A high-voltage connector for a drone
By achieving a stable connection between the three-phase female connector and the three-phase line, the problems of large size and high failure rate of UAV connectors are solved, and the miniaturization and high stability of the connector are realized.
Patent Information
- Application Number
- CN202511517883.8
- Authority / Receiving Office
- CN · China
- Patent Type
- Patents(China)
- Current Assignee / Owner
- Filing Date
- 2025-10-23
- Publication Date
- 2026-02-27
- Estimated Expiration
- 2045-10-23
AI Technical Summary
Existing drone connectors suffer from large size and high failure rate due to the scattered distribution of the three-phase wires.
The three-phase female connector is used to connect to the three-phase wires. A stable connection is achieved through plastic springs and bolt assemblies. The three-phase male connector is placed separately from the three-phase wires and is limited by plastic springs and clamps to prevent friction and slippage.
The reduced connector size lowers the drone failure rate and improves connection stability and security.
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Figure CN121011902B_ABST
Abstract
Description
TECHNICAL FIELD
[0001] The present application relates to the field of unmanned aerial vehicles, in particular to a high-voltage connector for unmanned aerial vehicles. BACKGROUND
[0002] In daily life, connectors are also called connectors, and in China they are also called connectors and sockets. Generally, it refers to electrical connectors, which are devices that connect two source devices to transmit current or signals. The male end and the female end can transmit information or current after contact, also known as connectors. Among them, the connector of the unmanned aerial vehicle is the core component to ensure the reliable operation of the unmanned aerial vehicle system, and its performance directly affects the flight safety, task efficiency and equipment life.
[0003] The current unmanned aerial vehicle connector on the market only has a high-voltage module connector, and in most cases uses an independent interface design. The independent interface needs to configure contacts and plug-in male heads for each phase line and ground line, which will result in a large overall size of the connector, increasing the load of the unmanned aerial vehicle and affecting its endurance. In addition, the three-phase lines at the back end of the connector are distributed randomly, and during the flight of the unmanned aerial vehicle, the frequent movement of the three-phase lines may cause mutual friction and wire pulling between the three-phase lines, increasing the overall failure rate of the unmanned aerial vehicle.
[0004] In summary, the above structure will increase the size of the connector due to the placement of the three-phase lines during actual use, and the random distribution of the three-phase lines may cause mutual friction and wire pulling between the three-phase lines, increasing the overall failure rate of the unmanned aerial vehicle. SUMMARY
[0005] Therefore, the purpose of the present application is to provide a high-voltage connector for unmanned aerial vehicles to solve the technical problem that the size of the connector is increased due to the placement of the three-phase lines during actual use, and the random distribution of the three-phase lines may cause mutual friction and wire pulling between the three-phase lines, increasing the overall failure rate of the unmanned aerial vehicle.
[0006] To achieve the above-mentioned purpose, the present application provides the following technical scheme: a high-voltage connector for unmanned aerial vehicles, comprising a plug-in male head, three-phase male pins, three-phase lines and signal lines, both ends of the plug-in male head are provided with plug-in female heads and male head rear covers, one end of the three-phase lines is provided with a three-phase female head, wherein the male head rear cover is provided with a plastic spring piece matched with the three-phase female head, the plug-in male head is provided with a plug hole, and the three-phase male pins and the plug-in female head are slidingly matched;
[0007] A top rod is elastically and penetratively arranged on the three-phase female head, one end of the top rod is connected with a clamping plate in the three-phase female head, a clamping groove is arranged on the outer wall of the three-phase female head at the position of the top rod, a conical ring is arranged on one side of the clamping groove, one end of the signal line penetrates into the plug-in female head, and a pin header is connected in the plug-in female head.
[0008] Through the adoption of the above technical scheme, the plastic elastic sheet is clamped on the outer wall of the three-phase female head under the action of the plastic elastic sheet, the plug male head is threadedly connected with the plug female head through the bolt assembly, so that the three-phase line is not exposed and hung after the plug-in of the three-phase line, the three-phase male pin is inserted into the plug female head and inserted into the three-phase female head, the electrical connection between the three-phase male pin and the three-phase line is realized, and the three-phase line is separately and separately arranged, so that the three-phase line and the three-phase male pin are prevented from being worn by swinging with other structural members after the plug-in of the three-phase line, and the plastic elastic sheet is pressed against the ejector rod, the clamping plate on the inner wall drives the outer wall of the three-phase male pin inserted into the three-phase female head to be limited, and the three-phase male pin is limited at the same time, so that the stability of the connection between the three-phase male pin and the three-phase line is ensured.
