CN216850659U - Many rotor unmanned aerial vehicle internal power deconcentrators - Google Patents
Many rotor unmanned aerial vehicle internal power deconcentrators Download PDFInfo
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- CN216850659U CN216850659U CN202220371578.8U CN202220371578U CN216850659U CN 216850659 U CN216850659 U CN 216850659U CN 202220371578 U CN202220371578 U CN 202220371578U CN 216850659 U CN216850659 U CN 216850659U
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- pcb
- soldering tin
- internal power
- tin layer
- unmanned aerial
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- 238000005476 soldering Methods 0.000 claims description 34
- ATJFFYVFTNAWJD-UHFFFAOYSA-N Tin Chemical compound [Sn] ATJFFYVFTNAWJD-UHFFFAOYSA-N 0.000 claims description 32
- VYPSYNLAJGMNEJ-UHFFFAOYSA-N Silicium dioxide Chemical compound O=[Si]=O VYPSYNLAJGMNEJ-UHFFFAOYSA-N 0.000 claims description 13
- 239000000741 silica gel Substances 0.000 claims description 13
- 229910002027 silica gel Inorganic materials 0.000 claims description 13
- 230000005611 electricity Effects 0.000 abstract description 9
- 238000004519 manufacturing process Methods 0.000 abstract description 6
- 238000009434 installation Methods 0.000 abstract description 3
- 238000003466 welding Methods 0.000 description 8
- 229910000679 solder Inorganic materials 0.000 description 3
- RSWGJHLUYNHPMX-UHFFFAOYSA-N Abietic-Saeure Natural products C12CCC(C(C)C)=CC2=CCC2C1(C)CCCC2(C)C(O)=O RSWGJHLUYNHPMX-UHFFFAOYSA-N 0.000 description 2
- KHPCPRHQVVSZAH-HUOMCSJISA-N Rosin Natural products O(C/C=C/c1ccccc1)[C@H]1[C@H](O)[C@@H](O)[C@@H](O)[C@@H](CO)O1 KHPCPRHQVVSZAH-HUOMCSJISA-N 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 238000009422 external insulation Methods 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- KHPCPRHQVVSZAH-UHFFFAOYSA-N trans-cinnamyl beta-D-glucopyranoside Natural products OC1C(O)C(O)C(CO)OC1OCC=CC1=CC=CC=C1 KHPCPRHQVVSZAH-UHFFFAOYSA-N 0.000 description 2
- XOMKZKJEJBZBJJ-UHFFFAOYSA-N 1,2-dichloro-3-phenylbenzene Chemical compound ClC1=CC=CC(C=2C=CC=CC=2)=C1Cl XOMKZKJEJBZBJJ-UHFFFAOYSA-N 0.000 description 1
- FPWNLURCHDRMHC-UHFFFAOYSA-N 4-chlorobiphenyl Chemical compound C1=CC(Cl)=CC=C1C1=CC=CC=C1 FPWNLURCHDRMHC-UHFFFAOYSA-N 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
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Abstract
The utility model relates to the technical field of unmanned aerial vehicles, in particular to an internal power supply deconcentrator of a multi-rotor unmanned aerial vehicle; the utility model comprises an upper PCB, an insulating pad, a lower PCB, a power cable and an XT series power connector, wherein the upper PCB and the lower PCB are respectively arranged at the upper side and the lower side of the insulating pad, the power cable is respectively connected with the upper PCB and the lower PCB, the upper PCB and the lower PCB are electrically connected, and the anode of the XT series power connector is connected with the upper PCB and the cathode is connected with the lower PCB; the utility model discloses during the wiring, direct with the electric wire of rotor insert XT series power connector can, it is very convenient, the electricity is connected stably moreover, the reliability is high, can effectively reduce the work load of many rotor unmanned aerial vehicle installation and production, improved production efficiency and customer experience.
Description
Technical Field
The utility model relates to an unmanned air vehicle technique field refers in particular to a many rotor unmanned aerial vehicle internal power source deconcentrators.
Background
The existing miniature and small-sized multi-rotor unmanned aerial vehicle has the characteristic of more rotor arms, generally mainly comprises four rotors, six rotors and eight rotors, and because the rotors are more, the number of internal power supply cables is more, so that the unmanned aerial vehicle is not beneficial to wiring and can be subjected to electromagnetic interference. Current many rotor unmanned aerial vehicle mostly is the direct parallelly connected multichannel cable of a set of power cord and supplies power for each rotor arm, and requirement is higher to welding requirement and welding equipment like this, and the condition such as many appear rosin joint false weldings, leads to many rotor unmanned aerial vehicle to lead to the flight attitude unstability at the flight in-process, and the magnetic compass receives the interference scheduling problem, influences the flight safety of aircraft.
