Satellite-borne device internal high-voltage transmission device

By using polyimide materials and specially designed electrical connectors, the problems of signal interference and welding damage in high-voltage transmission in space probes have been solved, achieving stable transmission of high-voltage signals and miniaturization of the probe.

CN121192435BActive Publication Date: 2026-04-14NAT SPACE SCI CENT CAS
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Patent Information

Authority / Receiving Office
CN · China
Patent Type
Patents(China)
Current Assignee / Owner
NAT SPACE SCI CENT CAS
Filing Date
2022-12-21
Publication Date
2026-04-14

AI Technical Summary

Technical Problem

In existing space probes, high-voltage transmission can easily lead to signal interference and instrument damage, and traditional welding methods increase the difficulty of disassembly and assembly and the risk of solder pads falling off, which cannot meet the requirements of miniaturized design.

Method used

The plug and socket bases are made of polyimide material, and through a special structural design and potting method, combined with high-insulation low-density materials and vent holes, stable transmission of high-voltage signals is achieved, reducing the interference of high-voltage transmission on analog circuits and the risk of soldering damage.

Benefits of technology

The voltage withstand value of the electrical connector has been improved, the weight and volume have been reduced, the complexity of disassembly and assembly has been reduced, and the safety and reliability of the detector have been enhanced, making it suitable for high-voltage transmission in space environment detectors.

✦ Generated by Eureka AI based on patent content.

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Abstract

The present application relates to the field of high-voltage electrical connector between boards, and particularly relates to a high-voltage transmission device inside a satellite-borne device. The electrical connector of the present application comprises a plug structure and a socket structure. The plug structure comprises a plug base and a pin; the plug base is internally designed with a slot according to the shape of the pin; the pin is embedded into the plug base by impact and is fixed by glue filling and adhesion through glue filling holes between the plug base and the pin; the socket structure comprises a socket base, a spigot and a spigot and spigot sleeve assembly; the socket base is internally designed with a slot according to the shape of the spigot and the spigot and spigot sleeve assembly after assembly; the sidewall of the plug base and the socket base is designed with at least two air release holes, two glue filling holes and two screw mounting holes; the spigot and the spigot and spigot sleeve assembly are assembled by screwing; the spigot and the spigot and spigot sleeve assembly are embedded into the socket base by impact after assembly, and the three are fixed by glue filling and adhesion through the glue filling holes.
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Description

Technical Field

[0001] This invention relates to the fields of aerospace electrical connectors, inter-board high-voltage electrical connectors, and high-voltage connectors, specifically to a high-voltage transmission device inside spaceborne equipment. Background Technology

[0002] The design of space probes is complex, requiring division according to instrument functional modules. Probes are typically divided into sensors and electronics enclosures. The electronics enclosure usually houses multiple printed circuit boards (PCBs) in different locations. This spatially isolated modular design reduces noise interference and signal coupling between PCBs, effectively improving probe performance. However, signal exchange is necessary between different PCBs and between electronics and sensors. Signal transmission typically uses aerospace-grade inter-board electrical connectors. To avoid electromagnetic interference to other probes on the satellite platform, the probe's electronics and sensors are usually integrated, mounted in different locations within the same housing. The probe housing is typically a sealed enclosure made of metals such as magnesium or aluminum. The housing effectively shields the probe's internal signals from the outside; therefore, all internal signals from the electronics and sensors must be transmitted or wired within the housing. Signal transmission between boards and between sensors and electronics typically uses internal electrical connectors or more traditional lead-wire connections.

[0003] There are many types of space environment detectors, each with different requirements for electrical connectors. Major space environment detectors such as low-energy particle detectors, optical detectors, X-ray detectors, and high-energy particle detectors all require high-voltage power supplies (tens of thousands of volts) for their sensors to operate. Furthermore, the scientific data generated by these sensors is analog signal. Therefore, the electronics boxes for these detectors typically include a high-voltage circuit module and a scientific data acquisition module. High voltage is prone to discharge, which can easily cause sensor malfunctions and potentially damage the instrument. Simultaneously, the scientific data generated by the sensors in these detectors is analog signal with a small amplitude, making it highly susceptible to interference from high-voltage signals, leading to abnormal data. Therefore, high-voltage transmission is particularly crucial in the design of these detectors.

