Satellite assembly auxiliary material multifunctional winding device

Abstract

The application discloses a kind of satellite assembly auxiliary material multifunctional winding equipment, comprising: base, electrical system, quick-release conversion head, damping winding machine, wire winding mechanism and machine cover;Wherein, machine cover is installed on base;Electrical system is fixed by base and machine cover installation;Electrical system is connected with damping winding machine or wire winding mechanism by quick-release conversion head.The satellite assembly auxiliary material multifunctional winding equipment described in the application is suitable for the winding processing of film and wire materials, controlled by electrical system, and the winding speed, winding direction and winding locking mode can be accurately controlled, effectively improving the winding efficiency, winding accuracy, eliminating material waste and rework.

Description

Technical Field

[0001] This invention belongs to the field of spacecraft overall assembly technology, and in particular relates to a multi-functional winding device for satellite assembly auxiliary materials. Background Technology

[0002] During satellite assembly, strip-shaped membrane material needs to be wound into small rolls to facilitate thermal control and EMC coating of pipelines and cables. Current technology involves manual winding of the membrane material using a hand-held electric rotary tool with cotter pins. This method suffers from the following problems: 1) The operating speed and rotation rate cannot be quantitatively controlled, resulting in low processing efficiency; 2) It is difficult to align the cotter pins with the shaft of the electric rotary tool, leading to misalignment, low processing accuracy, and poor product consistency; 3) The membrane material is prone to loosening after processing, easily requiring rework; 4) The electric rotary tool lacks an emergency stop mechanism, posing a safety risk; 5) The wound membrane material lacks a storage device, making it prone to detachment during use and hindering practicality.

[0003] During satellite assembly, wire materials need to be wound into ring bundles of different lengths according to process requirements to meet the needs of different procedures. Current technology involves manually winding the wire materials, which has the following main problems: 1) Manual winding has low precision, requiring allowances to meet requirements, resulting in material waste; 2) Manual winding results in inconsistent ring bundle diameters, leading to poor product consistency and hindering standardized management and operations; 3) Manual operation is inefficient, requires standing, and is physically demanding. Summary of the Invention

[0004] The technical problem solved by the present invention is to overcome the shortcomings of the prior art and provide a multifunctional winding equipment for satellite assembly auxiliary materials, which is suitable for winding and processing of membrane and wire materials.

[0005] To address the aforementioned technical problems, this invention discloses a multifunctional winding device for satellite assembly auxiliary materials, comprising: a base, an electrical system, a quick-release adapter, a damping winding device, a wire winding mechanism, and a cover; wherein, the cover is mounted on the base; the electrical system is fixedly mounted via the base and the cover; and the electrical system is connected to the damping winding device or the wire winding mechanism via the quick-release adapter.

[0006] In the aforementioned multi-functional winding equipment for satellite assembly auxiliary materials, the base serves as the foundation of the entire equipment and includes: a base plate and shock-absorbing pads; among them, four shock-absorbing pads are respectively set at the four corners of the bottom of the base plate to alleviate vibration and impact during equipment operation and ensure stable operation of the equipment.

[0007] In the aforementioned multi-functional winding equipment for satellite assembly auxiliary materials, the electrical system includes: a power module, a motor, a servo module, a modulator, and a heat sink; wherein, the power module, motor, and servo module are mounted on the base plate; the modulator is located on the front of the cover; and the heat sink is located on the back of the cover.

[0008] In the aforementioned multi-functional winding equipment for satellite assembly auxiliary materials,

[0009] The power module provides the voltage required for the operation of the motor, servo module, and modulator.

[0010] The modulator is used to respond to user operations, generate corresponding control commands, and send them to the servo module.

[0011] The servo module is used to control the operation of the motor according to control commands;

[0012] The motor is used to drive the damping winding device or wire winding mechanism to rotate via a quick-release adapter.

[0013] A radiator is used to dissipate heat from an electrical system, ensuring its stable operation.

