Spacecraft heat pipe polishing and spraying integrated device

Abstract

The invention provides a spacecraft heat pipe grinding and spraying integrated device which comprises a workbench, a first guide frame and a second guide frame are mounted at the top of the workbench; the material carrying assembly can move in the extending direction of the second guide frame, the material carrying top plate is rotatably arranged above the material carrying bottom plate, and a plurality of spacecraft heat pipes can be fixed; the grinding and spraying assembly is used for grinding and spraying the spacecraft heat pipe; the fixing part comprises a first fixing plate unit and a second fixing plate unit, the first fixing plate unit comprises a plurality of first fixing plates arranged on the material carrying top plate in parallel, the second fixing plate unit comprises a second fixing plate, first V-shaped blocks are arranged on the first fixing plates, and second V-shaped blocks matched with the first V-shaped blocks for fixing are arranged on the second fixing plate. A plurality of spacecraft heat pipes are fixed to the material carrying assembly at a time through the fixing piece, the grinding and spraying assembly grinds the spacecraft heat pipes and then conducts spraying immediately, and therefore the multiple spacecraft heat pipes can be ground and sprayed after being installed at a time.

Description

Technical Field

[0001] The present application relates to the technical field of polishing and spraying, and in particular to an integrated device for polishing and spraying a heat pipe of a spacecraft. Background Art

[0002] Spacecraft thermal control aluminum-ammonia heat pipes are mainly made of aluminum, a material that is lightweight, corrosion-resistant and has excellent heat transfer properties. Aluminum has a low density, only about 1 / 3 of steel, which gives aluminum-ammonia heat pipes significant advantages in application scenarios such as spacecraft that require strict weight control. At the same time, aluminum-ammonia heat pipes also have good thermal conductivity and can transfer heat quickly, which is crucial for the thermal control system of spacecraft.

[0003] The manufacturing process of aluminum-ammonia heat pipes for spacecraft thermal control involves multiple steps, including raw material preparation, extrusion molding, heat treatment, machining and shaping, surface treatment, special processing, and quality inspection and testing. Currently, the grinding and spraying processes for aluminum-ammonia heat pipes for spacecraft thermal control have higher technical requirements and special features than other heat pipes. Typically, a single aluminum-ammonia heat pipe is fixed before grinding and spraying. The time between grinding and spraying must be strictly controlled. Spraying should be performed as soon as possible after grinding to avoid secondary oxidation or contamination of the surface. Manual spraying can lead to uneven coating thickness or defects. Therefore, after grinding the heat pipe on the grinder, the heat pipe must be removed and installed on the sprayer for spraying. Once all are completed, the remaining heat pipes are fixed and then polished and sprayed again. This processing method can only process one aluminum-ammonia heat pipe at a time and the heat pipes must be transferred to different processing machines for processing. This method is not only time-consuming and labor-intensive, but also difficult to meet the needs of large-scale production. Summary of the Invention

[0004] Therefore, in order to overcome the shortcomings of the above-mentioned prior art, the present application proposes an integrated device for polishing and spraying spacecraft heat pipes, which solves the problem that spacecraft heat pipes need to be sprayed immediately after polishing, resulting in the inability to process multiple spacecraft heat pipes at one time, so that multiple spacecraft heat pipes can be processed in batches, and multiple surfaces of spacecraft heat pipes can be polished and sprayed after one installation.

[0005] The present application provides a spacecraft heat pipe grinding and spraying integrated device, including: a workbench, on which a first guide frame and a second guide frame perpendicular to the first guide frame are installed. The second guide frames are symmetrically arranged on both sides of the workbench, and the first guide frame is erected on the upper end of the second guide frame; a material loading assembly, including a material loading top plate and a material loading bottom plate. The material loading bottom plate is erected on the upper end of the second guide frame and can move along the extension direction of the second guide frame; the material loading top plate is rotatably arranged above the material loading bottom plate, and multiple spacecraft heat pipes are sequentially fixed on the material loading top plate through fixing members; a grinding and spraying assembly, used for grinding and spraying the spacecraft heat pipes; the grinding and spraying assembly can move along the extension direction of the first guide frame and can also move along the extension direction of the second guide frame; wherein, the fixing member includes a first fixing plate unit and a second fixing plate unit. The first fixing plate unit includes a plurality of first fixing plates arranged in parallel on the material loading top plate, and the second fixing plate unit includes second fixing plates corresponding to the first fixing plates. A first V-shaped block is arranged on the first fixing plate, and a second V-shaped block for cooperating with the first V-shaped block to fix the spacecraft heat pipe is arranged on the second fixing plate.

