CN211642605U - Combined quick-release expandable module circuit - Google Patents
Combined quick-release expandable module circuit Download PDFInfo
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- CN211642605U CN211642605U CN201922488993.2U CN201922488993U CN211642605U CN 211642605 U CN211642605 U CN 211642605U CN 201922488993 U CN201922488993 U CN 201922488993U CN 211642605 U CN211642605 U CN 211642605U
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- aerial vehicle
- unmanned aerial
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Abstract
The utility model discloses a but combination quick detach extends modular circuit, including setting up in the multi-functional platform circuit of unmanned aerial vehicle fuselage, set up in the unmanned aerial vehicle aircraft nose circuit of unmanned aerial vehicle aircraft nose, set up in the unmanned aerial vehicle tail circuit of unmanned aerial vehicle tail, set up in the unmanned aerial vehicle left wing circuit of unmanned aerial vehicle left wing and set up in the unmanned aerial vehicle right wing circuit of unmanned aerial vehicle right wing; the unmanned aerial vehicle right wing circuit is respectively in circuit connection with the unmanned aerial vehicle head circuit and the unmanned aerial vehicle tail circuit through plug structures; the unmanned aerial vehicle head circuit and the unmanned aerial vehicle tail circuit are in circuit connection through a plug structure; the unmanned aerial vehicle aircraft nose circuit and the multifunctional platform circuit realize circuit connection through the plug structure. The utility model discloses redesign a circuit to adopt plug structure to connect, can realize the modularization with whole unmanned aerial vehicle's circuit, realize the intercommunication of each circuit through the plug, the function of being convenient for is extended, easily maintenance.
Description
Technical Field
The utility model relates to an unmanned aerial vehicle circuit board technical field, in particular to modular circuit can be extended to combination quick detach.
Background
Most trade unmanned aerial vehicle is the kludge in the existing market to the integral type design is leading, is formed by each spare part equipment, and rather than corresponding circuit connection mode mainly for the lug weld, lead to trade unmanned aerial vehicle function singleness, be not convenient for function expansion, the difficult problem of maintenance.
SUMMERY OF THE UTILITY MODEL
In view of the current unmanned aerial vehicle circuit is direct welding formula circuit, causes the problem that leads to trade unmanned aerial vehicle function singleness, be not convenient for function expansion, maintenance difficulty etc.. The utility model provides a modular circuit can be extended to combination quick detach, redesign to adopt plug structure to connect, can realize the modularization with whole unmanned aerial vehicle's circuit, realize the intercommunication of each circuit through the plug, the function of being convenient for is extended, easily maintains.
The technical scheme of the utility model as follows: a modular circuit is expanded in combination quick detach includes: the system comprises a multifunctional platform circuit arranged on an unmanned aerial vehicle body, an unmanned aerial vehicle head circuit arranged on the unmanned aerial vehicle head, an unmanned aerial vehicle tail circuit arranged on an unmanned aerial vehicle tail, an unmanned aerial vehicle left wing circuit arranged on an unmanned aerial vehicle left wing and an unmanned aerial vehicle right wing circuit arranged on an unmanned aerial vehicle right wing; the unmanned aerial vehicle left wing circuit is respectively in circuit connection with the unmanned aerial vehicle head circuit, the multifunctional platform circuit and the unmanned aerial vehicle tail circuit through plug structures; the unmanned aerial vehicle right wing circuit is respectively in circuit connection with the unmanned aerial vehicle head circuit and the unmanned aerial vehicle tail circuit through plug structures; the unmanned aerial vehicle head circuit and the unmanned aerial vehicle tail circuit are in circuit connection through a plug structure; the unmanned aerial vehicle aircraft nose circuit and the multifunctional platform circuit realize circuit connection through the plug structure.
Further, as preferred, unmanned aerial vehicle tail circuit includes the battery as the power, and this battery is connected with power female plug board, is provided with power male plug board with this power female plug cooperation, power male plug board passes through plug structure and is connected to unmanned aerial vehicle right wing circuit, unmanned aerial vehicle left wing circuit and step-down module, step-down module is connected to the LED control panel, be connected with the LED banks base plate on the LED control panel.