[0014] In the aforementioned multi-functional winding equipment for satellite assembly auxiliary materials, the modulator includes: a display, a status indicator light, a multi-functional adjustment knob, a locking key, a direction switching key, a stop key, a start key, and an emergency stop switch; wherein, the display is used to display the operating status information of the equipment; the status indicator light is used to indicate the operating status of the equipment; the multi-functional adjustment knob, locking key, direction switching key, stop key, start key, and emergency stop switch are used to realize the operation control of the equipment.

[0015] In the aforementioned multi-functional winding equipment for satellite assembly auxiliary materials, the cover is equipped with mounting interfaces for installing modulators, radiators, and emergency stop switches, as well as air circulation channels; the air circulation channels are used to dissipate heat from the electrical system and ensure its stable operation.

[0016] In the aforementioned multi-functional winding equipment for satellite assembly auxiliary materials, a quick-release adapter is installed on the output shaft of the motor for connection with the damping winding device or wire winding mechanism, enabling quick clamping and disassembly of the damping winding device or wire winding mechanism.

[0017] In the aforementioned multi-functional winding equipment for satellite assembly auxiliary materials, the damping winding device includes: a damping receiver and a winding adapter.

[0018] A damping housing includes: a tubular body, a silicone oil damper, a wound shaft, and a miniature bearing; wherein, the tubular body has an overall through-tube structure, and a through-tube rectangular auxiliary material inlet / outlet is provided on the side of the tubular body; the silicone oil damper is installed at one end of the tubular body, and a connecting shaft is provided at one end of the silicone oil damper; the wound shaft is installed inside the tubular body, and a through-tube rectangular auxiliary material fixing port is provided on the side of the wound shaft, one end of the wound shaft mates with the connecting shaft, and a rectangular boss is provided at the other end of the wound shaft; the miniature bearing is installed at the other end of the tubular body, the bearing outer sleeve of the miniature bearing mates with the inner wall of the tubular body, and the bearing inner sleeve of the miniature bearing mates with the wound shaft;

[0019] The winding adapter has a cylindrical stepped structure; one end of the winding adapter is provided with a rectangular groove that mates with the rectangular boss of the winding shaft; the other end of the winding adapter mates with the quick-release adapter.

[0020] In the aforementioned multi-functional winding equipment for satellite assembly auxiliary materials, the wire winding mechanism includes: a base, a transfer shaft, a flip plate, a positioning shaft, a sliding block, and a limiting block;

[0021] The base includes: a chuck, a threaded shaft, and flap seats; wherein, the chuck has a disc-shaped structure; the chuck is provided with a wire material slot for fixing wire materials; the threaded shaft is provided on the chuck; the threaded shaft is provided with external threads; four flap seats are evenly distributed on the chuck;

[0022] The adapter shaft is located on one side of the chuck and is used to mate with the quick-release adapter.

[0023] The four flaps are set on the corresponding four flap seats and are connected and fixed by the positioning shaft. The flaps can rotate along the positioning shaft.

[0024] The sliding block is provided with an internal thread, which mates with the external thread on the threaded shaft and is installed on the threaded shaft; the sliding block can move axially along the threaded shaft; the outer end face of the sliding block contacts the flap, and the movement of the sliding block controls the outward and inward movement of the flap;

[0025] The limit block is set on the threaded shaft and is used to limit the sliding block.

[0026] In the aforementioned multi-functional winding equipment for satellite assembly auxiliary materials, during operation:

[0027] Connect the device to a power source; the electrical system is in standby mode.

[0028] The motor's operating speed, direction of travel, and locking mode are set via the modulator;

[0029] When the equipment uses a damping winding device for winding, first install the winding adapter onto the quick-release adapter head; then mate the winding shaft with the winding adapter device; then pass the film or wire material through the rectangular auxiliary material inlet and outlet on the tubular body and fix it in the rectangular auxiliary material fixing port on the winding shaft; the control electrical system works, driving the damping winding device to rotate through the quick-release adapter head to wind the film or wire material; finally, remove the wound film or wire material to complete the winding of the film or wire material.