[0006] Specifically, the heat pipe grinding and spraying integrated device further includes a pressing member, which is used to press the second fixing plate unit onto the first fixing plate unit, and includes: a top frame, a lifting plate, a second screw rod, a knob, a limiting rod and a top block. The top frame is fixedly connected with the material loading top plate; the second screw rod passes through the middle of the top of the top frame, and the rotation of the second screw rod controls the lifting of the lifting plate; the top end of the lifting plate is rotatably connected with the bottom end of the second screw rod, and the lifting of the lifting plate presses or releases the spacecraft heat pipe; the knob is fixedly connected to the top end of the second screw rod, and the knob is used to control the rotation of the second screw rod; the limiting rod passes through both sides of the top of the top frame, and the top block is fixedly arranged at the top end of the limiting rod. The limiting rod is used to limit the lifting plate.

[0007] Specifically, the second fixing plate unit is fixed to the bottom of the lifting plate, and the second fixing plate unit and the lifting plate move together in the vertical direction.

[0008] Specifically, side holes are opened on both side walls of the first V-shaped block, and the side holes are used to make the first V-shaped block and the second V-shaped block overlap after being combined.

[0009] Specifically, the polishing and spraying assembly includes an equipment frame, a polishing unit, a spraying unit, a pushing member, a translating member and a first guide block. The polishing unit is installed at the top of the equipment frame for polishing the spacecraft heat pipe; the spraying unit is installed on a side wall of the equipment frame for spraying the spacecraft heat pipe; the bottom end of the first guide block is slidably connected to the first guide frame, and the bottom of the equipment frame is slidably connected to the top of the first guide block along the extension direction of the second guide frame; the pushing member is used to drive the equipment frame to move along the extension direction of the second guide frame; the translating member is used to drive the equipment frame to move along the extension direction of the first guide frame.

[0010] Specifically, the translation member is arranged at the bottom of the equipment frame, and the translation member includes a first driving part and a first screw. The output part of the first driving part is rotatably connected to one end of the first screw; the first screw rotates to drive the grinding and spraying assembly to move on the first guide frame.

[0011] Specifically, the pushing member is arranged at the bottom of the equipment rack, and includes: a mounting plate, a second driving part and a fixing frame, the mounting plate is fixed to one side of the top end of the first guide block; the second driving part is installed on a side wall of the mounting plate; the fixing frame is transmission-connected to the output end of the second driving part, and is fixedly connected to the equipment rack.

[0012] Specifically, a connecting plate is provided between the top ends of the first guide blocks, the bottom of the connecting plate is slidably connected to the top end of the first guide block along the extension direction of the second guide frame; the top of the connecting plate is fixedly connected to the bottom of the equipment frame.

[0013] Specifically, the material loading assembly further includes a moving part and a rotating part. The moving part is used to drive the material loading assembly to move along the extension direction of the second guide frame; the rotating part is used to drive the material loading top plate to rotate relative to the material loading bottom plate.

[0014] Specifically, the movable member includes: a third guide block and a third driving part, the top of the third guide block is fixedly connected to the bottom of the loading base plate, and the bottom of the third guide block is slidingly connected to the second guide frame; the third driving part is used to drive the third guide block to move.

[0015] Specifically, the rotating member includes a support frame and a fourth driving part, the support frame is fixed to the bottom surface of the loading base plate, and the fourth driving part is arranged in the inner wall of the support frame; the output shaft of the fourth driving part passes through the loading base plate and is transmission-connected to the loading top plate, for driving the loading top plate to rotate relative to the loading base plate.

[0016] Compared with the prior art, in the present application, multiple spacecraft heat pipes are fixed on the loading top plate at one time through fixing parts, and the operation is simple. After the fixing is completed, the grinding and spraying assembly is moved in the extending direction of the first guide frame so that the grinding and spraying assembly is aligned with the outermost spacecraft heat pipe. Then, the loading assembly and the grinding and spraying assembly are sequentially moved in the extending direction of the second guide frame so that the grinding and spraying assembly approaches the spacecraft heat pipe. The grinding and spraying assembly grinds and sprays the spacecraft heat pipe. Then, the grinding and spraying assembly is moved in the extending direction of the second guide frame so that the grinding and spraying assembly moves away from the spacecraft heat pipe. The grinding and spraying assembly is moved in the extending direction of the first guide frame so that the grinding and spraying assembly is aligned with the next spacecraft heat pipe to be processed. The above steps are repeated to grind and spray one side of the spacecraft heat pipe in sequence, processing multiple spacecraft heat pipes simultaneously, saving time and labor, and meeting the requirements of large-scale production.

[0017] The grinding and spraying assembly realizes integrated grinding and spraying processing, reduces the conversion time of the spacecraft heat pipe between the grinding equipment and the spraying equipment, improves the production efficiency, and avoids secondary oxidation or pollution of the ground surface.