[0004] Miniaturization and lightweight design have become major development trends in aerospace probe development in recent years. Therefore, miniaturization and light weight have become important considerations for selecting aerospace electrical connectors. Furthermore, the harsh operating environment of aerospace probes places stringent requirements on the electrical connectors' resistance to high and low temperatures and vacuum environments. For space environment detectors such as low-energy particle detectors, optical detectors, X-ray detectors, and high-energy particle detectors, the inter-board electrical connectors must not only be resistant to high and low temperatures and vacuum environments, but also withstand high voltage.

[0005] Currently, there are no lightweight electrical connectors on the market capable of withstanding tens of thousands of volts. Therefore, the high-voltage transmission of space environment detectors such as low-energy particle detectors, optical detectors, X-ray detectors, and high-energy particle detectors all rely on traditional soldered high-voltage wires. In the early stages of instrument design, the detector undergoes numerous sensor and electronics assembly and disassembly tests. Each disassembly and reassembly requires soldering and desoldering the high-voltage solder joints. Repeated soldering can easily lead to the detachment of printed circuit board pads, and the soldering and desoldering also increases the difficulty of disassembling and assembling the instrument. Summary of the Invention

[0006] This invention addresses the problem of internal high-voltage transmission in current detectors by proposing a small-sized, lightweight (8g) aerospace-grade inter-board electrical connector capable of withstanding voltages above 10kV. This connector enables high-voltage transmission within the instrument, effectively preventing interference with other analog circuits or damage to the instrument due to improper soldering. Furthermore, it reduces the complexity of disassembling and assembling the detector's electronics box and sensors, significantly lowers the risk of pad detachment due to repeated soldering, improves the detector's safety and reliability, and expands the application areas of internal high-voltage electrical connectors.

[0007] This invention proposes a high-voltage transmission device for internal use in spaceborne equipment.

[0008] The electrical connector includes: a plug base (8), a pin (9), a socket base (6), and a cannula (14);

[0009] Both the plug base (8) and the socket base (6) are integrally processed from polyimide material;

[0010] The main body materials of the pin (9) and the cannula (14) are both metal, and both are wrapped with a layer of polyimide material on the outside of the main body material;

[0011] The plug base (8) has a pin through hole (8-0), and the pin (9) is disposed in the pin through hole (8-0) and is installed through the plug base (8);

[0012] The socket base (6) has a tube through hole (6-0), and the tube (14) is set in the tube through hole (6-0) and is installed through the socket base (6);

[0013] The diameters of the pin through hole (8-0) and the cannula through hole (6-0) are irregularly designed to form annular grooves that match the shapes of the pin (9) and the cannula (14), respectively.

[0014] The inner end of the pin (10) and the inner end of the tube (12) are paired and connected to form the electrical connector; the outer end of the pin and the outer end of the tube are respectively used for external circuits.

[0015] As an improvement to the above technical solution, the pin (9) includes, in sequence: an inner end (10), a middle part (15), and an outer end;

[0016] The cannula (14) comprises, in sequence: an inner end (12), a middle part (16), and an outer end;

[0017] The inner end of the pin (10) is a solid cylinder; the inner end of the cannula (12) is a hollow cylinder with slots on both sides; the inner end of the pin (10) and the inner end of the cannula (12) are paired and connected.

[0018] The slots on both sides of the inner end of the cannula (12) are used to prevent residual gas inside the electrical connector after the inner end of the pin (10) and the inner end of the cannula (12) are connected;

[0019] The middle part (15) of the pin is used to fix the pin (9) in the plug base (8); after the pin (9) is installed in the plug base (8), the inner end (10) of the pin and the plug base (8) are left with a gap that is consistent with the wall thickness of the tube (14), so that the pin (9) and the tube (14) can be inserted into each other.

[0020] The middle part (16) of the insertion tube is used to fix the insertion tube (14) in the socket base (6).

