Process method, device, electronic equipment and medium for copper-water heat pipe for space application
By obtaining the application scenarios of copper water-heat pipes for space application and the external dimensions of heat pipes, determining and controlling the process flow, and preparing and testing copper water-heat pipes for space application, the problem that the existing technology cannot meet the high safety and reliability requirements of copper water-heat pipes for space application is solved, and high-quality copper water-heat pipe production is achieved.
Patent Information
- Application Number
- CN202411925217.3
- Authority / Receiving Office
- CN · China
- Patent Type
- Applications(China)
- Current Assignee / Owner
- Filing Date
- 2024-12-25
- Publication Date
- 2025-04-04
AI Technical Summary
The prior art cannot meet the high safety and reliability requirements of copper hydrothermal pipes used in space, and the process flow of commercial copper hydrothermal pipes on the ground cannot meet the quality standards for space applications.
Provide a process method suitable for space application copper hydrothermal pipes. By obtaining application scenario parameters and heat pipe exterior dimension parameters, determining the production process flow, process parameters and test indicator parameters, controlling the process flow, preparing space application copper hydrothermal pipes, and conducting freeze-thaw and mechanical environment tests, pressure tests and accelerated life tests.
It has achieved the production of high-quality copper hydrothermal pipes that meet the space application scenarios, meeting the high requirements for safety and reliability in space applications.
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Figure CN119756038A_ABST
Abstract
Description
Technical Field
[0001] The present invention relates to the field of copper-water heat pipes for space applications, and in particular to a process method, a device, electronic equipment and a medium for copper-water heat pipes for space applications. Background Art
[0002] Copper-water heat pipes for space applications are heat pipes used in spacecraft. They use copper as the wick material and water as the working fluid to transfer heat through evaporation and condensation processes. Copper-water heat pipes for space applications require high safety and reliability and require more stringent processes. The current process flow for copper-water heat pipes is based on ground-based commercial copper-water heat pipes, and the process flow for ground-based commercial copper-water heat pipes cannot meet the quality requirements for copper-water heat pipes for space applications.
[0003] Therefore, there is an urgent need for a process method for copper-water heat pipes suitable for space applications. Summary of the invention
[0004] In view of this, the purpose of this application is to provide a process method, device, electronic equipment and medium for copper-water heat pipes for space applications, so as to produce heat pipes that meet the application scenarios of copper-water heat pipes for space applications.
[0005] In a first aspect, an embodiment of the present application provides a process method for a copper-water heat pipe for space application, the method comprising:
[0006] Obtaining a manufacturing process flow, manufacturing process parameters and test index parameters determined based on application scenario parameters of space application copper-water heat pipes and heat pipe shape and size parameters; the manufacturing process parameters are used to control the manufacturing process flow;
[0007] Manufacturing a copper-water heat pipe for space application according to the manufacturing process and the manufacturing process parameters;
[0008] Based on the test index parameters, the manufactured space-application copper-water heat pipe is tested to obtain the target space-application copper-water heat pipe.
[0009] In a possible implementation manner, the manufacturing process parameters include one or more of sintering process parameters, degassing process parameters, and filling medium process parameters.
[0010] In a possible implementation, the sintering process parameters include copper powder size, weight ratio of copper powders of different copper powder sizes, and wick parameters; manufacturing a copper-water heat pipe for space application according to the manufacturing process and the manufacturing process parameters includes:
[0011] If the current manufacturing process is a sintering process in the manufacturing process flow, the dried and cleaned center rod is inserted into the copper tube to be sintered;
[0012] Mixing copper powders of various copper powder sizes according to the weight ratio;
[0013] Filling the mixed copper powder into the copper tube after the central rod is inserted;
[0014] Inserting the copper tube filled with copper powder into the graphite carrier; locking the bell jar and the graphite carrier tightly to keep airtightness and then pushing it into the sintering furnace, sintering the copper tube filled with copper powder according to the sintering program corresponding to the wick parameters;
[0015] After sintering is completed, the bell jar is pushed to the cooling zone for cooling, and the center rod in the cooled copper tube is pulled out and placed in the material box.
[0016] In a possible implementation manner, the testing of the manufactured space application copper water heat pipe based on the test index parameters includes:
[0017] Based on the test index parameters, one or more tests of freeze-thaw and mechanical environment tests, pressure tests and accelerated life tests are performed on the manufactured copper-water heat pipes for space applications.
[0018] In a possible implementation, the test process of freeze-thaw and mechanical environment test includes:
[0019] The space application copper-water heat pipe is subjected to leak detection, heat transfer performance test, startup performance test, anti-gravity height test, first static freeze-thaw cycle test, leak detection, heat transfer performance test, startup performance test, anti-gravity height test, and first working freeze-thaw cycle test in sequence;
[0020] The space application copper-water heat pipe is subjected to leak detection, heat transfer performance test, startup performance test, anti-gravity height test, second static freeze-thaw cycle test, leak detection, heat transfer performance test, startup performance test, anti-gravity height test, and second working freeze-thaw cycle test in sequence;
[0021] The space application copper-water heat pipe is subjected to leak detection, heat transfer performance test, startup performance test, anti-gravity height test, sinusoidal vibration test, random vibration test, impact test, acceleration test, leak detection, heat transfer performance test, startup performance test, and anti-gravity height test in sequence.
[0022] In a possible implementation, the test process of the pressure test includes:
[0023] The space-application copper-water heat pipe is subjected to a first appearance inspection, a yield strength test, a second appearance inspection, a bursting pressure test and a third appearance inspection in sequence.