[0018] After processing one side of the spacecraft heat pipe, the loading top plate is rotated to face the other side of the spacecraft heat pipe to the grinding and spraying assembly, realizing grinding and spraying processing of the other side, without removing the spacecraft heat pipe for re-fixing, significantly improving the production efficiency and meeting the high-efficiency requirements of large-scale production. Brief Description of the Drawings

[0019] In order to more clearly illustrate the technical solutions of the embodiments of the present application, the drawings required for the embodiments will be briefly introduced below. Obviously, the drawings in the following description are only some embodiments of the present application. For those of ordinary skill in the art, without creative efforts, other drawings can be obtained based on these drawings.

[0020] Figure 1 is a three-dimensional schematic diagram of the integrated grinding and spraying device for spacecraft heat pipes in the embodiment of the present application;

[0021] Figure 2 is a schematic diagram when the loading top plate rotates relative to the loading bottom plate in the embodiment of the present application;

[0022] Figure 3 is a schematic diagram of the unlocked state of the pressing part in the embodiment of the present application;

[0023] Figure 4 is a schematic diagram of the loading assembly part in the embodiment of the present application;

[0024] Figure 5 is a schematic diagram of the first fixing plate and the second fixing plate in the embodiment of the present application;

[0025] Figure 6 It is a rear perspective schematic diagram of the spacecraft heat pipe grinding and spraying integrated device in the embodiment of the present application;

[0026] Figure 7 It is a schematic diagram of the grinding and spraying assembly in the embodiment of the present application;

[0027] Figure 8 It is a schematic diagram of the bottom of the material loading assembly in the embodiment of the present application. Detailed implementation manners

[0028] The embodiments of the present application will be described in detail below with reference to the accompanying drawings.

[0029] The following uses specific specific examples to illustrate the implementation manners of the present application. Those skilled in the art can easily understand other advantages and effects of the present application from the content disclosed in this specification. Obviously, the described embodiments are only a part of the embodiments of the present application, rather than all the embodiments. The present application can also be implemented or applied through other different specific implementation manners. Various details in this specification can also be modified or changed based on different viewpoints and applications without departing from the spirit of the present application. It should be noted that, without conflict, the following embodiments and the features in the embodiments can be combined with each other. All other embodiments obtained by those of ordinary skill in the art based on the embodiments in the present application without creative efforts belong to the scope of protection of the present application.

[0030] It should be noted that the following describes various aspects of the embodiments within the scope of the appended claims. It should be obvious that the aspects described herein can be embodied in a wide variety of forms, and any specific structure and / or function described herein is illustrative only. Based on the present application, those skilled in the art should understand that one aspect described herein can be implemented independently of any other aspect, and two or more of these aspects can be combined in various ways. For example, any number and aspects described herein can be used to implement the device and / or practice the method. In addition, this device and / or this method can be implemented using other structures and / or functions in addition to one or more of the aspects described herein.

[0031] It should also be noted that the drawings provided in the following embodiments only illustrate the basic concept of the present application schematically. The drawings only show the components related to the present application, rather than being drawn according to the number, shape and size of the components in actual implementation. The type, quantity and proportion of each component in its actual implementation can be an arbitrary change, and the component layout type may also be more complex.

[0032] In addition, in the following description, specific details are provided to facilitate a thorough understanding of the examples. However, those skilled in the art will understand that the examples can be practiced without these specific details.

[0033] As Figure 1 and Figure 2 shown, this embodiment provides an integrated device for grinding and spraying heat pipes of a spacecraft, including: a workbench 10, a material loading component 20, a grinding and spraying component 30, and a fixing component 40.

[0034] A first guide frame 101 and a second guide frame 102 are installed on the top of the workbench 10. The first guide frame 101 and the second guide frame 102 are perpendicular to each other. The second guide frame 102 is symmetrically arranged on both sides of the workbench 10, and the first guide frame 101 is erected on the upper end of the second guide frame 102.

[0035] The material loading component 20 includes a material loading top plate 201 and a material loading bottom plate 202. The material loading bottom plate 202 is erected on the upper end of the second guide frame 102. The material loading bottom plate 202 is parallel to the first guide frame 101. The material loading bottom plate 202 can move along the extending direction of the second guide frame 102, and the material loading bottom plate 202 can move closer to or away from the first guide frame 101. The material loading top plate 201 is rotatably arranged above the material loading bottom plate. A plurality of heat pipes 1 of the spacecraft are sequentially fixed on the material loading top plate 201 through the fixing component 40.

[0036] The grinding and spraying component 30 is used for grinding and spraying the heat pipes of the spacecraft. Spraying operation can be carried out immediately after grinding. The grinding treatment removes surface defects and improves the adhesion of the coating. The spraying treatment forms the required thermal control coating. The grinding and spraying component 30 is arranged on the first guide frame 101 and can be translated on the first guide frame 101 manually or driven by a motor. That is, the grinding and spraying component 30 is translated on the first guide frame 101 to different heat pipes 1 of the spacecraft, and continuously grinds and sprays different heat pipes 1. And the grinding and spraying component 30 can move along the extending direction of the second guide frame 102, and the grinding and spraying component 30 moves closer to or away from the heat pipes 1 of the spacecraft.