[0021] As an improvement to the above technical solution, the outer end of the insertion pin is a insertion pin welding cup (11); the outer end of the insertion tube is an insertion tube welding cup (17);

[0022] The pin solder cup (11) and the tube solder cup (17) are used for external circuits, respectively.

[0023] As an improvement to the above technical solution, the cannula (14) further includes a cannula assembly protective tube (13);

[0024] The cannula assembly protective tube (13) is a hollow cylinder, which is screwed on the outside of the cannula docking end (12) to provide a sealed protection for the cannula docking end (12).

[0025] As an improvement to the above technical solution, the middle part (15) of the pin includes, in sequence: a pin clamp (15-1) and a pin glue-filling position (15-2); the outer perimeter of the pin clamp (15-1) is greater than the outer perimeter of the pin glue-filling position (15-2);

[0026] The middle part (16) of the cannula includes, in sequence, a cannula clamp (16-1) and a cannula glue filling position (16-2); the outer perimeter of the cannula clamp (16-1) is greater than the outer perimeter of the cannula glue filling position (16-2);

[0027] The pin clamp (15-1) is used to secure the pin (9) to the corresponding position in the pin through hole (8-0) when the pin (9) is embedded into the plug base (8) by impact; the pin glue filling position (15-2) is used to fill glue after the pin (9) is in the corresponding position to bond the pin (9) and the plug base (8);

[0028] The insertion tube clamp (16-1) is used to secure the insertion tube (14) to the corresponding position in the insertion tube through hole (6-0) when the insertion tube (14) is embedded into the socket base (6) by impact. The insertion tube glue filling position (16-2) is used to fill glue after the insertion tube (4) is in the corresponding position to bond the insertion tube (14) and the socket base (6).

[0029] As an improvement to the above technical solution, both the side wall of the socket base (6) and the side wall of the plug base (8) are provided with a potting hole (4) and a venting hole (5);

[0030] The glue-filling hole (4) on the side wall of the socket base (6) is used to fill glue after the insertion tube (14) is embedded into the socket base (6) by impact, so that the glue-filling position (16-2) of the insertion tube is tightly bonded to the socket base (6);

[0031] The glue-filling hole (4) on the side wall of the plug base (8) is used to fill the plug base (8) with glue after the pin (9) is embedded into the plug base (8) by impact, so that the glue-filling position (15-2) of the pin is tightly bonded to the plug base (8).

[0032] The vent hole (5) is used to vent gas during potting and socket plug connection to prevent gas residue.

[0033] As an improvement to the above technical solution, the pin (9) is embedded into the plug base (8) by impact and then potted with glue to form a plug structure (1).

[0034] The insertion tube (14) is embedded into the socket base (6) by impact and then potted with glue to form the socket structure (2).

[0035] The connection between the plug structure (1) and the socket structure (2) is a crimp-locking method.

[0036] As an improvement to the above technical solution, the electrical connector further includes a mounting screw (3) made of polyimide;

[0037] The mounting screw (3) is used to fix the connected plug structure (1) and socket structure (2) in a set position.

[0038] As an improvement to the above technical solution, the plug base (8) includes: a first plug base structure (8-1), a second plug base structure (8-2), and a third plug base structure (8-3);

[0039] The first structure (8-1) of the plug base is a cylinder with through holes, which is the remaining cylinder after the two sides of the cylinder are cut off parallel to each other along the height direction of the cylinder. This leaves space for screw installation while making the connector smaller and lighter.

[0040] The second structure (8-2) of the plug base is a cylinder with through holes, which is the remaining cylinder after the two sides of the cylinder are cut off parallel to each other along the height direction of the cylinder. This can make the connector smaller and lighter. The cross-sectional area of ​​the second structure (8-2) of the plug base is larger than that of the first structure (8-1) of the plug base, and at least one screw mounting hole (7) is opened on each side.