[0030] When the equipment uses a wire winding mechanism for winding, first install the wire winding mechanism onto the quick-release adapter head; then tighten the sliding block clockwise to control the flap to extend outward; then hang the head of the wire material on the wire material slot on the chuck; control the electrical system to work, and drive the wire winding mechanism to wind the wire material through the quick-release adapter head; finally, loosen the sliding block counterclockwise to control the flap to close inward, remove the wound wire, and complete the winding of the wire material.

[0031] The present invention has the following advantages:

[0032] (1) This invention discloses a multi-functional winding equipment for satellite assembly auxiliary materials. It is controlled by an electrical system and can accurately control the winding speed, winding direction and winding locking mode, effectively improving winding efficiency and accuracy, and eliminating material waste and rework.

[0033] (2) This invention discloses a multi-functional winding equipment for satellite assembly auxiliary materials. The electrical system is equipped with an emergency stop switch, which effectively ensures production safety.

[0034] (3) This invention discloses a multi-functional winding equipment for satellite assembly auxiliary materials. It can quickly replace the damping winding device and the wire winding mechanism through a quick-release conversion head, and can meet the winding processing of different types of materials, realizing multi-functional processing, high-precision processing and standardized processing.

[0035] (4) This invention discloses a multi-functional winding equipment for satellite assembly auxiliary materials. When the damping winding device is used for winding, the material is not easy to loosen after winding and is conducive to the later assembly implementation. When the wire winding mechanism is used, the winding can be quickly disassembled. It has the advantages of high winding efficiency and high quality. Attached Figure Description

[0036] Figure 1 This is a schematic diagram of the structure of a multi-functional winding device for satellite assembly auxiliary materials during the assembly of a damping winding device, according to an embodiment of the present invention.

[0037] Figure 2 This is a schematic diagram of the structure of a multi-functional winding device for satellite assembly auxiliary materials in an assembly wire winding mechanism according to an embodiment of the present invention;

[0038] Figure 3 This is a schematic diagram of the structure of a base in an embodiment of the present invention;

[0039] Figure 4 This is an installation diagram of an electrical system according to an embodiment of the present invention;

[0040] Figure 5 This is a schematic diagram of the installation of a modulator according to an embodiment of the present invention;

[0041] Figure 6 This is a schematic diagram of the structure of a damping winding device according to an embodiment of the present invention;

[0042] Figure 7 This is a cross-sectional view of a damping winding device according to an embodiment of the present invention;

[0043] Figure 8 This is a schematic diagram of the structure of a wire winding mechanism according to an embodiment of the present invention;

[0044] Figure 9 This is a cross-sectional view of a wire winding mechanism according to an embodiment of the present invention. Detailed Implementation

[0045] To make the objectives, technical solutions, and advantages of the present invention clearer, the embodiments disclosed in the present invention will be described in further detail below with reference to the accompanying drawings.

[0046] One of the core ideas of this invention is to address the problems of existing winding schemes, such as the inability to quantitatively control the number of winding turns and winding speed, the inability to switch winding directions, low processing accuracy, low efficiency, poor product consistency, material waste, safety hazards, and poor implementability. This invention proposes a multi-functional winding device for satellite assembly auxiliary materials. It enables precise quantitative control of the number of winding turns and winding speed, allows for switching of winding directions, and facilitates quick replacement of the damping winding device and the wire winding mechanism via a quick-release conversion head, thereby enabling the winding of various materials. When using the damping winding device, the material is less prone to loosening after winding, which is beneficial for subsequent assembly. When using the wire winding mechanism, quick disassembly after winding is possible. It boasts advantages such as high winding efficiency and high quality.