[0037] As Figure 3As shown, the fixing member 40 includes a first fixing plate unit 401 and a second fixing plate unit 402. The first fixing plate unit 401 includes a plurality of first fixing plates 4011 arranged in parallel on the loading top plate 201. The second fixing plate unit 402 includes a plurality of second fixing plates 4021 arranged in parallel. The plurality of second fixing plates 4021 arranged in parallel are connected as a whole. A first V-shaped block 4012 is arranged on the first fixing plate 4011, and a second V-shaped block 4022 is arranged on the second fixing plate 4021. The first V-shaped block 4012 and the second V-shaped block 4022 cooperate with each other to fix the spacecraft heat pipe 1 between the first V-shaped block 4012 and the second V-shaped block 4022.

[0038] The staff manually place a plurality of spacecraft heat pipes 1 on the first fixing plate unit 401, and the spacecraft heat pipes 1 correspond to the first fixing plates 4011 one by one. The spacecraft heat pipes 1 are embedded in the first V-shaped blocks 4012. Then, the second fixing plate unit 402 and the first fixing plate unit 401 are overlapped and fixed. The plurality of second fixing plates 4021 in the second fixing plate unit 402 correspond to the plurality of first fixing plates 4011 one by one. The first V-shaped block 4012 and the second V-shaped block 4022 cooperate to fix the spacecraft heat pipe 1 between the first V-shaped block 4012 and the second V-shaped block 4022. After the spacecraft heat pipes 1 are fixed and clamped by multiple pairs of first V-shaped blocks 4012 and second V-shaped blocks 4022, a neat row of spacecraft heat pipes 1 is formed.

[0039] The grinding and spraying assembly 30 moves on the first guide frame 101 until the grinding and spraying assembly 30 corresponds to the spacecraft heat pipe 1 at the edge in the neat row of spacecraft heat pipes 1.

[0040] Coarsely adjust the distance between the spacecraft heat pipe 1 and the grinding and spraying assembly 30. The loading bottom plate 202 in the loading assembly 20 approaches the first guide frame 101, that is, the spacecraft heat pipe 1 fixed on the loading top plate 201 approaches the grinding and spraying assembly 30.

[0041] Then finely adjust the distance between the spacecraft heat pipe 1 and the grinding and spraying assembly 30. The grinding and spraying assembly 30 can move along the extension direction of the second guide frame 102, and the grinding and spraying assembly 30 approaches the spacecraft heat pipe 1 again until a part of the grinding and spraying assembly 30 contacts the spacecraft heat pipe 1.

[0042] The grinding and spraying assembly 30 starts to grind the spacecraft heat pipe 1 and then sprays after the grinding is completed.

[0043] After the grinding and spraying of the spacecraft heat pipe 1 are completed, the grinding and spraying assembly moves along the extension direction of the second guide frame 102 and moves away from the spacecraft heat pipe 1. The grinding and spraying assembly 30 moves to the next spacecraft heat pipe 1 until it is aligned with the next spacecraft heat pipe 1, and then the grinding and spraying operations are performed on this spacecraft heat pipe 1.

[0044] Repeat the above operations of moving the grinding and spraying assembly 30 to the next spacecraft heat pipe 1 and performing the grinding and spraying operations until all the spacecraft heat pipes 1 in the whole row facing the grinding and spraying assembly 30 are ground and sprayed.

[0045] The loading base plate 202 in the loading assembly 20 moves away from the first guide frame 101, that is, the spacecraft heat pipe 1 fixed on the loading base plate 201 moves away from the grinding and spraying assembly 30.

[0046] The loading top plate 201 rotates 180° relative to the loading base plate 202, so that the spacecraft heat pipe 1 on the other side that has not been ground and sprayed faces the grinding and spraying assembly 30.

[0047] After the rotation is completed, the grinding and spraying assembly 30 moves on the first guide frame 101 until the grinding and spraying assembly 30 corresponds to the spacecraft heat pipe 1 at the edge in the whole row of spacecraft heat pipes 1.

[0048] Coarsely adjust the distance between the spacecraft heat pipe 1 and the grinding and spraying assembly 30. The loading base plate 202 in the loading assembly 20 moves closer to the first guide frame 101, that is, the spacecraft heat pipe 1 fixed on the loading base plate 201 moves closer to the grinding and spraying assembly 30.

[0049] Then finely adjust the distance between the spacecraft heat pipe 1 and the grinding and spraying assembly 30. The grinding and spraying assembly 30 can move along the extension direction of the second guide frame 102 and moves closer to the spacecraft heat pipe 1 until a part of the grinding and spraying assembly 30 contacts the spacecraft heat pipe 1.