[0041] The third structure (8-3) of the plug base is a column with a rounded rectangular cross-section and a through hole;

[0042] The through holes of the first structure (8-1), the second structure (8-2), and the third structure (8-3) of the plug base are connected to form a pin through hole (8-0); at least two pin through holes (8-0) are provided;

[0043] When the pin (9) is installed into the plug base (8), the third structure (8-1) of the plug base corresponds to the direction of the inner end (10) of the pin, and the third structure (8-3) of the plug base corresponds to the direction of the pin solder cup (11).

[0044] As an improvement to the above technical solution, the socket base (6) includes: a first socket base structure (6-1), a second socket base structure (6-2), and a third socket base structure (6-3);

[0045] The first structure (6-1) of the socket base is a hollow cylinder surrounding the insertion tube through hole (6-0);

[0046] The second structure (6-2) of the socket base is a cylinder with a through hole, and at least one screw mounting hole (7) is opened on each side of the cylinder;

[0047] The third structure (6-3) of the socket base is a column with a rounded rectangular cross-section and a through hole. The hollow cylinder of the first structure (6-1) of the socket base, the through hole of the second structure (6-2) of the socket base, and the through hole of the third structure (6-3) of the socket base are connected to form a tube through hole (6-0); at least two tube through holes (6-0) are provided.

[0048] After the pin (9) and the cannula (14) are paired and connected, the distance between the two sets meets the high voltage safety distance requirement; the high voltage safety distance requirement is: when the distance is 1mm, the high voltage between the two reaches 3000V to 4000V;

[0049] When the insertion tube (14) is installed into the socket base (6), the first structure (6-1) of the socket base corresponds to the direction of the insertion tube (14) mating end (12), and the third structure (6-3) of the socket base corresponds to the direction of the insertion tube welding cup (17).

[0050] Advantages of the electrical connector of this invention:

[0051] 1. This invention designs an inter-board electrical connector that can withstand voltages of up to 10kV to achieve high-voltage transmission within the instrument;

[0052] 2. This invention uses polyimide (YS20) material as the base of the electrical connector, which effectively improves the withstand voltage of the contacts and effectively reduces the weight of the contacts. Furthermore, this material has been used in orbit on multiple satellites and exhibits excellent insulation properties. Polyimide is a novel high-insulation material with high hardness and is relatively brittle, making it difficult to process and expensive. Currently, few electrical connectors on the market use polyimide as the base.

[0053] 3. This invention proposes a special structural design (grooves, vent holes, etc.) to increase the withstand voltage parameters of the electrical connector;

[0054] 4. The purpose of this invention is to solve the technical problem of high voltage transmission inside the detector; the invention uses high-insulation, low-density polyimide material as the insulating base of the electrical connector, which effectively improves the withstand voltage of the electrical connector, while reducing the weight and volume of the electrical connector, which is beneficial to the miniaturization design of the detector.

[0055] 5. This invention effectively improves the withstand voltage of electrical connectors through structural design and material selection, greatly reduces the complexity of disassembling and assembling detector electronics boxes and sensors, reduces the risk of solder pads falling off after multiple soldering of electronics box and the risk of high voltage transmission interfering with other analog circuits, and has a wide range of application needs in the field of board-to-board connectors, especially in the field of high voltage transmission inside space environment detectors.

[0056] 6. To improve the withstand voltage of the electrical connector, this invention uses polyimide bases to isolate the two cannulas at the socket end and the two pins at the plug end, ensuring that the dielectric material between the two cores is polyimide, a material with a high dielectric constant. The solder cup ends of the pins and cannulas are designed such that the polyimide base is higher than the solder cup, and the cannulas mating ends are designed such that the polyimide base fits tightly against the cannulas, thus increasing the dielectric constant between the two cores. An annular recess is designed on the outer edge of the pin through-hole at the pin mating end to increase the creepage distance. These designs effectively improve the withstand voltage between the two cores and reduce the overall size.

[0057] 7. This invention designs vent holes at the mating ends of the electrical connectors and grooves at the mating ends of the insertion tubes to ensure thorough venting after connector mating. This prevents residual gas inside the connector from causing low-pressure discharge of the transmitted high-voltage signal. The potting process uses vacuum-sealed adhesive and is performed under vacuum conditions to prevent residual gas from remaining inside the potting compound. Attached Figure Description

[0058] Figure 1 is a diagram showing the connection of the internal high-voltage transmission device of the spaceborne equipment of the present invention.