Therefore, based on the above-mentioned defect of current many rotor unmanned aerial vehicle, need improve current many rotor unmanned aerial vehicle.
SUMMERY OF THE UTILITY MODEL
The utility model aims to provide a many rotor unmanned aerial vehicle internal power source deconcentrators to the not enough of prior art, this many rotor unmanned aerial vehicle internal power source deconcentrators have solved that current many rotor unmanned aerial vehicle exists: inconvenient wiring, poor reliability and the like.
In order to achieve the purpose, the utility model is realized by the following technical scheme: many rotor unmanned aerial vehicle internal power source deconcentrators, including upper PCB, insulating pad, lower floor's PCB, power cable, XT series power connector, upper PCB, lower floor's PCB set up respectively in the upper and lower both sides of insulating pad, and power cable connects upper PCB, lower floor's PCB respectively, and upper PCB, lower floor's PCB electricity are connected, and lower floor's PCB is connected to XT series power connector's anodal upper PCB, negative pole connection.
Furthermore, the plurality of XT series power connectors are uniformly arranged along the periphery of the insulating pad, so that the wiring is more reasonable.
Furthermore, the insulating pad is circular, and wiring is convenient.
Furthermore, the upper layer of soldering tin layer is arranged above the upper layer of PCB, the positive electrode of the XT series power connector is connected with the upper layer of soldering tin layer, the upper layer of soldering tin layer is electrically connected with the upper layer of PCB, welding is convenient, and the stability of electrical connection is ensured.
Furthermore, the upper soldering tin layer is circular, and welding is convenient.
Further, the below of lower floor's PCB be provided with lower floor's soldering tin layer, lower floor's soldering tin layer is connected to XT series power connector's negative pole, lower floor's soldering tin layer is connected with lower floor's PCB electricity, convenient welding guarantees the stability of electricity connection.
Furthermore, the lower soldering tin layer is circular, and welding is convenient.
Furthermore, the upper PCB and the lower PCB are both circular, and welding is facilitated.
Furthermore, the upper layer of the soldering tin layer is covered with the upper layer of insulating silica gel, so that the safety is ensured.
Furthermore, lower floor's soldering tin layer below cover and have lower floor's insulating silica gel, guarantee the security.
The beneficial effects of the utility model reside in that: during the wiring, direct with the electric wire of rotor insert XT series power connector can, it is very convenient, the electricity is connected stably moreover, the reliability is high, can effectively reduce the work load of many rotor unmanned aerial vehicle installation and production, improved production efficiency and customer experience.
Drawings
Fig. 1 is a schematic perspective view of the present invention.
Fig. 2 is a schematic view of the exploded structure of the present invention.
Fig. 3 is a schematic top view of the present invention.
Fig. 4 is a schematic side view of the present invention.
Reference numbers and descriptions:
the high-voltage power supply comprises an upper insulating silica gel 1, an upper soldering silica gel layer 2, an upper PCB3, an insulating pad 4, a lower PCB5, a lower soldering silica gel layer 6, a lower insulating silica gel 7, a power supply cable 8 and an XT series power supply connector 9.
Detailed Description
The present invention will be further described with reference to the accompanying drawings.
See fig. 1-4, the utility model discloses many rotor unmanned aerial vehicle internal power source deconcentrators includes: the power cable comprises an upper PCB3, an insulating pad 4, a lower PCB5, a power cable 8 and an XT series power connector 9, wherein the upper PCB3 and the lower PCB5 are respectively arranged on the upper side and the lower side of the insulating pad 4 and are insulated by the insulating pad 4. The power cable 8 is respectively connected with the upper layer PCB3 and the lower layer PCB5, the upper layer PCB3 and the lower layer PCB5 are electrically connected, and the positive electrode of the XT series power connector 9 is connected with the upper layer PCB3 and the negative electrode is connected with the lower layer PCB 5.
The utility model discloses a XT series power connector 9 has a plurality ofly, evenly sets up around along insulating pad 4 respectively. The insulating pad 4 is circular.
The utility model discloses an upper PCB 3's top is provided with upper soldering tin layer 2, and upper soldering tin layer 2 is connected to XT series power connector 9's positive pole, and upper soldering tin layer 2 is connected with upper PCB3 electricity. The upper soldering tin layer 2 is circular, so that the XT series power connector 9 is convenient to weld, the condition of insufficient solder and false solder is not easy to cause, and the stability of electric connection is ensured.
The utility model discloses a lower floor's PCB5 below is provided with lower floor's soldering tin layer 6, and lower floor's soldering tin layer 6 is connected to XT series power connector 9's negative pole, and lower floor's soldering tin layer 6 is connected with lower floor's PCB5 electricity. Lower floor's soldering tin layer 6 is circular, makes things convenient for XT series power connector 9 to weld, is difficult to cause the condition of rosin joint, false solder joint, guarantees that the electricity is connected stably.