[0050] The grinding and spraying assembly 30 starts to grind the spacecraft heat pipe 1 and performs spraying after the grinding is completed.

[0051] After the grinding and spraying of this spacecraft heat pipe 1 are completed, the grinding and spraying assembly moves along the extension direction of the second guide frame 102 and moves away from the spacecraft heat pipe 1. The grinding and spraying assembly 30 moves to the next spacecraft heat pipe 1 until it is aligned with the next spacecraft heat pipe 1, and then the grinding and spraying operations are performed on this spacecraft heat pipe 1.

[0052] Repeat the above operations of moving the grinding and spraying assembly 30 to the next spacecraft heat pipe 1 and performing the grinding and spraying operations until all the spacecraft heat pipes 1 in the whole row facing the grinding and spraying assembly 30 are ground and sprayed.

[0053] At this time, both side portions of multiple spacecraft heat pipes 1 are polished and sprayed. The second fixing plate unit 402 is removed from the first fixing plate unit 401, and the spacecraft heat pipe 1 is released. Multiple spacecraft heat pipes are removed in sequence, and multiple processed spacecraft heat pipes are obtained at one time.

[0054] In this embodiment, multiple spacecraft heat pipes 1 are fixed on the loading top plate 201 at one time through fixing members, and the operation is simple. After the fixing is completed, the grinding and spraying assembly 30 is moved in the extending direction of the first guide frame 101 so that the grinding and spraying assembly 30 is aligned with the outermost spacecraft heat pipe 1. Then, the loading assembly 20 and the grinding and spraying assembly 30 are moved in sequence along the extending direction of the second guide frame 102 so that the grinding and spraying assembly 30 approaches the spacecraft heat pipe 1. The grinding and spraying assembly 30 grinds and sprays the spacecraft heat pipe 1. Then, the grinding and spraying assembly 30 is moved along the extending direction of the second guide frame 102 so that the grinding and spraying assembly 30 moves away from the spacecraft heat pipe 1. The grinding and spraying assembly 30 is moved in the extending direction of the first guide frame 101 so that the grinding and spraying assembly 30 is aligned with the next spacecraft heat pipe 1 to be processed. The above steps are repeated to grind and spray one side portion of the spacecraft heat pipe 1 in sequence, and multiple spacecraft heat pipes 1 are processed simultaneously, saving time and labor and meeting the requirements of large-scale production.

[0055] The grinding and spraying assembly 30 realizes integrated grinding and spraying processing, reduces the conversion time of the spacecraft heat pipe 1 between the grinding equipment and the spraying equipment, improves the production efficiency, and avoids secondary oxidation or contamination of the polished surface.

[0056] After the processing of one side portion of the spacecraft heat pipe 1 is completed, the loading top plate 201 is rotated so that the other side portion of the spacecraft heat pipe 1 faces the grinding and spraying assembly 30 to realize the grinding and spraying processing of the other side portion, without removing the spacecraft heat pipe 1 for re-fixing, significantly improving the production efficiency and meeting the high-efficiency requirements of large-scale production.

[0057] Such as Figure 3 and Figure 4As shown, in one embodiment, the integrated device for grinding and spraying heat pipes further includes a pressing member 50. The pressing member 50 is used to press the second fixed plate unit 402 onto the first fixed plate unit 401. The pressing member 50 includes a top frame 501, a lifting plate 502, a second screw 503, a knob 504, a limiting rod 505, and a top block 506. The top frame 501 straddles above the fixing member 40, and the two bottom ends of the top frame 501 are respectively fixedly connected to the top surface of the loading top plate 201. The second screw 503 is penetrated through the middle of the top of the top frame 501. The second screw 503 can rotate in the through hole of the top frame 501. The bottom end of the second screw 503 is rotatably connected to the top end of the lifting plate 502. Rotating the second screw 503 can control the lifting of the lifting plate 502. The lifting plate 502 moves up and down in the vertical direction to press or release the second fixed plate unit 402, thereby realizing the pressing or releasing of the spacecraft heat pipe 1. The knob 504 is fixedly connected to the top end of the second screw 503. Rotating the knob 504 can control the rotation of the second screw 503. The limiting rod 505 is penetrated through both sides of the top of the top frame 501. The top block 506 is fixedly arranged at the top end of the limiting rod 505. The top block 506 and the limiting rod 505 cooperate to limit the lifting plate 502 to prevent the spacecraft heat pipe 1 from shifting during the grinding and spraying process.

[0058] As Figure 3 shown, in one embodiment, the second fixed plate unit 402 is fixed to the bottom of the lifting plate 502, and the second fixed plate unit 402 and the lifting plate 502 move together in the vertical direction. After all the spacecraft heat pipes 1 are placed, rotate the knob 504 to drive the second screw 503 to rotate. The lifting plate 502 rotatably connected to the second screw 503 drives the second fixed plate unit 402 to descend together. The second fixed plate unit 402 is fixedly matched with the first unit fixed plate unit 401, and at this time, the lifting plate 502 presses the second fixed plate unit 402, and the fixing and pressing operations of the fixing member 40 are completed synchronously.