Further, as preferred, the unmanned aerial vehicle right wing circuit includes the right wing divides the electric plate, and this right wing divides the electric plate to be connected to unmanned aerial vehicle tail circuit and unmanned aerial vehicle head circuit.
Further, as preferred, the right wing divides the electroplax to be connected with first electricity through plug structure and transfers, just first electricity is transferred and is provided with right wing function motor, first electricity is transferred and is connected to through plug structure unmanned aerial vehicle aircraft nose circuit, unmanned aerial vehicle aircraft nose circuit directly also is connected with right wing shower nozzle motor through plug structure.
Further, as preferred, the unmanned aerial vehicle left wing circuit includes the left wing distributor plate, and this left wing distributor plate is connected to unmanned aerial vehicle tail circuit and unmanned aerial vehicle head circuit.
Further, as preferred, the left wing electricity divides the board to be connected with the second electricity through plug structure and transfers, just it is provided with left wing function motor to transfer to the second electricity, the second electricity is transferred and is connected to through plug structure unmanned aerial vehicle aircraft nose circuit, unmanned aerial vehicle aircraft nose circuit directly also is connected with left wing shower nozzle motor through plug structure.
Further, as preferred, be provided with the multi-functional platform circuit connecting plate that pairs each other on multi-functional platform circuit and the unmanned aerial vehicle aircraft nose circuit, and set up on the multi-functional platform circuit connecting plate is connected with the third electricity and transfers, the third electricity is transferred and is connected with fuselage function motor.
Further, as preferred, the third electricity is transferred and is four with fuselage function motor, just fuselage function motor with the third electricity is transferred the one-to-one and is connected, four fuselage function motor is used for the seeding respectively, sprays the blanking, water pump and powder sprays.
Further, as preferred, be connected with the flowmeter on the unmanned aerial vehicle aircraft nose circuit.
Has the advantages that: the utility model discloses think about novelty, reasonable in design, and convenient to use, the utility model discloses redesign a circuit to adopt the plug structure to connect, can realize the modularization with whole unmanned aerial vehicle's circuit, realize the intercommunication of each circuit through the plug, the function of being convenient for extends, easily maintains.
Drawings
Fig. 1 is a block diagram of the overall structure of an embodiment of the present invention.
Fig. 2 is the circuit diagram of the tail of the unmanned aerial vehicle in an embodiment of the present invention.
Fig. 3 is a circuit diagram of the right wing of the unmanned aerial vehicle in an embodiment of the present invention.
Fig. 4 is a circuit diagram of the left wing of the drone in an embodiment of the present invention.
Fig. 5 is a circuit diagram of a multi-function platform according to an embodiment of the present invention.
Fig. 6 is the circuit diagram of the unmanned aerial vehicle head in an embodiment of the present invention.
Detailed Description
The invention will be further explained with reference to the following figures and examples:
referring to fig. 1, a combined fast-dismounting expandable module circuit includes: the system comprises a multifunctional platform circuit IV arranged on an unmanned aerial vehicle body, an unmanned aerial vehicle head circuit V arranged on the unmanned aerial vehicle head, an unmanned aerial vehicle tail circuit I arranged on an unmanned aerial vehicle tail, an unmanned aerial vehicle left wing circuit III arranged on an unmanned aerial vehicle left wing and an unmanned aerial vehicle right wing circuit II arranged on an unmanned aerial vehicle right wing; the unmanned aerial vehicle left wing circuit III is respectively in circuit connection with the unmanned aerial vehicle head circuit V, the multifunctional platform circuit IV and the unmanned aerial vehicle tail circuit I through plug structures; the unmanned aerial vehicle right wing circuit II is respectively in circuit connection with the unmanned aerial vehicle head circuit V and the unmanned aerial vehicle tail circuit I through plug structures; the unmanned aerial vehicle head circuit V and the unmanned aerial vehicle tail circuit I are in circuit connection through a plug structure; unmanned aerial vehicle aircraft nose circuit V and multifunctional platform circuit IV pass through plug structure and realize circuit connection.