[0009] The application is further provided that the plug female head is provided with a flat hole penetrating through, and the outer wall of the three-phase male pin is provided with a horizontal surface matched with the flat hole.
[0010] As preferred, the flat hole is provided to ensure the consistency of the three-phase male pin when the three-phase male pin is inserted into the plug female head, prevent the inclination of the three-phase male pin connection, and avoid the need for adjusting the angle of the three-phase male pin after the subsequent installation is completed.
[0011] The application is further provided that the inner wall of the three-phase female head is provided with an inner groove, and the depth of the inner groove is greater than the thickness of the clamping plate.
[0012] As preferred, the inner groove is provided to facilitate the clamping of the clamping plate into the inner groove by the ejector rod, and the depth of the inner groove can ensure that the clamping plate is completely in the inner groove, so that the clamping plate does not hinder the subsequent sliding connection of the three-phase male pin, and the stability of the overall installation is further improved.
[0013] The application is further provided that one end of the plastic elastic sheet is provided in an inner recessed manner, and a tapered surface is arranged on the inner wall of the plastic elastic sheet, and the connection between the one end of the plastic elastic sheet and the tapered ring is provided in a smooth manner, and the outer diameter of one end of the tapered surface is the same as the inner diameter of the plastic elastic sheet.
[0014] As preferred, the inner recessed manner facilitates the extrusion of the ejector rod during the subsequent elastic reset process, and the tapered surface facilitates the sliding of the plastic elastic sheet to the outer wall of the tapered ring during the sliding of the three-phase female head, so that the plastic elastic sheet can still be limited and fixed, and after the subsequent extrusion of the plastic elastic sheet to the ejector rod is completed, the outer wall of the tapered ring is in full contact with the inner wall of the plastic elastic sheet, further sealing the slot at the ejector rod, effectively preventing the limitation of the sliding part of the ejector rod during the subsequent gluing.
[0015] The application is further provided with a first threaded hole on the male head and the male head rear cover, and a second threaded hole on the outer wall of the male head and the female head.
[0016] As preferred, the male head rear cover is fixed and limited with the male head through the cooperation of the first threaded hole and the bolt assembly, and then the male head and the female head are fixed and limited through the cooperation of the second threaded hole and the bolt assembly, thereby completing the overall fixing and installation work.
[0017] The application is further provided with an opening at one end of the insertion hole, and a smooth surface on the inner wall of the insertion hole.
[0018] As preferred, the opening facilitates the guiding of the three-phase female head, and the smooth surface effectively reduces the sliding friction between the three-phase female head and the insertion hole, ensuring that the male head rear cover can be stably inserted into the male head.
[0019] The application is further provided with a flexible protective sleeve on the inner wall of the clamping plate, and the flexible protective sleeve is detachably arranged on the inner wall of the clamping plate.
[0020] As preferred, the flexible protective sleeve prevents the clamping plate from directly contacting the outer wall of the three-phase male pin, effectively preventing the outer wall of the three-phase male pin from being worn during the clamping process, and the flexible protective sleeve is made of insulating material, preventing electric leakage, and the detachable arrangement facilitates regular maintenance and replacement by the staff.
[0021] The application is further provided with a sealing rubber ring on the outer wall of the male head, and a rubber groove for the sealing rubber ring on the inner wall of the female head.
[0022] As preferred, the sealing rubber ring ensures the sealing between the male head and the female head, effectively reducing the moisture in the air entering the male head during the flight of the unmanned aerial vehicle, and the rubber groove of the female head makes the contact with the sealing rubber ring more closely, further improving the sealing effect of the male head and the female head.
[0023] The application is further provided with an elastic assembly in the interlayer of the three-phase female head, and one end of the elastic assembly is fixedly connected to the three-phase female head, and the other end is connected to the outer wall of the top rod.
[0024] As preferably, in the normal state, the outer wall of the top rod penetrates the three-phase female head, under the action of the plastic elastic sheet, the top rod is pressed to move downward, at this time the elastic assembly is compressed, then when the plastic elastic sheet is removed, the top rod is reset to slide again under the reset action of the elastic assembly.