[0047] Reference Figures 1-2 In this embodiment, the multi-functional winding equipment for satellite assembly auxiliary materials includes: a base 1, an electrical system 2, a quick-release adapter 3, a damping winding device 4, a wire winding mechanism 5, and a cover 6. The cover 6 is mounted on the base 1; the electrical system 2 is fixedly mounted via the base 1 and the cover 6; and the electrical system 2 is connected to the damping winding device 4 or the wire winding mechanism 5 via the quick-release adapter 3.

[0048] In this embodiment, as Figure 3As shown, the base 1 serves as the foundation of the entire equipment and includes: a base plate 101 and shock-absorbing pads 102. Four shock-absorbing pads 102 are respectively positioned at the four corners of the bottom of the base plate 101 to mitigate vibrations and impacts during equipment operation, ensuring stable equipment operation.

[0049] In this embodiment, as Figures 4-5 As shown, the electrical system 2 includes: a power supply module 201, a motor 202, a servo module 203, a modulator 204, and a heat sink 205. The power supply module 201, motor 202, and servo module 203 are mounted on the base plate 101; the modulator 204 is located on the front of the cover 6; and the heat sink 205 is located on the back of the cover 6.

[0050] Power module 201 primarily provides the necessary voltage for the operation of motor 202, servo module 203, and modulator 204. Modulator 204 primarily responds to user operations, generates corresponding control commands, and sends them to servo module 203. Servo module 203 primarily controls the operation of motor 202 according to the control commands. Motor 202 primarily drives the damping winding device 4 or wire winding mechanism 5 to rotate via quick-release adapter 3. Heat sink 205 primarily dissipates heat from the electrical system 2, ensuring its stable operation.

[0051] The modulator 204 includes: a display 2041, status indicator lights 2042, a multi-function adjustment knob 2043, a lock key 2044, a direction switching key 2045, a stop key 2046, a start key 2047, and an emergency stop switch 2048. The display 2041 is used to display the operating status information of the device. The status indicator lights 2042 are used to indicate the operating status of the device, including, but not limited to: a running status indicator, a self-locking status indicator, a forward status indicator, and a reverse status indicator. The multi-function adjustment knob 2043, lock key 2044, direction switching key 2045, stop key 2046, start key 2047, and emergency stop switch 2048 are used to control the operation of the device.

[0052] In this embodiment, the cover 6 is provided with mounting interfaces for installing the modulator 204, the radiator 205, and the emergency stop switch 2048, as well as an air circulation channel 601. The air circulation channel 601 is used to dissipate heat from the electrical system 2, ensuring its stable operation.

[0053] In this embodiment, the quick-release adapter 3 is installed on the output shaft of the motor 202 and is used to connect with the damping winding device 4 or the wire winding mechanism 5, so as to realize the quick clamping and disassembly of the damping winding device 4 or the wire winding mechanism 5.

[0054] In this embodiment, the damping winding device 4 is mainly used for winding film and wire materials. The wound material is not loose, effectively eliminating waste and facilitating the next step of the process. For example... Figures 6-7 As shown, the damping winding device 4 includes: a damping housing 401 and a winding adapter 402. The damping housing 401 includes: a tubular body 4011, a silicone oil damper 4012, a winding shaft 4013, and a miniature bearing 4014. The tubular body 4011 has a through-tube shape, and its side has a through-tube rectangular auxiliary material inlet / outlet 40111. The silicone oil damper 4012 is installed at one end of the tubular body 4011, and a connecting shaft 40121 is provided at one end of the silicone oil damper 4012. The winding shaft 4013 is installed inside the tubular body 4011. The side of the 013 has a through rectangular auxiliary material fixing port 40131. One end of the winding shaft 4013 mates with the connecting shaft 40121, and the other end of the winding shaft 4013 has a rectangular boss 40132. The miniature bearing 4014 is installed at the other end of the tubular body 4011. The bearing outer sleeve of the miniature bearing 4014 mates with the inner wall of the tubular body 4011, and the bearing inner sleeve of the miniature bearing 4014 mates with the winding shaft 4013. To reduce weight, the miniature bearing 4014 can be made of nylon or other engineering plastics. The winding adapter 402 has a cylindrical stepped structure. One end of the winding adapter 402 has a rectangular groove 4021, which mates with the rectangular boss 40132 of the winding shaft 4013. The other end of the winding adapter 402 mates with the quick-release adapter 3.