[0059] As Figure 5 shown, in one embodiment, side holes 4013 are opened on both side walls of the first V-shaped block 4012. The side holes 4013 are used to enable the first V-shaped block 4012 and the second V-shaped block 4022 to overlap after being combined. The second V-shaped block 4022 can be embedded into the side holes 4013 of the first V-shaped block 4012. When the size of the spacecraft heat pipe 1 is smaller than the space between the first V-shaped block 4012 and the second V-shaped block 4022, the volume of the second V-shaped block 4022 embedded into the side holes 4013 is large, and the spacecraft heat pipe 1 is firmly clamped between the first V-shaped block 4012 and the second V-shaped block 4022. The design of the side holes 4013 enables the first V-shaped block 4012 and the second V-shaped block 4022 to adapt to spacecraft heat pipes 1 with different diameters.

[0060] As Figure 6 andFigure 7 As shown, in one embodiment, the grinding and spraying assembly 30 includes an equipment rack 301, a grinding unit 302, a spraying unit 303, a pushing member 304, a translation member 305, and a first guiding block 306. The equipment rack 301 is used to support and install components such as the grinding unit 302 and the spraying unit 303. The grinding unit 302 is installed at the top of the equipment rack 301. The grinding unit 302 is used to grind the spacecraft heat pipe 1, remove surface defects, and improve the coating adhesion. The spraying unit 303 is installed on one side wall of the equipment rack 301. The spraying unit 303 is used to spray the spacecraft heat pipe 1 that has undergone the grinding operation to form the required thermal control coating. The bottom end of the first guiding block 306 is slidably connected to the first guiding frame 101. When the first guiding block 306 translates on the first guiding frame 101, the equipment rack 301 and the grinding unit 302 and the spraying unit 303 provided on the equipment rack 301 all translate on the first guiding frame 101 in the extending direction of the first guiding frame 101 together with the equipment rack 301. The grinding and spraying assembly 30 can be translated to the corresponding position of the spacecraft heat pipe 1 to be processed as required. The bottom of the equipment rack 301 is slidably connected to the top of the first guiding block 306 along the extending direction of the second guiding frame 102. The equipment rack 301 drives the grinding unit 302 and the spraying unit 303 to approach or move away from the spacecraft heat pipe 1 on the first guiding block 306. The pushing member 304 is used to drive the equipment rack 301 to move along the extending direction of the second guiding frame 102. The translation member 305 is used to drive the equipment rack 301 to move along the extending direction of the first guiding frame 101.

[0061] As Figure 6 shown, in one embodiment, the translation member 305 is provided at the bottom of the equipment rack 301. Specifically, the translation member 305 is provided on the first guiding frame 101. The first guiding frame 101 is composed of two side plates and two slats. The translation member 305 includes a first driving portion 3051 and a first screw 3052. The first driving portion 3051 is installed on one side wall of the first guiding frame 101. The first driving portion 3051 can be a motor. The output shaft of the first driving portion 3051 passes through the side wall surface of the first guiding frame 101 through a bearing movably, and the output portion of the first driving portion 3051 is rotationally connected to one end of the first screw 3052. The first guiding block 306 is slidably connected to the slats. The first driving portion 3051 drives the first screw 3052 to rotate, and the first screw 3052 drives the grinding and spraying assembly 30 to move on the first guiding frame 101, realizing the stable translation of the equipment rack 301 and the grinding unit 302 and the spraying unit 302 installed thereon in the extending direction of the first guiding frame 101, facilitating the processing of spacecraft heat pipes 1 at different positions, and improving the processing efficiency.

[0062] As Figure 6 and Figure 7As shown, in one embodiment, the pusher 304 is disposed at the bottom of the equipment rack 301. The pusher 304 includes a mounting plate 3041, a second driving part 3042, and a fixing frame 3043. The mounting plate 3041 is fixed to one side of the top of the first guiding block 306 for mounting the second driving part 3042. The second driving part 3042 is mounted on one side wall of the mounting plate 3041. The second driving part 3042 can be a cylinder. The fixing frame 3043 is in transmission connection with the output end of the second driving part 3042 and is fixedly connected to the equipment rack 301. The second driving part 3042 drives the fixing frame 3043 to move, and the fixing frame 3043 drives the equipment rack 301 to move together. The equipment rack 301, the grinding unit 302, and the spraying unit 303 move together along the extension direction of the second guiding frame 102 on the first guiding block 306. The second driving part 3042 directly acts on the equipment rack 301 to move, realizing precise movement control of the equipment rack, thereby controlling the grinding unit 302 and the spraying unit 303 to approach or move away from the spacecraft heat pipe, improving the flexibility and automation of the operation.