In a specific implementation process, as a preferred implementation manner, please refer to fig. 2, the tail circuit I of the unmanned aerial vehicle includes a battery as a power supply, the battery is connected with a power female plug board, a power male plug board is arranged in cooperation with the power female plug, the power male plug board is connected to the right wing circuit II of the unmanned aerial vehicle, the left wing circuit III of the unmanned aerial vehicle and the voltage reduction module through a plug structure, the voltage reduction module is connected to an LED control board, and the LED control board is connected with an LED lamp set substrate. Specifically, referring to fig. 2, the 14S battery 1 supplies power to the whole unmanned aerial vehicle, and is connected to the power supply female plug board 2 through the power supply female plug 4. The power male plug strip 3 is connected with an XT150U-F plug 6, an XT150U-F plug 8 and an XT30U-F plug 10 through a power male plug 5. XT150U-M plug 7 is in circuit connection with the right wing of the drone. XT150U-M plug 9 is in circuit connection with the drone's left wing. The XT30U-M plug 11 is connected with a 20-60V-to-6V/10A voltage reduction module 12, the 20-60V-to-6V/10A voltage reduction module 12 is connected with an LED control board 13, the LED control board 13 is respectively connected with 6 LED lamp group aluminum substrates 14, 14 LED lamp group aluminum substrates 15, 6 LED lamp group aluminum substrates 16 and 14 LED lamp group aluminum substrates 17, the 20-60V-to-6V/10A voltage reduction module 12 is used for supplying power to the LED control board 13, 6 LED lamp group aluminum substrates 14, 14 LED lamp group aluminum substrates 15, 6 LED lamp group aluminum substrates 16 and 14 LED lamp group aluminum substrates 17, and the LED control board 13 controls the 6 LED lamp group aluminum substrates 14, 14 LED lamp group aluminum substrates 15, 6 LED lamp group aluminum substrates 16 and 14 LED lamp group aluminum substrates 17. The LED tail signal lamp 18 is connected with the unmanned aerial vehicle head circuit 5.
In a specific implementation process, referring to fig. 3, as a preferred implementation manner, the right wing circuit 2 of the drone includes a right wing distribution board, and the right wing distribution board is connected to the drone tail circuit 1 and the drone head circuit 5. In a specific implementation process, please refer to fig. 3 as a preferred implementation manner, the right-wing distributor plate is connected with a first electric controller through a plug structure, the first electric controller is provided with a right-wing function motor, the first electric controller is connected to the unmanned aerial vehicle head circuit 5 through the plug structure, and the unmanned aerial vehicle head circuit 5 is directly connected with a right-wing nozzle motor through the plug structure. Specifically, referring to fig. 3, the right-wing distributor plate 19 is connected to the tail circuit 1 and the head circuit 5 of the unmanned aerial vehicle, and is simultaneously connected to the XT60U-F plug 21, the XT60U-F plug 23, and the XT60U-F plug 25, the XT60U-M plug 20 is connected to the electronic controller 26, the XT60U-M plug 22 is connected to the electronic controller 27, and the XT60U-M plug 24 is connected to the electronic controller 28. The electric regulator 26 is respectively connected with the LED-M129, the permanent magnet brushless direct current motor 32 and the BD3-M connector 35, and is connected with the unmanned aerial vehicle head circuit 5 through the BD3-F connector 36. The electric regulator 27 is respectively connected with the LED-M630, the permanent magnet brushless direct current motor 33 and the BD3-M connector 37, and is connected with the unmanned aerial vehicle head circuit 5 through the BD3-F connector 38. The electric regulator 28 is respectively connected with the LED-M531, the permanent magnet brushless direct current motor 34 and the BD3-M connector 39, and is connected with the unmanned aerial vehicle head circuit 5 through the BD3-F connector 40. The nozzle permanent magnet brushless direct current motor 45 is connected with the MR30U-M connector 41 and is connected with the unmanned aerial vehicle head circuit 5 through the MR30U-F connector 42. The nozzle permanent magnet brushless direct current motor 46 is connected with the MR30U-M connector 43 and is connected with the unmanned aerial vehicle head circuit 5 through the MR30U-F connector 44. The 2.4G antenna 47 is connected with the unmanned aerial vehicle head circuit 5 through an SMA external thread female connector 48.