[0059] Figure 2(a) is a schematic diagram of the pin, Figure 2(b) and Figure 2(c) are schematic diagrams of the plug base at two different angles, and Figure 2(d) and Figure 2(e) are the side view and front view of the plug structure along the cross section, respectively.

[0060] Figure 3(a) is a schematic diagram of the insertion tube, Figure 3(b) is a schematic diagram of the socket base, and Figures 3(c) and 3(d) are the side view and front view of the socket structure along the cross section, respectively.

[0061] Figure 4 Diagram showing the mounting holes for the socket and printed circuit board;

[0062] Figure 5 shows the mounting hole diagram for the metal boss at the plug and sensor end.

[0063] Figure 6 shows the docking installation diagram inside the detector.

[0064] Attached Figure Labels

[0065] Detailed Implementation

[0066] The technical solutions provided by the present invention will be further illustrated below with reference to the embodiments.

[0067] The purpose of this invention is to overcome the problem of high-voltage transmission inside the detector.

[0068] This invention provides a high-voltage resistant miniature inter-board electrical connector device. Figure 1 is a docking diagram of the high-voltage transmission device inside the spaceborne equipment of this invention. The electrical connector is divided into a plug structure 1 (pin) and a socket structure 2 (tube). In use, the plug structure 1 and the socket structure 2 are used in pairs.

[0069] Both plug structure 1 and socket structure 2 consist of an insulator base, contact elements (pins, tubes), and a protective tube assembly.

[0070] Figure 2(a) is a schematic diagram of the pin 9, Figure 2(b) and Figure 2(c) are schematic diagrams of the plug structure 1 from two different angles, Figure 2(d) and Figure 2(e) are the side view and front view of the plug structure along the cross section, respectively; Figure 3(a) is a schematic diagram of the tube 14, Figure 3(b) is a schematic diagram of the socket structure 2, Figure 3(c) and Figure 3(d) are the side view and front view of the socket structure along the cross section, respectively; After potting, the pin welding cup 11 and the adjacent parts of the plug base third structure 8-3 are filled with potting compound; the tube welding cup 17 and the adjacent parts of the socket base third structure 6-3 are filled with potting compound.

[0071] The plug structure 1 includes a plug base 8 and a pin 9. The plug base 8 has a groove designed according to the shape of the pin 9, and at least two vent holes 5, two glue holes 4 and two M2 screw mounting holes 7 are designed on the side wall. The pin 9 is embedded into the plug base 8 by impact and glued and fixed to the plug base 8 and the pin 9 by glue through the glue holes 4.

[0072] The socket structure 2 includes a socket base 6, a plug tube 14, and a plug tube protective assembly 13. The socket base 6 has a groove designed according to the shape of the plug tube 4 and the plug tube protective assembly 13 after assembly. At least two vent holes 5, two glue holes 4, and two M2 screw mounting holes 7 are designed on the side wall. The plug tube 14 and the plug tube protective assembly 13 are assembled by tightening the threads. After the plug tube 14 and the plug tube protective assembly 13 are assembled, they are embedded into the socket base 6 by impact and glued and fixed through the glue holes.

[0073] Both the plug base 8 and the socket base 6 are made of high-insulation polyimide (YS20) material. This material has good electrical properties, corrosion resistance, fatigue resistance, high temperature resistance, wear resistance, impact resistance, low density, and long service life. It is widely used in the structural materials of aerospace probes.

[0074] The contacts (pin 9, cannula 14) are made of beryllium bronze (QSn4-3 Y), and the sheath assembly 13 is made of stainless steel (0Cr18Ni10Ti). Both beryllium bronze (QSn4-3 Y) and stainless steel (0Cr18Ni10Ti) are commonly used materials for high-grade electrical connectors. The sealant used for potting is EC 104 A / B, an epoxy adhesive commonly used in aerospace products.