[0055] In this embodiment, the wire winding mechanism 5 is mainly used for winding wire materials. For example... Figures 8-9As shown, the wire winding mechanism 5 includes: a base 501, an adapter shaft 502, a flap 503, a positioning shaft 504, a sliding block 505, and a limiting block 506. The base 501 includes: a chuck 5011, a threaded shaft 5012, and flap seats 5013. The chuck 5011 has a disc-shaped structure and a wire material slot 50111 for fixing the wire material. The threaded shaft 5012 is mounted on the chuck 5011 and has external threads. Four flap seats 5013 are evenly distributed on the chuck 5011. The adapter shaft 502 is located on one side of the chuck 5011 and is used to cooperate with the quick-release adapter head 3. The four flaps 503 are mounted on corresponding flap seats 5013 and are connected and fixed by the positioning shaft 504. The flaps 503 can rotate along the positioning shaft 504. The sliding block 505 has an internal thread that mates with the external thread on the threaded shaft 5012 and is mounted on the threaded shaft 5012. The sliding block 505 can move axially along the threaded shaft 5012. The outer end face of the sliding block 505 contacts the flap 503, and the movement of the sliding block 505 controls the outward and inward movement of the flap 503. A limiting block 506 is provided on the threaded shaft 5012 to limit the sliding block 505.

[0056] In this embodiment, the working principle of the multi-functional winding equipment for satellite assembly auxiliary materials is as follows:

[0057] Connect the device to a power source; electrical system 2 is in standby mode.

[0058] The operating speed, direction of operation, and locking mode of the motor 202 are set by the modulator 204.

[0059] When the equipment uses the damping winding device 4 for winding processing, first install the winding adapter 402 onto the quick-release adapter 3; then mate the winding shaft 4013 with the winding adapter 402; then pass the film or wire material through the rectangular auxiliary material inlet / outlet 40111 on the tubular body 4011 and fix it in the rectangular auxiliary material fixing port 40131 on the winding shaft 4013; the control electrical system 2 works, driving the damping winding device 4 to rotate through the quick-release adapter 3 to wind the film or wire material; finally, remove the wound film or wire material to complete the winding of the film or wire material.

[0060] When the equipment uses the wire winding mechanism 5 for winding processing, first install the wire winding mechanism 5 onto the quick-release adapter 3; then tighten the sliding block 505 clockwise to control the flap 503 to extend outward; then hang the head of the wire material on the wire material slot 50111 on the chuck 5011; control the electrical system 2 to work, and drive the wire winding mechanism 5 to wind the wire material through the quick-release adapter 3; finally, loosen the sliding block 505 counterclockwise to control the flap 503 to close inward, remove the wound wire, and complete the winding of the wire material.

[0061] It should be noted that if any sudden situation arises that affects safety during equipment operation, the emergency stop switch can be pressed to stop the equipment from running.

[0062] In summary, this invention discloses a multi-functional winding equipment for satellite assembly auxiliary materials, which has the advantages of high winding accuracy, no material waste, switchable winding direction, meeting different winding requirements, wide applicability, ability to process various materials, non-loosening of materials after winding, effective elimination of waste and rework, rapid disassembly of wire materials after winding, high winding efficiency, and high quality.