In the specific implementation process, as a preferred implementation manner, please refer to fig. 4, the drone left wing circuit 3 includes a left wing distributor plate, and the left wing distributor plate is connected to the drone tail circuit 1 and the drone head circuit 5. In a specific implementation process, as a preferred implementation mode, please refer to fig. 4, the left-wing distributor plate is connected with a second electric regulator through a plug structure, the second electric regulator is provided with a left-wing function motor, the second electric regulator is connected to the unmanned aerial vehicle head circuit 5 through the plug structure, and the unmanned aerial vehicle head circuit 5 is directly connected with a left-wing nozzle motor through the plug structure.
In a specific implementation process, please refer to fig. 5 as a preferred implementation manner, the multifunctional platform circuit 4 and the unmanned aerial vehicle handpiece circuit 5 are provided with a multifunctional platform circuit connection board which is paired with each other, and the multifunctional platform circuit connection board arranged on the multifunctional platform circuit 4 is connected with a third electric controller, and the third electric controller is connected with a fuselage function motor. In the specific implementation process, as a preferred implementation mode, please refer to fig. 4, four third electric regulators and four fuselage function motors are provided, the fuselage function motors are connected with the third electric regulators in a one-to-one correspondence manner, and the four fuselage function motors are respectively used for seeding, spraying and blanking, water pumps and powder spraying. Specifically, referring to fig. 5, the drone left wing circuit 3 includes: the left wing distributor board 49 is connected with the tail circuit 1 and the multifunctional platform circuit 4 of the unmanned aerial vehicle, and is simultaneously connected with an XT60U-F plug 51, an XT60U-F plug 53 and an XT60U-F plug 55. XT60U-M plug 50 is connected to an electrical lead 56. XT60U-M plug 52 is connected to an electrical tilt 57. XT60U-M plug 54 is connected to power brick 58. The electric regulator 56 is respectively connected with the LED-M259, the permanent magnet brushless direct current motor 62 and the BD3-M connector 65, and is connected with the unmanned aerial vehicle head circuit 5 through the BD3-F connector 66. The electric regulator 57 is respectively connected with the LED-M160, the permanent magnet brushless direct current motor 63 and the BD3-M connector 67, and is connected with the unmanned aerial vehicle head circuit 5 through the BD3-F connector 68. The electric regulator 58 is connected with the LED-M161, the permanent magnet brushless direct current motor 64 and the BD3-M connector 69 respectively and is connected with the unmanned aerial vehicle head circuit 5 through the BD3-F connector 70. The nozzle permanent magnet brushless direct current motor 75 is connected with the MR30U-M connector 71 and is connected with the unmanned aerial vehicle head circuit 5 through the MR30U-F connector 72. The nozzle permanent magnet brushless direct current motor 76 is connected with the MR30U-M connector 73 and is connected with the unmanned aerial vehicle head circuit 5 through the MR30U-F connector 74. The 5.8G antenna 77 is connected to the drone handpiece circuit 5 through an SMA external screw female connector 79. The 5.8G antenna 78 is connected to the UAV handpiece circuit 5 through an SMA outer screw female connector 80.