[0063] As Figure 6 and Figure 7 shown, in one embodiment, the number of the first guiding blocks 306 is multiple. The multiple first guiding blocks 306 correspond to the feet of the equipment rack 301 one by one. A connecting plate 3061 is arranged between the tops of the multiple first guiding blocks 306. The top of the connecting plate 3061 is fixedly connected to the feet at the bottom of the equipment rack 301. The bottom of the connecting plate 3061 is slidably connected to the tops of the first guiding blocks 306 along the extension direction of the second guiding frame 102. The connecting plate 3061 drives the equipment rack 301 to move together, avoiding inconsistent actions of the feet of the equipment rack 301, resulting in tilting and oscillation of the equipment rack 301, providing stable guiding and support for the equipment rack 301, ensuring that the grinding unit 302 and the spraying unit 303 can move smoothly both in the extension direction of the second guiding frame 102 and in the extension direction of the first guiding frame 101, and improving the processing accuracy.

[0064] As Figure 2 and Figure 8 shown, in one embodiment, the loading assembly 20 further includes a moving part 203 and a rotating part 204. The moving part 203 is used to drive the loading assembly 20 to move along the extension direction of the second guiding frame 102. The moving part 203 drives the loading assembly 20 to approach or move away from the grinding and spraying assembly 30. The rotating part 204 is used to drive the loading top plate 201 to rotate relative to the loading bottom plate 202, so that the spacecraft heat pipe 1 fixed on the loading top plate 201 faces the grinding and spraying assembly 30 on the other side. It is not necessary to manually remove the spacecraft heat pipe 1 and then fix it again.

[0065] As Figure 2 and Figure 8As shown, in one embodiment, the moving member 203 includes a third guiding block 2031 and a third driving part. The top of the third guiding block 2031 is fixedly connected to the bottom of the material loading bottom plate 202. The bottom of the third guiding block 2031 is slidably connected to the second guiding frame 102. The movement of the third guiding block 2031 drives the material loading bottom plate 202 to move together on the second guiding frame 102, approaching or moving away from the grinding and spraying assembly 30. The third driving part drives the third guiding block 2031 to move. There is a certain frictional force between the contact surfaces of the third guiding block 2031 and the second guiding frame 102. When the third guiding block 2031 is driven to any position, without applying additional external force to it, it will not move arbitrarily. The cooperative design of the moving member 203 and the second guiding frame 102 provides stable guiding for the material loading bottom plate 202, the material loading top plate 201 thereon, and the fixed spacecraft heat pipe 1, ensuring that the material loading assembly 2 can maintain stability during rotation or movement, and avoiding processing errors caused by shaking.

[0066] As Figure 8 shown, in one embodiment, the rotating member 204 includes a support frame 2041 and a fourth driving part 2042. The support frame 2041 is fixed to the bottom surface of the material loading bottom plate 202 and is used to support the fourth driving part 2042, which is also arranged on the bottom surface of the material loading bottom plate 202 to prevent the fourth driving part 2042 from falling. The fourth driving part 2042 is arranged inside the inner wall of the support frame 2041. The output shaft of the fourth driving part 2042 penetrates through the material loading bottom plate 202 and is in transmission connection with the material loading top plate 201. The fourth driving part 2042 drives the material loading top plate 201 to rotate relative to the material loading bottom plate 202, realizing the rotation control of the spacecraft heat pipe 1 fixed on the material loading top plate 201, facilitating uniform grinding and spraying of each side of the spacecraft heat pipe 1, and improving the processing quality and consistency.

[0067] The above is only the specific implementation manner of the present application, but the protection scope of the present application is not limited thereto. Any changes or substitutions that can be easily thought of by those skilled in the art within the technical scope disclosed in the present application should be covered within the protection scope of the present application. Therefore, the protection scope of the present application should be subject to the protection scope of the claims.

Claims

1. An integrated device for grinding and spraying heat pipes of a spacecraft, characterized in that, Comprising: A workbench, on the top of which a first guide frame and a second guide frame perpendicular to the first guide frame are installed. The second guide frame is symmetrically arranged on both sides of the workbench, and the first guide frame is erected on the upper end of the second guide frame; A material loading component, including a material loading top plate and a material loading bottom plate. The material loading bottom plate is erected on the upper end of the second guide frame and can move along the extending direction of the second guide frame; the material loading top plate is rotatably arranged above the material loading bottom plate, and a plurality of spacecraft heat pipes are sequentially fixed on the material loading top plate through fixing members; A grinding and spraying component, used for grinding and spraying the spacecraft heat pipes; the grinding and spraying component can move along the extending direction of the first guide frame and can also move along the extending direction of the second guide frame; Wherein, the fixing member includes a first fixing plate unit and a second fixing plate unit. The first fixing plate unit includes a plurality of first fixing plates arranged in parallel on the material loading top plate. The second fixing plate unit includes second fixing plates arranged corresponding to the first fixing plates. A first V-shaped block is arranged on the first fixing plate, and a second V-shaped block for cooperating with the first V-shaped block to fix the spacecraft heat pipe is arranged on the second fixing plate.