[0063] Although the present invention has been disclosed above with reference to preferred embodiments, it is not intended to limit the present invention. Any person skilled in the art can make possible changes and modifications to the technical solutions of the present invention by utilizing the methods and techniques disclosed above without departing from the spirit and scope of the present invention. Therefore, any simple modifications, equivalent changes and alterations made to the above embodiments based on the technical essence of the present invention without departing from the content of the technical solutions of the present invention shall fall within the protection scope of the technical solutions of the present invention.

[0064] The contents not described in detail in this specification are common knowledge to those skilled in the art.

Claims

1. A multi-functional winding device for satellite assembly auxiliary materials, characterized in that, include: The components include a base (1), an electrical system (2), a quick-release adapter (3), a damping winding device (4), a wire winding mechanism (5), and a cover (6); wherein the cover (6) is mounted on the base (1); the electrical system (2) is fixed by the base (1) and the cover (6); the electrical system (2) is connected to the damping winding device (4) or the wire winding mechanism (5) by the quick-release adapter (3).

2. The multi-functional winding equipment for satellite assembly auxiliary materials according to claim 1, characterized in that, The base (1) serves as the foundation of the entire equipment and includes: a base plate (101) and a shock-absorbing pad (102); wherein, four shock-absorbing pads (102) are respectively set at the four corners of the bottom of the base plate (101) to alleviate the vibration and impact during the operation of the equipment and ensure the smooth operation of the equipment.

3. The multi-functional winding equipment for satellite assembly auxiliary materials according to claim 2, characterized in that, The electrical system (2) includes: a power module (201), a motor (202), a servo module (203), a modulator (204), and a heat sink (205); wherein the power module (201), the motor (202), and the servo module (203) are mounted on the base plate (101); the modulator (204) is located on the front of the cover (6); and the heat sink (205) is located on the back of the cover (6).

4. The multi-functional winding equipment for satellite assembly auxiliary materials according to claim 3, characterized in that, The power supply module (201) is used to provide the voltage required for the operation of the motor (202), the servo module (203), and the modulator (204); The modulator (204) is used to respond to user operations, generate corresponding control commands, and send them to the servo module (203); The servo module (203) is used to control the operation of the motor (202) according to the control commands; The motor (202) is used to drive the damping winding device (4) or the wire winding mechanism (5) to rotate via the quick-release adapter (3); The radiator (205) is used to dissipate heat from the electrical system (2) and ensure the stable operation of the electrical system (2).

5. The multi-functional winding equipment for satellite assembly auxiliary materials according to claim 3, characterized in that, The modulator (204) includes: a display (2041), a status indicator (2042), a multi-function adjustment knob (2043), a lock key (2044), a direction switching key (2045), a stop key (2046), a start key (2047), and an emergency stop switch (2048); wherein, the display (2041) is used to display the operating status information of the device; the status indicator (2042) is used to indicate the operating status of the device; the multi-function adjustment knob (2043), the lock key (2044), the direction switching key (2045), the stop key (2046), the start key (2047), and the emergency stop switch (2048) are used to realize the operation control of the device.

6. The multi-functional winding equipment for satellite assembly auxiliary materials according to claim 5, characterized in that, The cover (6) is provided with mounting interfaces for installing modulator (204), radiator (205), emergency stop switch (2048), and air circulation channel (601); wherein, the air circulation channel (601) is used to realize heat dissipation of electrical system (2) and ensure stable operation of electrical system (2).

7. The multi-functional winding equipment for satellite assembly auxiliary materials according to claim 3, characterized in that, The quick-release adapter (3) is installed on the output shaft of the motor (202) and is used to connect with the damping winding device (4) or the wire winding mechanism (5), so as to realize the quick clamping and disassembly of the damping winding device (4) or the wire winding mechanism (5).