In a specific implementation process, as a preferred implementation mode, please refer to fig. 5, a flow meter is connected to the unmanned aerial vehicle head circuit 5. Specifically, referring to fig. 5, a flow meter 81 is connected to the head circuit of the drone. A multifunction platform circuit connection board-M90 is connected to electrical tilt 82, electrical tilt 83, electrical tilt 84, and electrical tilt 85 by a multifunction platform circuit male plug 92. The electronic regulator 82 is connected with a powder-spraying permanent magnet brushless direct current motor 86. The electronic regulator 83 is connected with a permanent magnet brushless DC motor 87 of the water pump. The electronic regulator 84 is connected with a seeding blanking turntable permanent magnet brushless direct current motor 88. The electric regulator 85 is connected with a seeding turntable permanent magnet brushless direct current motor 89. Multifunctional platform circuit connection board-F91 links to each other with unmanned aerial vehicle left wing circuit 3 and unmanned aerial vehicle aircraft nose circuit 5 through multifunctional platform circuit female plug 93.
In addition, in the unmanned aerial vehicle head circuit 5, please refer to fig. 6, the right 180 ° connection board 94 is connected to the unmanned aerial vehicle right wing circuit 2 and the unmanned aerial vehicle tail circuit 1 through the 40-pin connector female plug 96. The right 90-degree connecting plate 95 comprises a 40-pin connector male plug 97, an MR30PW-M plug 98, an MR30PW-M plug 100, an XT30U-F plug 102, an XT30U-F plug 105, an XT30U-F plug 107 and an XT30U-F plug 109, wherein the 40-pin connector male plug 97 is connected with the MR30PW-M plug 98, the MR30PW-M plug 100, the XT30U-F plug 102, the XT30U-F plug 105, the XT30U-F plug 107 and the XT30U-F plug 109, and is simultaneously connected with the flight control 136, so that the flight control 136 can control the permanent magnet brushless direct current motor 32, the permanent magnet brushless direct current motor 33 and the permanent magnet brushless direct current motor 34 in the right wing circuit 2 of the unmanned aerial vehicle. MR30PW-F plug 99 is connected to MR30U-M plug 126, and MR30U-M plug 126 is connected to 4-in-1 electrical tap 124. MR30PW-F plug 101 is connected to MR30U-F plug 125, and MR30U-F plug 125 is connected to 4-in-1 electrical tune 124. The XT30U-M plug 103 is connected with a 30-60V-to-24V/8A output voltage reduction module 133, the 30-60V-to-24V/8A output voltage reduction module 133 is connected with an XT30U-F plug 132 and a 32-pin connector female plug 115, the XT30U-M plug 131 is connected with an XT30U-M plug 130, and the XT30U-M plug 130 is connected with a 4-in-1 electric regulator 124 to supply power for the 4-in-1 electric regulator 124. The 4-in-1 electric regulator 124 is connected with an MR30U-M plug 127, an MR30U-M plug 128 and a BD3-F plug 129, the MR30U-M plug 127 is connected with an MR30U-F plug 117, the MR30U-M plug 128 is connected with an MR30U-F plug 119, the MR30U-M plug 116 and the MR30U-M plug 118 are connected with a 40-pin connector female plug, the BD3-F plug 129 is connected with a BD3-F plug 134, the BD30-M plug 135 is connected with a 3-F Y type plug 161, and the BD3-F Y type plug 161 is connected with a 158 receiver, so that control over the nozzle permanent magnet brushless direct current motor 45, the permanent magnet brushless direct current motor 46 and the nozzle brushless permanent magnet direct current motor 75 and the permanent magnet brushless direct current motor 76 in the right wing circuit 2 of the unmanned aerial vehicle is realized. XT30U-M plug 104 is connected to power management module 105, power management module 105 is connected to BD30-F plug 145, and BD30-F plug 145 is connected to 136 flight control to provide power for 136 flight control. 