[0025] The application is further provided that the outer wall of the top rod is arc-shaped at one end of the plastic elastic sheet, and a smooth surface is arranged at the arc-shaped end face.
[0026] As preferably, the arc-shaped arrangement facilitates the subsequent sliding of the plastic elastic sheet to the top of the top rod through the outer wall of the conical ring to achieve the completion of the pressing work, and the smooth surface of the arc-shaped end face effectively reduces the sliding friction between the two, ensuring the stability of the sliding of the plastic elastic sheet at the top rod.
[0027] In summary, the application mainly has the following beneficial effects:
[0028] 1. The three-phase female head is connected with the three-phase line, then inserted into the plug-in male head socket, and clamped on the outer wall of the three-phase female head under the action of the plastic elastic sheet, the plug-in male head is threadedly connected with the plug-in female head through the bolt assembly, so that the three-phase line after the plug-in does not exist exposed and suspended outside, then the three-phase male pin is inserted into the plug-in female head and inserted into the three-phase female head, realizing the electrical connection between the three-phase male pin and the three-phase line, and the three-phase line is separated and placed, which avoids the swing wear with other structural parts after the three-phase line is plugged in, reduces the indirect contact between the three-phase line connection part and other structural parts, and effectively reduces the overall failure rate of the unmanned aerial vehicle.
[0029] 2. The three-phase female head is inserted into the plastic elastic sheet and pushed inward a certain distance, so that the plastic elastic sheet contacts the outer wall of the conical ring, at this time the three-phase male pin penetrates the plug-in female head and the plug-in male head and is inserted into the three-phase female head, then the male head rear cover is inserted into the plug-in male head, and the plastic elastic sheet is reset to the clamping groove through the extrusion of the inner wall of the plug-in male head, at this time the clamping groove limits the three-phase female head, which can prevent the three-phase line from sliding out backward, and the plastic elastic sheet will press the top rod, the clamping plate of the inner wall limits the outer wall of the three-phase male pin inserted into the three-phase female head, and the three-phase male pin is limited, thereby ensuring the stability of the connection between the three-phase male pin and the three-phase line, and preventing the three-phase male pin and the three-phase line from slipping during the flight of the unmanned aerial vehicle.
[0030] 3. The high-voltage connector of the application realizes the socket connection of the phase line and the row pin connection of the signal line, thereby realizing the integration of the high-voltage module and the low-voltage module, making the product smaller, having no wear risk, and being safer. BRIEF DESCRIPTION OF DRAWINGS
[0031] Figure 1 isometric view of the present application;
[0032] Figure 2 exploded view of the present application;
[0033] Figure 3 schematic view of the three-phase male pin structure of the present application;
[0034] Figure 4 schematic view of the plug male structure of the present application;
[0035] Figure 5 schematic view of the three-phase wire installation structure of the present application;
[0036] Figure 6 cross-sectional view of the present application;
[0037] Figure 7 enlarged view of A in the present application Figure 6
[0038] Figure 8 schematic view of the plug male rear cover structure of the present application;
[0039] Figure 9 schematic view of the three-phase male pin and three-phase wire connection state of the present application;
[0040] Figure 10 enlarged view of B in the present application Figure 9
[0041] Figure 11 schematic view of the three-phase female structure of the present application;
[0042] Figure 12 enlarged view of C in the present application Figure 11
[0043] BRIEF DESCRIPTION OF DRAWINGS
[0044] 1, plug male; 2, plug female; 3, plug male rear cover; 4, three-phase wire; 5, three-phase male pin; 6, jack; 7, first threaded hole; 8, second threaded hole; 9, three-phase female; 10, plastic spring; 11, inner groove; 12, top rod; 13, clamping plate; 14, clamping groove; 15, conical ring; 16, signal line; 17, pin array; 18, female array. DETAILED DESCRIPTION
[0045] The technical solutions in the embodiments of the present application will be described clearly and completely below with reference to the drawings in the embodiments of the present application. The embodiments described below with reference to the drawings are exemplary and are only used to explain the present application, and cannot be understood as a limitation of the present application.
[0046] The embodiments are described below according to the overall structure of the present application.