[0075] The connector's structural design features an external insulating base. Pins 9, canopy 14, and sheath assembly 13 are first embedded into the base via impact, then secured a second time using potting compound. The connector has two contacts. One end of plug structure 1 is a pin-type contact, and one end of socket structure 2 is a canopy-type contact. Pin 9 mates with canopy 14. The other ends of both plug structure 1 and socket structure 2 have solder cup-type leads connected to solder joints. Both plug structure 1 and socket structure 2 have two M2 mounting screw holes on their bases, allowing them to be fixed to two parallel printed circuit boards.

[0076] Since the printed circuit board is installed inside the housing and the spacing between the boards is fixed, the electrical connectors between the boards experience very little force, and the screw strength requirements are low. Therefore, the mounting screws 3 of the electrical connector in this design are made of polyimide material, which can effectively prevent high voltage discharge to the metal screws. To prevent high voltage discharge between the two pins, the pins 9 and the tubes 14 of this electrical connector are specially designed.

[0077] Cannula 14 design: The outer layer of cannula 14 is tightly wrapped with polyimide material.

[0078] Pin 9 design: Pin 9 is surrounded by a polyimide material. A gap with the same diameter as the cannula 14 is left between pin 9 and the polyimide material to allow for pin-to-pin insertion. Circular grooves are designed on the sidewalls of the polyimide material to increase the creepage distance on the polyimide surface. This design effectively avoids the risk of discharge when the two cores transmit different high voltages.

[0079] In addition, to prevent residual gas inside the contacts after the electrical connector is mated, which could cause discharge during high-voltage transmission under low air pressure, the protective tube assembly 13, the socket base 6 and the plug base 8 are all designed with vent holes with a diameter of 1-1.5mm on their side walls, and the insertion tube (14) is designed with a slot with a width of 1-1.5mm on its side wall to ensure good vacuum inside the electrical connector when used in a vacuum state.

[0080] The wall thickness of the hollow cylinder is not less than 0.3 mm;

[0081] The diameter of the solid cylinder 10 is 0.7 mm;

[0082] The installation method of the electrical connector is as follows: the connection between the plug structure 1 and the socket structure 2 is a crimping and locking method, that is, the electronic box and the sensor or printed circuit board are assembled and then crimped and locked.

[0083] The schematic diagram of the electrical connector structure in this application is shown below. Figure 1 The electrical connector shown weighs only 8g.

[0084] The socket structure 2 inside the detector is fixed to the printed circuit board, such as... Figure 4 ; The plug structure 1 is fixed to the metal platform inside the detector sensor, such as Figure 5 As shown, Figure 6 The diagram shows the inter-board electrical connector of this application installed at the interface between the detector's internal electronics box and the sensor. The plug is mounted on the base of the housing with screws, and the socket is fixed to the printed circuit board with screws.

[0085] In this implementation case, the performance of the electrical connector was tested, including the following tests:

[0086] 1. Atmospheric pressure high and low temperature power-on test: Temperature range: -35℃~+60℃, electrical connector is assembled inside the detector, high voltage transmission range: 0~-2000V.

[0087] 2. Thermal vacuum power-on test: Temperature range: -35℃~+60℃, electrical connector is assembled inside the detector, high voltage transmission range: 0~-6000V.

[0088] 3. Rated withstand voltage test: Temperature: +85℃, the electrical connector is installed separately in the housing, the voltage difference between the two contacts increases in a step-like manner from 1000V, 2000V, 3000V... The high voltage and current of the contacts are monitored using a high voltage probe and current clamp, and the discharge phenomenon is monitored by single-pulse triggering method of oscilloscope. The high voltage is maintained for 60 minutes under each step. According to the test results, the withstand voltage between the two contacts of the electrical connector is better than 10kV.

[0089] As can be seen from the above detailed description of the present invention, the present invention uses high-insulation, low-density polyimide material as the insulating base of the electrical connector, while increasing the dielectric constant between the two cores and increasing the creepage distance in the design, and setting special designs such as venting holes on the connector, which effectively improves the withstand voltage value of the electrical connector, while reducing the weight and volume of the electrical connector, which is beneficial to the miniaturization design of the detector.

