corresponding power supply interface is reserved for supplying power to other equipment, such as differential equipment and the like. All requirements related to all power supplies in the airplane are integrated on the circuit board, and the flight control signals are divergently connected to all equipment including motor electricity regulation, a cradle head, data transmission and the like in the circuit board; all signals provided by flight control are led out, and utilization of flight control functional resources is maximized.
In a preferred embodiment, the first power interface is configured as a V power interface and the second power interface is configured as a V power interface.
In a preferred embodiment, a first power module, a second power module, a third power module and a fourth power module are fixedly arranged on one side of the top of the circuit board.
In a preferred embodiment, the first power module is electrically connected to a second power module, a third power module and a fourth power module, the second power module is electrically connected to the first power interface, the third power module is electrically connected to the flight control interface, and the fourth power module is electrically connected to the second power interface.
In a preferred embodiment, the flight control interface is connected to the first motor interface, the second motor interface, the third motor interface, the fourth motor interface, the fifth motor interface, and the sixth motor interface.
In a preferred embodiment, the first power interface is electrically connected with the pan/tilt/zoom interface and the data transmission interface.
In a preferred embodiment, the first power module is electrically connected to the first motor interface, the second motor interface, the third motor interface, and the fourth motor interface.
In a preferred embodiment, the flight control interface is electrically connected to the pan/tilt interface and the data transmission interface.
The utility model discloses a technological effect and advantage:
1. the utility model discloses a to the power line, on integrated to a circuit board after the arrangement of planning such as equipment power cord and signal line, various interfaces that correspond are left to the outside again, to originally disordered various walking of line, the very orderly of arrangement improves rotor unmanned aerial vehicle security reliability, simultaneously, can improve the efficiency of production and inspection maintenance.
Drawings
Fig. 1 is a schematic diagram of the circuit board structure of the present invention.
Fig. 2 is a schematic diagram of the circuit connection of the present invention.
The reference signs are: the system comprises a circuit board 1, a first power module 2, a first motor interface 3, a second motor interface 4, a third motor interface 5, a fourth motor interface 6, a fifth motor interface 7, a sixth motor interface 8, a first power interface 9, a second power interface 10, a flight control interface 11, a cradle head interface 12, a data transmission interface 13, a second power module 14, a third power module 15 and a fourth power module 16.
Detailed Description
The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only some embodiments of the present invention, not all embodiments. Based on the embodiments in the present invention, all other embodiments obtained by a person skilled in the art without creative work belong to the protection scope of the present invention.
The utility model provides an integrated circuit board, which comprises a circuit board 1, wherein one end of the top of the circuit board 1 is fixedly provided with a first motor interface 3, a second motor interface 4 is arranged on one side of the first motor interface 3, a third motor interface 5 is fixedly arranged on one side of the top of the circuit board 1, a fourth motor interface 6 is arranged on one side of the third motor interface 5, a fifth motor interface 7 is fixedly arranged at one end of the top of the circuit board 1, a sixth motor interface 8 is arranged on one side of the fifth motor interface 7, a first power supply interface 9 is fixedly arranged on one side of the circuit board 1, a second power supply interface 10 is arranged on one side of the first power supply interface 9, a flight control interface 11 is arranged on one side of the fifth motor interface 7, and a pan-tilt interface 12 is arranged on one side of the sixth motor interface 8, and a data transmission interface 13 is arranged on one side of the third motor interface 5.
The first power interface 9 is set to a 12V power interface and the second power interface 10 is set to a 5V power interface.
A first power module 2, a second power module 14, a third power module 15 and a fourth power module 16 are fixedly arranged on one side of the top of the circuit board 1.
The first power module 2 is electrically connected with the second power module 14, the third power module 15 and the fourth power module 16, the second power module 14 is electrically connected with the first power interface 9, the third power module 15 is electrically connected with the flight control interface 11, and the fourth power module 16 is electrically connected with the second power interface 10.