[0047] Embodiment one: please refer to Figures 1-12 The unmanned aerial vehicle high-voltage connector shown in the figure comprises a plug male head 1, a plug female head 2, a male head rear cover 3, a sliding mechanism, a sealing mechanism and a limiting mechanism. A plurality of hole grooves are formed on the male head rear cover 3. The worker places the three-phase line 4 immersed in tin after stripping in the three-phase female head 9, clamps the three-phase line 4 and the three-phase female head 9 by means of a tool, then inserts the three-phase line 4 into the hole grooves formed on the male head rear cover 3 correspondingly, so that the three-phase line 4 is placed separately and is prevented from swinging and wearing with other structural parts. The indirect contact of the three-phase line 4 connection part with other structural parts is reduced, the overall failure rate of the unmanned aerial vehicle is effectively reduced, one end of the signal line 16 penetrates into the plug female head 2, the pin header 17 is connected in the plug female head 2, the signal line 16 is connected with the female header 18, the pin header 17 and the female header 18 at one end of the signal line 16 are inserted, the integration of the low-voltage module is realized, the sealing glue is poured after fixing, and the inner wall of the male head rear cover 3 is provided with the plastic spring 10 at the hole groove. Since the outer diameter of one end of the three-phase female head 9 is greater than that of the other end, the plastic spring 10 is stretched during the inward sliding process.
[0048] The different outer diameters of the three-phase female head 9 at both ends form a clamping groove 14 at the middle position. When the plastic elastic sheet 10 is located at the clamping groove 14, it is reset by the elastic effect of the plastic elastic sheet 10 itself, and is waterproof and fixed to prevent dragging. A tapered ring 15 is arranged on the outer wall of the three-phase female head 9 on the side of the clamping groove 14. When the three-phase female head 9 continues to slide to one side, the plastic elastic sheet 10 is located on the outer wall of the tapered ring 15. Then, the staff inserts the three-phase male pin 5 into the inside of the plug-in female head 2 and the plug-in male head 1 to the inside of the three-phase female head 9, realizing the integration of the high-voltage module. The integration of the low-voltage module and the high-voltage module reduces the overall volume and the load of the unmanned aerial vehicle, and ensures the endurance of the unmanned aerial vehicle. The space in the module is used to glue the wire insertion part, which can effectively protect and greatly improve the waterproof and dustproof ability. When the three-phase male pin 5 at one end contacts and inserts the three-phase wire 4 in the three-phase female head 9, the first threaded hole 7 is arranged on the plug-in male head 1 and the male head rear cover 3, and the second threaded hole 8 is arranged on the outer wall of the plug-in male head 1 and the plug-in female head 2. The first threaded hole 7 and the second threaded hole 8 are matched by the bolt assembly, and the assembly gap is protected by the sealing glue. The plug-in male head 1 and the plug-in female head 2 are fixed by the cooperation of the second threaded hole 8 and the bolt assembly, and the male head rear cover 3 is inserted into the plug-in male head 1. Since the plug-in male head 1 is provided with a plug hole 6 for inserting the three-phase female head 9, when the three-phase female head 9 is completely inserted into the plug hole 6, it continues to slide to one side, which pushes the plastic elastic sheet 10 to reset and move on the outer wall of the tapered ring 15.
[0049] Since the three-phase female head 9 is elastically penetrated by the top rod 12, one end of the top rod 12 is connected with the clamping plate 13 in the three-phase female head 9. During the sliding process of the plastic elastic sheet 10, the top rod 12 is pressed, which drives the clamping plate 13 at the bottom to slide down. Since one end of the three-phase wire 4 is located on one side of the clamping plate 13 in the initial state, and the three-phase male pin 5 contacts the three-phase wire 4 at this time, one end of the three-phase male pin 5 is located at the bottom of the clamping plate 13. Under the action of the top rod 12, the clamping plate 13 limits and clamps the three-phase male pin 5. Then, the male head rear cover 3 and the plug-in male head 1 are fixed by the cooperation of the first threaded hole 7 and the bolt assembly, thereby completing the overall fixing and installation work. The three-phase female head 9 is limited by the clamping groove 14, which can prevent the three-phase wire 4 from sliding back out, thereby ensuring the stability of the connection between the three-phase male pin 5 and the three-phase wire 4, preventing the three-phase male pin 5 and the three-phase wire 4 from slipping off during the flight shaking of the unmanned aerial vehicle, and effectively reducing the overall failure rate of the unmanned aerial vehicle.