[0090] Finally, it should be noted that the above embodiments are only used to illustrate the technical solutions of the present invention and are not intended to limit it. Although the present invention has been described in detail with reference to the embodiments, those skilled in the art should understand that modifications or equivalent substitutions to the technical solutions of the present invention do not depart from the spirit and scope of the technical solutions of the present invention, and all such modifications or substitutions should be covered within the scope of the claims of the present invention.

Claims

1. A high-voltage transmission device inside a spaceborne equipment, characterized in that, The high-voltage transmission device includes: a plug base (8), a pin (9), a socket base (6), and a tube (14); Both the plug base (8) and the socket base (6) are integrally processed from polyimide material; The main body materials of the pin (9) and the cannula (14) are both metal, and both are wrapped with a layer of polyimide material on the outside of the main body material; The plug base (8) has a pin through hole (8-0), and the pin (9) is disposed in the pin through hole (8-0) and is installed through the plug base (8); The socket base (6) has a tube through hole (6-0), and the tube (14) is set in the tube through hole (6-0) and is installed through the socket base (6); The diameters of the pin through hole (8-0) and the cannula through hole (6-0) are irregularly designed to form annular grooves that match the shapes of the pin (9) and the cannula (14), respectively. The pin (9) includes, in sequence: an inner end (10), a middle part (15), and an outer end; The cannula (14) comprises, in sequence: an inner end (12), a middle part (16), and an outer end; The inner end of the pin (10) and the inner end of the tube (12) are paired and connected to form the high voltage transmission device; the outer end of the pin and the outer end of the tube are respectively used for external circuit connection; The inner end of the pin (10) is a solid cylinder; the inner end of the cannula (12) is a hollow cylinder with slots on both sides; the inner end of the pin (10) and the inner end of the cannula (12) are paired and connected. The slots on both sides of the inner end (12) of the insertion tube are used to prevent the residual gas inside the high-voltage transmission device from causing low-pressure discharge of the transmitted high-voltage signal after the inner end (10) of the insertion pin and the inner end (12) of the insertion tube are connected. The cannula (14) also includes a cannula assembly sheath (13); The cannula assembly protective tube (13) is a hollow cylinder, which is screwed and fixed to the outside of the inner end (12) of the cannula to provide a sealed protection for the inner end (12) of the cannula. The outer end of the insertion pin is a insertion pin welding cup (11); the outer end of the insertion tube is an insertion tube welding cup (17); The pin solder cup (11) and the tube solder cup (17) are used for external circuits, respectively; The solder cup end of the pin and cannula is designed with a polyimide base higher than the solder cup; The middle part (15) of the pin includes, in sequence: a pin clamp (15-1) and a pin glue-filling position (15-2); the outer perimeter of the pin clamp (15-1) is greater than the outer perimeter of the pin glue-filling position (15-2); The middle part (16) of the cannula includes, in sequence, a cannula clamp (16-1) and a cannula glue filling position (16-2); the outer perimeter of the cannula clamp (16-1) is greater than the outer perimeter of the cannula glue filling position (16-2); Both the side wall of the socket base (6) and the side wall of the plug base (8) are provided with a glue-filling hole (4) and a vent hole (5); The glue-filling hole (4) on the side wall of the socket base (6) is used to fill glue after the insertion tube (14) is embedded into the socket base (6) by impact, so that the glue-filling position (16-2) of the insertion tube is tightly bonded to the socket base (6); The glue-filling hole (4) on the side wall of the plug base (8) is used to fill the plug base (8) with glue after the pin (9) is embedded into the plug base (8) by impact, so that the glue-filling position (15-2) of the pin is tightly bonded to the plug base (8). The vent hole (5) is used to vent gas during potting and socket plug connection to prevent gas residue; The glue is applied using vacuum-sealed glue and is applied in a vacuum environment to prevent residual gas from entering the glue.