2. The integrated device for grinding and spraying the heat pipe of a spacecraft according to claim 1, wherein, The heat pipe grinding and spraying integrated device further includes a pressing member, which is used to press the second fixing plate unit onto the first fixing plate unit, and includes: a top frame, a lifting plate, a second screw rod, a knob, a limiting rod and a top block, The top frame is fixedly connected to the material loading top plate; The second screw rod penetrates through the middle of the top of the top frame, and the rotation of the second screw rod controls the lifting of the lifting plate; The top end of the lifting plate is rotatably connected to the bottom end of the second screw rod, and the lifting of the lifting plate presses or releases the spacecraft heat pipe; The knob is fixedly connected to the top end of the second screw rod, and the knob is used to control the rotation of the second screw rod; The limiting rod penetrates through both sides of the top of the top frame, and the top block is fixedly arranged at the top end of the limiting rod. The limiting rod is used to limit the lifting plate.

3. The integrated device for grinding and spraying the heat pipe of a spacecraft according to claim 2, characterized in that, The second fixing plate unit is fixed at the bottom of the lifting plate, and the second fixing plate unit and the lifting plate move together in the vertical direction.

4. The integrated device for grinding and spraying the heat pipe of a spacecraft according to claim 1, characterized in that, Side holes are opened on both side walls of the first V-shaped block, and the side holes are used for the first V-shaped block and the second V-shaped block to overlap after being combined.

5. The integrated device for grinding and spraying the heat pipe of the spacecraft according to claim 1, characterized in that, The grinding and spraying component includes an equipment frame, a grinding unit, a spraying unit, a pushing member, a translation member and a first guide block, The grinding unit is installed at the top end of the equipment frame and is used for grinding the spacecraft heat pipes; The spraying unit is installed on one side wall of the equipment frame and is used for spraying the spacecraft heat pipes; The bottom end of the first guide block is slidably connected to the first guide frame, and the bottom of the equipment frame is slidably connected to the top of the first guide block along the extending direction of the second guide frame; The pushing member is used to drive the equipment frame to move along the extending direction of the second guide frame; The translation member is used to drive the equipment frame to move along the extending direction of the first guide frame.

6. The integrated device for grinding and spraying the heat pipe of a spacecraft according to claim 5, wherein The translation member is provided at the bottom of the equipment rack, and the translation member includes a first driving portion and a first screw rod. The output portion of the first driving portion is rotatably connected to one end of the first screw rod. When the first screw rod rotates, it drives the grinding and spraying assembly to move on the first guiding rack.

7. The integrated device for grinding and spraying the heat pipe of the spacecraft according to claim 5, characterized in that, The pushing member is provided at the bottom of the equipment rack and includes: a mounting plate, a second driving portion, and a fixing frame. The mounting plate is fixed to one side of the top end of the first guiding block. The second driving portion is mounted on one side wall of the mounting plate. The fixing frame is in transmission connection with the output end of the second driving portion and is fixedly connected to the equipment rack.

8. The integrated device for grinding and spraying the heat pipe of the spacecraft according to claim 5, characterized in that A connecting plate is provided between the top ends of the first guiding blocks. The bottom of the connecting plate is slidably connected to the top ends of the first guiding blocks along the extending direction of the second guiding rack. The top of the connecting plate is fixedly connected to the bottom of the equipment rack.

9. The integrated device for grinding and spraying the heat pipe of a spacecraft according to claim 1, characterized in that, The material loading assembly further includes a moving member and a rotating member. The moving member is used to drive the material loading assembly to move along the extending direction of the second guiding rack. The rotating member is used to drive the material loading top plate to rotate relative to the material loading bottom plate.

10. The integrated device for grinding and spraying the heat pipe of a spacecraft according to claim 9, characterized in that, The moving member includes: a third guiding block and a third driving portion. The top of the third guiding block is fixedly connected to the bottom of the material loading bottom plate, and the bottom of the third guiding block is slidably connected to the second guiding rack. The third driving portion is used to drive the third guiding block to move.

11. The integrated device for grinding and spraying heat pipes of a spacecraft according to claim 9, characterized in that, The rotating member includes a support frame and a fourth driving portion. The support frame is fixed to the bottom surface of the material loading bottom plate, and the fourth driving portion is arranged inside the inner wall of the support frame. The output shaft of the fourth driving portion penetrates through the material loading bottom plate and is in transmission connection with the material loading top plate, and is used to drive the material loading top plate to rotate relative to the material loading bottom plate.

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