[0050] In the above embodiment, please refer to Figure 3 andFigure 6 Wherein the female adapter 2 is provided with a flat hole, and the outer wall of the three-phase male pin 5 is provided with a horizontal surface matched with the flat hole. The flat hole ensures that the three-phase male pin 5 is consistent in inclination when inserted into the female adapter 2, preventing the three-phase male pin 5 from being inclined, and avoiding the need to adjust the angle of the three-phase male pin 5 after installation.
[0051] In the above embodiment, please refer to Figure 7 The inner wall of the three-phase female head 9 is provided with an inner groove 11, and the depth of the inner groove 11 is greater than the thickness of the clamping plate 13. The inner groove 11 facilitates the clamping plate 13 to be clamped into the inner groove 11 by the ejector rod 12, and the depth of the inner groove 11 ensures that the clamping plate 13 is completely in the inner groove 11, preventing the clamping plate 13 from hindering the sliding connection of the three-phase male pin 5, and further improving the stability of the overall installation.
[0052] In the above embodiment, please refer to Figure 11 The inner wall of the clamping plate 13 is provided with a flexible protective sleeve, which is detachably arranged on the inner wall of the clamping plate 13. The flexible protective sleeve prevents the clamping plate 13 from directly contacting the outer wall of the three-phase male pin 5, effectively preventing the outer wall of the three-phase male pin 5 from being worn during the clamping process. The flexible protective sleeve is made of insulating material, which can prevent electric leakage, and the detachable arrangement facilitates regular maintenance and replacement by the staff.
[0053] Embodiment two: please refer to Figure 7 and Figure 10 The overall structure is similar to that of embodiment one. One end of the plastic elastic sheet 10 is concave, and the inner wall of the plastic elastic sheet 10 is provided with a tapered surface. The connection between one end of the plastic elastic sheet 10 and the tapered ring 15 is smooth, and the outer diameter of one end of the tapered surface is the same as the inner diameter of the plastic elastic sheet 10. The concave arrangement facilitates the extrusion of the ejector rod 12 during the subsequent elastic reset process, and the tapered surface allows the plastic elastic sheet 10 to slide away from the outer wall of the tapered ring 15 during the sliding process of the three-phase female head 9. Thus, the plastic elastic sheet 10 can still limit and fix the tapered ring 15, and after the plastic elastic sheet 10 extrudes the ejector rod 12, the outer wall of the tapered ring 15 will be in full contact with the inner wall of the plastic elastic sheet 10, further sealing the slot of the ejector rod 12 and effectively preventing the sliding of the ejector rod 12 during subsequent gluing.
[0054] In the above embodiment, please refer to Figure 10The outer wall of the push rod 12 and one end of the plastic spring 10 are arc-shaped, and a smooth surface is provided at the arc-shaped end face. The arc shape facilitates the movement of the plastic spring 10 to the top of the push rod 12 when it slides through the outer wall of the conical ring 15 to complete the compression work. The smooth surface of the arc-shaped end face effectively reduces the sliding friction between the two, ensuring the stability of the plastic spring 10 sliding at the push rod 12.
[0055] In practical operation, this invention is used by fixing the stripped and tinned three-phase wires 4 to the three-phase female connector 9. Then, each set of three-phase wires 4 is inserted into the plastic spring 10 of the male connector back cover 3. At this time, one end of the plastic spring 10 will be pressed against the conical ring 15. The three-phase male pin 5 passes through the female connector 2 and the male connector 1 and is inserted into the three-phase female connector 9, so that the three-phase wires 4 are separated and placed separately. After the three-phase wires 4 are connected, they avoid swinging and wear with other structural components. At the same time, it reduces the indirect contact between the three-phase wires 4 and other structural components, effectively reducing the overall failure rate of the UAV. Furthermore, the male connector 1, the female connector 2 and the male connector back cover 3 are limited and fixed by the bolt assembly, so that there will be no situation where a bunch of three-phase wires 4 are exposed and hanging outside after being connected.
[0056] Simultaneously, when the male connector back cover 3 is inserted into the socket 6 inside the male connector 1, one end of the socket 6 will push the three-phase female connector 9 to slide to one side. At this time, the plastic spring 10 will be stuck in the slot 14 of the three-phase female connector 9. The slot 14 limits the three-phase female connector 9, preventing the three-phase wire 4 from sliding out. The plastic spring 10 will also squeeze the push rod 12 on the three-phase female connector 9. During this process, the push rod 12 drives the clamping plate 13 at the bottom to limit and clamp the three-phase male pin 5, thereby ensuring the stability of the connection between the three-phase male pin 5 and the three-phase wire 4 and preventing the three-phase male pin 5 from slipping off the three-phase wire 4 during the drone's flight.