136 flight controls are connected to 141BD3-F plug, BD3-F plug 142, BD3-F plug 143, BD3-F plug 144, BD4-F plug 146, BD3-F plug 147, BD3-F plug 148, and BD4-F plug 149. The BD3-F plug 141, the BD3-F plug 142, the BD3-F plug 143, the BD3-F plug 144 and the BD3-F plug 147 are connected with the 32-pin connector female plug 115, so that the control of the permanent magnet brushless direct current motor 62, the permanent magnet brushless direct current motor 63 and the permanent magnet brushless direct current motor 64 in the left wing circuit 3 of the unmanned aerial vehicle is realized. The BD4-F plug 146 is connected to a CAN communication module. BD3-F plug 148 is connected to BD3-F plug 159 and BD3-F plug 159 is connected to receiver 158. BD4-F plug 149 is connected to DB4-F plug 160, and DB4-F plug 160 is connected to receiver 158. XT30U-M plug 106 is connected with CAN communication module 151, CAN communication module 151 is connected with BD4-F plug 152, BD4-F plug 154, BD4-F plug 152 is connected with BD4-F plug 153, BD4-F plug 153 is connected with obstacle avoidance radar 157. BD4-F plug 154 was connected to 156BD4-F plug, and BD4-F plug 156 was connected to imitation terrestrial radar 158. The XT30U-M plug 108 is coupled to the receiver 158 to power the receiver 158. Receiver 158 is connected to a BD3-F Y type plug 161, an MMCX pin plug 162, an MMCX pin plug 163, an MMCX pin plug 164, and a BD8-F plug 165. BD3-F Y type plug 161 links to each other with 32 pin connector female plug 115, and MMCX inner needle plug 162 links to each other with SMA outer screw hole plug 111, and SMA inner screw pin plug 110 links to each other with unmanned aerial vehicle right wing circuit 2, receives the signal of 2.4G antenna 47 in the unmanned aerial vehicle right wing circuit 2. MMCX inner needle plug 163 links to each other with SMA outer screw hole plug 121, and SMA inner needle plug 120 links to each other with unmanned aerial vehicle left wing circuit 3 in the SMA, receives the signal of 5.8G antenna 77 in the unmanned aerial vehicle left wing circuit 3. MMCX inner needle plug 164 links to each other with SMA outer screw hole plug 123, and SMA inner needle plug 122 links to each other with unmanned aerial vehicle left wing circuit 3 in the SMA, receives the signal of 5.8G antenna 78 in the unmanned aerial vehicle left wing circuit 3. The DB8-F plug 165 is connected with the camera 167 and receives signals of the camera 167, and the camera 167 is connected with the LEDs 1-C168 and the LEDs 2-C169. The left 90 ° connector board 113 includes a 32 pin connector female plug 115, an MR30U-M plug 116, and an MR30U-M plug 118. The left 180-degree connecting plate 112 is connected with the left wing circuit 3 of the unmanned aerial vehicle and the multifunctional platform circuit 4 through a 32-pin connector male plug 114, so that control over the left wing circuit 3 of the unmanned aerial vehicle is achieved, and control over the permanent magnet brushless direct current motor 86 for powder spraying, the permanent magnet brushless direct current motor 87 for water pump, the permanent magnet brushless direct current motor 88 for seeding blanking turntable and the permanent magnet brushless direct current motor 89 for seeding turntable in the multifunctional platform circuit 4 is achieved.
The foregoing has described in detail preferred embodiments of the present invention. It should be understood that numerous modifications and variations can be devised by those skilled in the art in light of the teachings of the present invention without undue experimentation. Therefore, the technical solutions that can be obtained by a person skilled in the art through logic analysis, reasoning or limited experiments based on the prior art according to the concepts of the present invention should be within the scope of protection defined by the claims.