The flight control interface 11 is connected with the first motor interface 3, the second motor interface 4, the third motor interface 5, the fourth motor interface 6, the fifth motor interface 7 and the sixth motor interface 8.
The first power interface 9 is electrically connected with the pan/tilt/zoom interface 12 and the data transmission interface 13.
The first power module 2 is electrically connected with the first motor interface 3, the second motor interface 4, the third motor interface 5 and the fourth motor interface 6.
The flight control interface 11 is electrically connected with the pan/tilt head interface 12 and the data transmission interface 13.
As shown in fig. 1-2, the embodiment specifically is: when the device is produced or used, the battery is connected into the circuit box to supply power to the motors and the power modules, after the voltage is reduced by the power modules, the power is supplied to the flight control interface 11, the cradle head interface 12 and the data transmission interface 13, and the corresponding power interfaces are reserved for supplying power to other devices, such as differential devices and the like. All requirements related to all power supplies in the airplane are integrated on the circuit board 1, and flight control signals are divergently connected to all devices in the circuit board 1, wherein the devices comprise a motor electric regulator, a cradle head, a data transmission device and the like; all signals provided by flight control are led out, and utilization of flight control functional resources is maximized.
Can improve unmanned aerial vehicle inner line's regularity, change the chaotic condition of current inner line, after installation circuit board 1, follow-up connection need not the welding, and all tie points are the plug connector, and convenient and fast is difficult for makeing mistakes, when having improved security and reliability, reduces the use of process, reduction wire rod. Meanwhile, the internal circuit is very ordered and looks beautiful and simple, so that production and assembly testers can assemble the airplane more quickly, and the production efficiency is improved; the tester can check the internal circuit more quickly, eliminate the instability of the flight control signal and improve the quality of the control signal.
The utility model discloses the theory of operation:
when the device is produced or used, the battery is connected into the circuit box to supply power to the motors and the power modules, after the voltage is reduced by the power modules, the power is supplied to the flight control interface 11, the cradle head interface 12 and the data transmission interface 13, and the corresponding power interfaces are reserved for supplying power to other devices, such as differential devices and the like. All requirements related to all power supplies in the airplane are integrated on the circuit board 1, and flight control signals are divergently connected to all devices in the circuit board 1, wherein the devices comprise a motor electric regulator, a cradle head, a data transmission device and the like; all signals provided by flight control are led out, and utilization of flight control functional resources is maximized.
Can improve unmanned aerial vehicle inner line's regularity, change the chaotic condition of current inner line, after installation circuit board 1, follow-up connection need not the welding, and all tie points are the plug connector, and convenient and fast is difficult for makeing mistakes, when having improved security and reliability, reduces the use of process, reduction wire rod. Meanwhile, the internal circuit is very ordered and looks beautiful and simple, so that production and assembly testers can assemble the airplane more quickly, and the production efficiency is improved; the tester can check the internal circuit more quickly, eliminate the instability of the flight control signal and improve the quality of the control signal.
The points to be finally explained are: first, in the description of the present application, it should be noted that, unless otherwise specified and limited, the terms "mounted," "connected," and "connected" should be understood broadly, and may be a mechanical connection or an electrical connection, or a communication between two elements, and may be a direct connection, and "upper," "lower," "left," and "right" are only used to indicate a relative positional relationship, and when the absolute position of the object to be described is changed, the relative positional relationship may be changed;
secondly, the method comprises the following steps: in the drawings of the disclosed embodiments of the present invention, only the structures related to the disclosed embodiments are referred to, and other structures can refer to the common design, and under the condition of no conflict, the same embodiment and different embodiments of the present invention can be combined with each other;
and finally: the above description is only for the preferred embodiment of the present invention and should not be taken as limiting the invention, and any modifications, equivalent replacements, improvements, etc. made within the spirit and principle of the present invention should be included in the protection scope of the present invention.