The utility model discloses an upper PCB3, lower floor PCB5 all are circularly, and the XT series power connector 9 of being convenient for connects.
The utility model discloses a 2 tops on upper soldering tin layer cover have upper insulating silica gel 1, play the external insulation effect.
The utility model discloses a 6 below covers on lower floor's soldering tin layer have lower floor's insulating silica gel 7, play the external insulation effect.
The utility model discloses a XT series power connector 9 can have four, six or eight, and the picture shows six XT series power connector 9, evenly distributed.
The utility model discloses an upper insulating silica gel 1, lower floor's insulating silica gel 7 can adopt the mode of direct lock to assemble together, and it is fixed in proper order with upper soldering tin layer 2, upper PCB3, insulating pad 4, lower floor's PCB5, lower floor's soldering tin layer 6, lower floor's insulating silica gel 7.
The utility model discloses during the wiring, direct with the electric wire of rotor insert XT series power connector 9 can, it is very convenient, the electricity is connected stably moreover, the reliability is high.
The utility model discloses simple structure, safe and reliable can effectively reduce the work load of many rotor unmanned aerial vehicle installation and production, has improved production efficiency and customer experience, provides more convenient mode of connection, has improved the holistic reliability of unmanned aerial vehicle.
Of course, the above-mentioned embodiments are only preferred examples of the present invention, and not intended to limit the scope of the present invention, so that all equivalent changes or modifications made by the structure, features and principles described in the claims of the present invention should be included in the claims of the present invention.
Claims (10)
1. Many rotor unmanned aerial vehicle internal power deconcentrators, its characterized in that: the power cable is respectively connected with the upper PCB and the lower PCB, the upper PCB and the lower PCB are electrically connected, and the positive electrode of the XT series power connector is connected with the upper PCB and the negative electrode of the lower PCB.
2. The internal power splitter for multi-rotor drones of claim 1, wherein: the XT series power supply connectors are arranged uniformly along the periphery of the insulating pad.
3. The internal power splitter for multi-rotor drones of claim 1, wherein: the insulating pad is circular.
4. The internal power splitter of multi-rotor drone of claim 1, 2 or 3, wherein: an upper soldering tin layer is arranged above the upper PCB, the positive electrode of the XT series power supply connector is connected with the upper soldering tin layer, and the upper soldering tin layer is electrically connected with the upper PCB.
5. The internal power splitter of multi-rotor drone of claim 4, wherein: the upper soldering tin layer is circular.
6. The internal power splitter of multi-rotor drone of claim 4, wherein: the lower PCB is provided with a lower soldering tin layer below, the negative pole of the XT series power connector is connected with the lower soldering tin layer, and the lower soldering tin layer is electrically connected with the lower PCB.
7. The internal power splitter for multi-rotor drones of claim 6, wherein: the lower soldering tin layer is circular.
8. The internal power splitter for multi-rotor drones of claim 1, wherein: the upper PCB and the lower PCB are both circular.
9. The internal power splitter of multi-rotor drone of claim 4, wherein: and an upper insulating silica gel layer is covered above the upper soldering tin layer.
10. The internal power splitter for multi-rotor drones of claim 6, wherein: and the lower insulating silica gel layer is covered below the lower soldering tin layer.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202220371578.8U CN216850659U (en) | 2022-02-23 | 2022-02-23 | Many rotor unmanned aerial vehicle internal power deconcentrators |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202220371578.8U CN216850659U (en) | 2022-02-23 | 2022-02-23 | Many rotor unmanned aerial vehicle internal power deconcentrators |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN216850659U true CN216850659U (en) | 2022-06-28 |
Family
ID=82091437
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202220371578.8U Active CN216850659U (en) | 2022-02-23 | 2022-02-23 | Many rotor unmanned aerial vehicle internal power deconcentrators |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN216850659U (en) |
-
2022
- 2022-02-23 CN CN202220371578.8U patent/CN216850659U/en active Active
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| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| TR01 | Transfer of patent right | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20240824 Address after: 341400 Units 129-130, Building H7, China Ganzhou Low altitude Economic Industrial Park, Longhui Town, Nankang District, Ganzhou City, Jiangxi Province Patentee after: Mingde New Materials (Ganzhou) Technology Co.,Ltd. Country or region after: China Address before: 518106 floor 6, building B, yueshengtong science and Technology Park, No. 46, Zhenxing Road, liyuhe Industrial Zone, Loucun community, Gongming street, Guangming New Area, Shenzhen, Guangdong Patentee before: Shenzhen Mingde New Material Technology Co.,Ltd. Country or region before: China |