Claims (9)
1. A modular circuit can be extended in combination quick detach which characterized in that includes: the system comprises a multifunctional platform circuit (IV) arranged on an unmanned aerial vehicle body, an unmanned aerial vehicle head circuit (V) arranged on the unmanned aerial vehicle head, an unmanned aerial vehicle tail circuit (I) arranged on an unmanned aerial vehicle tail, an unmanned aerial vehicle left wing circuit (III) arranged on an unmanned aerial vehicle left wing and an unmanned aerial vehicle right wing circuit (II) arranged on an unmanned aerial vehicle right wing; the unmanned aerial vehicle left wing circuit (III) is respectively in circuit connection with the unmanned aerial vehicle head circuit (V), the multifunctional platform circuit (IV) and the unmanned aerial vehicle tail circuit (I) through plug structures; the unmanned aerial vehicle right wing circuit (II) is respectively in circuit connection with the unmanned aerial vehicle head circuit (V) and the unmanned aerial vehicle tail circuit (I) through plug structures; the unmanned aerial vehicle head circuit (V) is in circuit connection with the unmanned aerial vehicle tail circuit (I) through a plug structure; the unmanned aerial vehicle aircraft nose circuit (V) and multifunctional platform circuit (IV) realize circuit connection through the plug structure.
2. The circuit of claim 1, wherein: unmanned aerial vehicle tail circuit (I) is including the battery as the power, and this battery is connected with power female plug board, is provided with power male plug board with this power female plug cooperation, power male plug board is connected to through pin structure unmanned aerial vehicle right wing circuit (II), unmanned aerial vehicle left wing circuit (III) and step-down module, step-down module is connected to the LED control panel, be connected with the LED banks base plate on the LED control panel.
3. The circuit of claim 2, wherein the circuit comprises: the unmanned aerial vehicle right wing circuit (II) comprises a right wing distribution board, and the right wing distribution board is connected to the unmanned aerial vehicle tail circuit (I) and the unmanned aerial vehicle head circuit (V).
4. The circuit of claim 3, wherein the circuit comprises: the right wing divides the electroplax to be connected with first electricity through plug structure and transfers, just first electricity is transferred and is provided with right wing function motor, first electricity is transferred and is connected to through plug structure unmanned aerial vehicle aircraft nose circuit (V), unmanned aerial vehicle aircraft nose circuit (V) directly also is connected with right wing shower nozzle motor through plug structure.
5. The circuit of claim 4, wherein the circuit comprises: the unmanned aerial vehicle left wing circuit (III) comprises a left wing distribution board, and the left wing distribution board is connected to the unmanned aerial vehicle tail circuit (I) and the unmanned aerial vehicle head circuit (V).
6. The circuit of claim 5, wherein: the left wing electricity distribution board is connected with the second electricity through plug structure and is transferred, just the second electricity is transferred and is provided with left wing function motor, the second electricity is transferred and is connected to through plug structure unmanned aerial vehicle aircraft nose circuit (V), unmanned aerial vehicle aircraft nose circuit (V) directly also is connected with left wing shower nozzle motor through plug structure.
7. The circuit of claim 6, wherein: be provided with the multi-functional platform circuit connecting plate that pairs each other on multi-functional platform circuit (IV) and unmanned aerial vehicle aircraft nose circuit (V), and set up on the multi-functional platform circuit (IV) the multi-functional platform circuit connecting plate is connected with the third electricity and transfers, the third electricity is transferred and is connected with fuselage function motor.
8. The circuit of claim 7, wherein: the third electricity is transferred and is connected with fuselage function motor four, just fuselage function motor with the third electricity is transferred the one-to-one, four fuselage function motor is used for the seeding respectively, sprays the blanking, water pump and powder sprays.
9. The circuit of claim 8, wherein: and the unmanned aerial vehicle head circuit (V) is connected with a flowmeter.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201922488993.2U CN211642605U (en) | 2019-12-31 | 2019-12-31 | Combined quick-release expandable module circuit |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201922488993.2U CN211642605U (en) | 2019-12-31 | 2019-12-31 | Combined quick-release expandable module circuit |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN211642605U true CN211642605U (en) | 2020-10-09 |
Family
ID=72702495
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201922488993.2U Expired - Fee Related CN211642605U (en) | 2019-12-31 | 2019-12-31 | Combined quick-release expandable module circuit |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN211642605U (en) |
-
2019
- 2019-12-31 CN CN201922488993.2U patent/CN211642605U/en not_active Expired - Fee Related
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| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20201009 Termination date: 20211231 |
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| CF01 | Termination of patent right due to non-payment of annual fee |