2. The high-voltage transmission device inside the spaceborne equipment according to claim 1, characterized in that, The middle part (15) of the pin is used to fix the pin (9) in the plug base (8); after the pin (9) is installed in the plug base (8), the inner end (10) of the pin and the plug base (8) are left with a gap that is consistent with the wall thickness of the tube (14), so that the pin (9) and the tube (14) can be inserted into each other. The middle part (16) of the insertion tube is used to fix the insertion tube (14) in the socket base (6).

3. The high-voltage transmission device inside the spaceborne equipment according to claim 2, characterized in that, The pin clamp (15-1) is used to secure the pin (9) to the corresponding position in the pin through hole (8-0) when the pin (9) is embedded into the plug base (8) by impact; the pin glue filling position (15-2) is used to fill glue after the pin (9) is in the corresponding position to bond the pin (9) and the plug base (8); The insertion tube clamp (16-1) is used to secure the insertion tube (14) to the corresponding position in the insertion tube through hole (6-0) when the insertion tube (14) is embedded into the socket base (6) by impact. The insertion tube glue filling position (16-2) is used to fill glue after the insertion tube (14) is in the corresponding position to bond the insertion tube (14) and the socket base (6).

4. The high-voltage transmission device inside the spaceborne equipment according to claim 1, characterized in that, The pin (9) is embedded into the plug base (8) by impact and then potted with glue to form a plug structure (1). The insertion tube (14) is embedded into the socket base (6) by impact and then potted with glue to form the socket structure (2). The connection between the plug structure (1) and the socket structure (2) is a crimp-locking method.

5. The high-voltage transmission device inside the spaceborne equipment according to claim 4, characterized in that, The high-voltage transmission device also includes mounting screws (3) made of polyimide; The mounting screw (3) is used to fix the connected plug structure (1) and socket structure (2) in a set position.

6. The high-voltage transmission device inside the spaceborne equipment according to claim 5, characterized in that, The plug base (8) includes: a first plug base structure (8-1), a second plug base structure (8-2), and a third plug base structure (8-3); The first structure (8-1) of the plug base is a cylinder with through holes, which is the remaining cylinder after the two sides of the cylinder are cut off parallel to each other along the height direction of the cylinder. The second structure (8-2) of the plug base is a cylinder with through holes, which is the remaining cylinder after the two sides of the cylinder are cut off parallel to each other along the height direction of the cylinder; the cross-sectional area of ​​the second structure (8-2) of the plug base is larger than that of the first structure (8-1) of the plug base, and at least one screw mounting hole (7) is opened on each side. The third structure (8-3) of the plug base is a column with a rounded rectangular cross-section and a through hole; The through holes of the first structure (8-1), the second structure (8-2), and the third structure (8-3) of the plug base are connected to form a pin through hole (8-0); at least two pin through holes (8-0) are provided; when the pin (9) is installed into the plug base (8), the third structure (8-3) of the plug base corresponds to the direction of the inner end (10) of the pin and the direction of the pin solder cup (11).

7. The high-voltage transmission device inside the spaceborne equipment according to claim 6, characterized in that, The socket base (6) includes: a first socket base structure (6-1), a second socket base structure (6-2), and a third socket base structure (6-3); The first structure (6-1) of the socket base is a hollow cylinder surrounding the insertion tube through hole (6-0); The second structure (6-2) of the socket base is a cylinder with a through hole, and at least one screw mounting hole (7) is opened on each side of the cylinder; The third structure (6-3) of the socket base is a column with a rounded rectangular cross-section and a through hole; The hollow cylinder of the first structure (6-1) of the socket base, the through hole of the second structure (6-2) of the socket base, and the through hole of the third structure (6-3) of the socket base are connected to form a tube through hole (6-0); at least two tube through holes (6-0) are provided; After the pin (9) and the tube (14) are paired and connected, the distance between the two sets meets the high-voltage safety distance; when the tube (14) is installed into the socket base (6), the first structure (6-1) of the socket base corresponds to the direction of the inner end (12) of the tube (14), and the third structure (6-3) of the socket base corresponds to the direction of the tube welding cup (17).

Citation Information

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