[0057] The high-voltage connector of this invention integrates high-voltage and low-voltage modules by realizing the plug-in connection of phase wires and the pin header connection of signal wires, resulting in a smaller product size, no risk of wear, and higher safety.
[0058] Although embodiments of the present invention have been shown and described, these specific embodiments are merely explanations of the invention and are not intended to limit it. The specific features, structures, materials, or characteristics described may be combined in any suitable manner in one or more embodiments or examples. After reading this specification, those skilled in the art may make modifications, substitutions, and variations to the embodiments as needed without departing from the principles and spirit of the invention, but such modifications, substitutions, and variations are protected by patent law as long as they are within the scope of the claims of the present invention.
Claims
1. A high-voltage connector for unmanned aerial vehicles (UAVs), comprising a male connector (1), three-phase male pins (5), three-phase wires (4), and a signal wire (16), wherein the two ends of the male connector (1) are respectively provided with a female connector (2) and a male connector back cover (3), characterized in that: One end of the three-phase line (4) is fitted with a three-phase female connector (9), wherein the male connector back cover (3) is provided with a plastic spring (10) that mates with the three-phase female connector (9), the male connector (1) is provided with a socket (6), and the three-phase male pin (5) slides with the female connector (2). A push rod (12) is elastically inserted through the three-phase female connector (9), one end of which is located inside the three-phase female connector (9) and connected to a clamp (13). A slot (14) is provided on the outer wall of the three-phase female connector (9) at the push rod (12). A conical ring (15) is provided on one side of the slot (14) on the outer wall of the three-phase female connector (9). One end of the signal line (16) passes through to the connector (2) and is connected to a pin header (17) inside the connector (2). One end of the plastic spring (10) is concave and a conical surface is provided on the inner wall of the plastic spring (10). The connection between one end of the plastic spring (10) and the conical ring (15) is smooth. The outer diameter of one end of the conical surface is the same as the inner diameter of the plastic spring (10). During the sliding process of the plastic spring sheet, it will squeeze the top rod, causing the top rod to drive the bottom clamping plate to slide downward. Since one end of the three-phase line is located on one side of the clamping plate in the initial state, and the three-phase male pin is in contact with the three-phase line at this time, one end of the three-phase male pin will be at the bottom of the clamping plate. Under the action of the top rod, the clamping plate will limit and clamp the three-phase male pin. The male connector (1) and the male connector back cover (3) are both provided with a first threaded hole (7), and the outer walls of the male connector (1) and the female connector (2) are both provided with a second threaded hole (8). The first threaded hole (7) and the second threaded hole (8) are connected by a bolt assembly.
2. The UAV high-voltage connector according to claim 1, characterized in that: The female connector (2) has a through hole, and the outer wall of the three-phase male pin (5) has a horizontal surface that matches the through hole.
3. The UAV high-voltage connector according to claim 1, characterized in that: The inner wall of the three-phase female connector (9) is provided with an inner groove (11), wherein the depth of the inner groove (11) is greater than the thickness of the clamping plate (13).
4. The UAV high-voltage connector according to claim 1, characterized in that: One end of the socket (6) is open, and the inner wall of the socket (6) is provided with a smooth surface.
5. The UAV high-voltage connector according to claim 1, characterized in that: The inner wall of the clamp (13) is provided with a flexible protective sleeve, wherein the flexible protective sleeve and the inner wall of the clamp (13) are detachable.
6. The UAV high-voltage connector according to claim 1, characterized in that: The outer wall of the male connector (1) is provided with a sealing ring, and the inner wall of the female connector (2) is provided with a groove for the sealing ring to be inserted.
7. The UAV high-voltage connector according to claim 1, characterized in that: An elastic component is provided in the interlayer of the three-phase female connector (9), wherein one end of the elastic component is fixedly connected to the three-phase female connector (9), and the other end is connected to the outer wall of the top rod (12).
8. The UAV high-voltage connector according to claim 1, characterized in that: The outer wall of the top rod (12) and one end of the plastic spring sheet (10) are arranged in an arc shape.
Citation Information
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