8. The multi-functional winding equipment for satellite assembly auxiliary materials according to claim 3, characterized in that, The damping winding device (4) includes: a damping receiver (401) and a winding adapter (402); A damping housing (401) includes: a tubular body (4011), a silicone oil damper (4012), a winding shaft (4013), and a miniature bearing (4014); wherein, the tubular body (4011) has an overall through-tube structure, and a through-tube rectangular auxiliary material inlet / outlet (40111) is provided on the side of the tubular body (4011); the silicone oil damper (4012) is installed at one end of the tubular body (4011), and a connecting shaft (40121) is provided at one end of the silicone oil damper (4012); the winding shaft (4013) is installed... Inside the tubular body (4011), a through rectangular auxiliary material fixing port (40131) is provided on the side of the winding shaft (4013). One end of the winding shaft (4013) is engaged with the connecting shaft (40121), and the other end of the winding shaft (4013) is provided with a rectangular boss (40132). A miniature bearing (4014) is installed at the other end of the tubular body (4011). The bearing outer sleeve of the miniature bearing (4014) is engaged with the inner wall of the tubular body (4011), and the bearing inner sleeve of the miniature bearing (4014) is engaged with the winding shaft (4013). The winding adapter (402) has a cylindrical stepped structure; one end of the winding adapter (402) is provided with a rectangular groove (4021) that cooperates with the rectangular boss (40132) of the winding shaft (4013); the other end of the winding adapter (402) cooperates with the quick-release adapter (3).

9. The multi-functional winding equipment for satellite assembly auxiliary materials according to claim 8, characterized in that, The wire winding mechanism (5) includes: a base (501), a connecting shaft (502), a flap (503), a positioning shaft (504), a sliding block (505), and a limiting block (506); The base (501) includes: a chuck (5011), a threaded shaft (5012), and a flap seat (5013); wherein, the chuck (5011) has a disc-shaped structure; the chuck (5011) is provided with a wire material slot (50111) for fixing wire materials; the threaded shaft (5012) is provided on the chuck (5011); the threaded shaft (5012) is provided with an external thread; four flap seats (5013) are evenly distributed on the chuck (5011); The adapter shaft (502) is located on one side of the chuck (5011) and is used to cooperate with the quick-release adapter (3); Four flaps (503) are set on four corresponding flap seats (5013) and are connected and fixed by a positioning shaft (504). The flaps (503) can rotate along the positioning shaft (504). The sliding block (505) is provided with an internal thread, which mates with the external thread on the threaded shaft (5012) and is installed on the threaded shaft (5012); the sliding block (505) can move axially along the threaded shaft (5012); the outer end face of the sliding block (505) contacts the flap (503), and the movement of the sliding block (505) controls the outward expansion and inward contraction of the flap (503); The limiting block (506) is set on the threaded shaft (5012) and is used to limit the sliding block (505).

10. The multi-functional winding equipment for satellite assembly auxiliary materials according to claim 9, characterized in that, During work: Connect the device to the power supply, and the electrical system (2) is in standby mode; The operating speed, direction of operation, and locking mode of the motor (202) are set by the modulator (204); When the equipment uses a damping winding device (4) for winding processing, first install the winding adapter (402) onto the quick-release adapter (3); then mate the winding shaft (4013) with the winding adapter (402); then pass the film or wire material through the rectangular auxiliary material inlet and outlet (40111) on the tubular body (4011) and fix it in the rectangular auxiliary material fixing port (40131) on the winding shaft (4013); the control electrical system (2) works, drives the damping winding device (4) to rotate through the quick-release adapter (3) to wind the film or wire material; finally, remove the wound film or wire material to complete the winding of the film or wire material. When the equipment uses the wire winding mechanism (5) for winding processing, first install the wire winding mechanism (5) onto the quick-release adapter (3); then tighten the sliding block (505) clockwise to control the flap (503) to extend outward; then hang the head of the wire material on the wire material slot (50111) on the chuck (5011); The electrical control system (2) operates and drives the wire winding mechanism (5) to wind the wire material through the quick-release adapter (3); finally, the sliding block (505) is released counterclockwise, the control flap (503) is closed, the wound wire is removed, and the winding of the wire material is completed.

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