Claims (8)
1. An integrated circuit board comprising a circuit board (1), characterized in that: a first motor interface (3) is fixedly arranged at one end of the top of the circuit board (1), a second motor interface (4) is arranged on one side of the first motor interface (3), a third motor interface (5) is fixedly arranged on one side of the top of the circuit board (1), a fourth motor interface (6) is arranged on one side of the third motor interface (5), a fifth motor interface (7) is fixedly arranged at one end of the top of the circuit board (1), a sixth motor interface (8) is arranged on one side of the fifth motor interface (7), a first power interface (9) is fixedly arranged on one side of the circuit board (1), a second power interface (10) is arranged on one side of the first power interface (9), a flight control interface (11) is arranged on one side of the fifth motor interface (7), and a pan-tilt interface (12) is arranged on one side of the sixth motor interface (8), and a data transmission interface (13) is arranged on one side of the third motor interface (5).
2. An integrated circuit board according to claim 1, wherein: the first power interface (9) is set to be a 12V power interface, and the second power interface (10) is set to be a 5V power interface.
3. An integrated circuit board according to claim 1, wherein: the circuit board is characterized in that a first power supply module (2), a second power supply module (14), a third power supply module (15) and a fourth power supply module (16) are fixedly arranged on one side of the top of the circuit board (1).
4. An integrated circuit board according to claim 3, wherein: the first power module (2) is electrically connected with the second power module (14), the third power module (15) and the fourth power module (16), the second power module (14) is electrically connected with the first power interface (9), the third power module (15) is electrically connected with the flight control interface (11), and the fourth power module (16) is electrically connected with the second power interface (10).
5. An integrated circuit board according to claim 1, wherein: the flight control interface (11) is connected with the first motor interface (3), the second motor interface (4), the third motor interface (5), the fourth motor interface (6), the fifth motor interface (7) and the sixth motor interface (8).
6. An integrated circuit board according to claim 1, wherein: the first power supply interface (9) is electrically connected with the holder interface (12) and the data transmission interface (13).
7. An integrated circuit board according to claim 3, wherein: the first power supply module (2) is electrically connected with the first motor interface (3), the second motor interface (4), the third motor interface (5) and the fourth motor interface (6).
8. An integrated circuit board according to claim 1, wherein: the flight control interface (11) is electrically connected with the holder interface (12) and the data transmission interface (13).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201922327962.9U CN211543920U (en) | 2019-12-23 | 2019-12-23 | Integrated circuit board |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201922327962.9U CN211543920U (en) | 2019-12-23 | 2019-12-23 | Integrated circuit board |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN211543920U true CN211543920U (en) | 2020-09-22 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201922327962.9U Active CN211543920U (en) | 2019-12-23 | 2019-12-23 | Integrated circuit board |
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| Country | Link |
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| CN (1) | CN211543920U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112918692A (en) * | 2021-03-19 | 2021-06-08 | 江苏沃得农业机械股份有限公司 | One-machine-multi-purpose functional module of plant protection unmanned aerial vehicle |
-
2019
- 2019-12-23 CN CN201922327962.9U patent/CN211543920U/en active Active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112918692A (en) * | 2021-03-19 | 2021-06-08 | 江苏沃得农业机械股份有限公司 | One-machine-multi-purpose functional module of plant protection unmanned aerial vehicle |
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| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20230831 Address after: Factory A11, No. 555 Dujuan Road, Kunshan Development Zone, Suzhou City, Jiangsu Province, 215000 Patentee after: Guozhong Shengyao (Kunshan) Aerospace New Materials Technology Research Institute Co.,Ltd. Address before: Room 503, 5th Floor, Building 2, No. 588 Zixing Road, Minhang District, Shanghai, 201100 Patentee before: SHANGHAI SHENGYAO INTELLIGENT SCIENCE & TECHNOLOGY CO.,LTD. |
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| TR01 | Transfer of patent right |