[0024] In a possible implementation, the test process of the accelerated life test includes:
[0025] The space application copper-water heat pipe is subjected to a heat transfer performance test, a startup performance test, an anti-gravity height test, an accelerated life test, a heat transfer performance test, a startup performance test and an anti-gravity high-speed test in sequence.
[0026] In a second aspect, the present application also provides a process device for a space application copper-water heat pipe, the device comprising:
[0027] An acquisition module, used to acquire a manufacturing process flow, manufacturing process parameters and test index parameters determined based on application scenario parameters of the space application copper-water heat pipe and the heat pipe external dimension parameters; the manufacturing process parameters are used to control the manufacturing process flow;
[0028] A manufacturing module, used for manufacturing a copper-water heat pipe for space application according to the manufacturing process and the manufacturing process parameters;
[0029] The test module is used to test the manufactured space-application copper-water heat pipe based on the test index parameters to obtain the target space-application copper-water heat pipe.
[0030] In the third aspect, an embodiment of the present application also provides an electronic device, comprising: a processor, a storage medium and a bus, wherein the storage medium stores machine-readable instructions executable by the processor, and when the electronic device is running, the processor communicates with the storage medium through the bus, and the processor executes the machine-readable instructions to perform the steps of the process method for space application copper-water heat pipes as described in any one of the first aspects.
[0031] In a fourth aspect, an embodiment of the present application further provides a computer-readable storage medium, on which a computer program is stored. When the computer program is executed by a processor, the steps of the process method for space application of copper-water heat pipes as described in any one of the first aspects are executed.
[0032] The embodiment of the present application provides a process method, device, electronic device and medium for copper-water heat pipes for space applications, the method comprising: obtaining a manufacturing process flow, manufacturing process parameters and test index parameters determined based on application scenario parameters of copper-water heat pipes for space applications and heat pipe external dimension parameters; the manufacturing process parameters are used to control the manufacturing process flow; manufacturing copper-water heat pipes for space applications according to the manufacturing process flow and the manufacturing process parameters; testing the manufactured copper-water heat pipes for space applications based on the test index parameters to obtain target copper-water heat pipes for space applications. Through the method of the present application, heat pipes that meet the application scenarios of copper-water heat pipes for space applications can be manufactured. BRIEF DESCRIPTION OF THE DRAWINGS
[0033] In order to more clearly illustrate the technical solutions of the embodiments of the present application, the drawings required for use in the embodiments will be briefly introduced below. It should be understood that the following drawings only show certain embodiments of the present application and therefore should not be regarded as limiting the scope. For ordinary technicians in this field, other related drawings can be obtained based on these drawings without paying creative work.
[0034] Figure 1 A flow chart showing a process method for a space application copper-water heat pipe provided in an embodiment of the present application is shown;
[0035] Figure 2 A flow chart showing another process method for a space application copper-water heat pipe provided in an embodiment of the present application is shown;
[0036] Figure 3 A schematic structural diagram of a process device for a space-application copper-water heat pipe provided in an embodiment of the present application is shown;
[0037] Figure 4 A schematic structural diagram of an electronic device provided in an embodiment of the present application is shown. DETAILED DESCRIPTION
[0038] To make the purpose, technical scheme and advantages of the embodiments of the present application clearer, the technical scheme in the embodiments of the present application will be clearly and completely described below in conjunction with the drawings in the embodiments of the present application. It should be understood that the drawings in the present application only serve the purpose of explanation and description and are not used to limit the scope of protection of the present application. In addition, it should be understood that the schematic drawings are not drawn in real proportion. The flowchart used in this application shows the operations implemented according to some embodiments of the present application. It should be understood that the operations of the flowchart can be implemented out of sequence, and the steps without logical context can be reversed in order or implemented simultaneously. In addition, those skilled in the art can add one or more other operations to the flowchart under the guidance of the content of the present application, or remove one or more operations from the flowchart.
[0039] In addition, the described embodiments are only a part of the embodiments of the present application, rather than all the embodiments. The components of the embodiments of the present application described and shown in the drawings here can be arranged and designed in various configurations. Therefore, the following detailed description of the embodiments of the present application provided in the drawings is not intended to limit the scope of the application claimed for protection, but merely represents the selected embodiments of the present application. Based on the embodiments of the present application, all other embodiments obtained by those skilled in the art without making creative work belong to the scope of protection of the present application.
[0040] In order to enable those skilled in the art to use the content of this application, the following implementation is given in conjunction with the specific application scenario "the field of copper-water heat pipes for space applications". For those skilled in the art, the general principles defined here can be applied to other embodiments and application scenarios without departing from the spirit and scope of this application. Although this application is mainly described around the "field of copper-water heat pipes for space applications", it should be understood that this is only an exemplary embodiment.
[0041] It should be noted that the term "comprising" will be used in the embodiments of the present application to indicate the existence of the features declared thereafter, but does not exclude the addition of other features.
[0042] The following is a detailed description of a process method for a space application copper-water heat pipe provided in an embodiment of the present application.
[0043] Reference Figure 1 As shown, it is a schematic diagram of a process method of a space application copper-water heat pipe provided by an embodiment of the present application. The exemplary steps of the embodiment of the present application are described below:
[0044] S101, obtaining a manufacturing process flow, manufacturing process parameters and test index parameters determined based on application scenario parameters of the copper-water heat pipe for space applications and outer dimension parameters of the heat pipe.
[0045] In the implementation mode of the present application, the application scenario parameters are used to characterize the working environment of the copper-water heat pipe for space application to be manufactured; taking the application scenario as an aircraft, the application scenario parameters may include the orbit altitude (such as 500km to 36,000km), the launch vibration environment, the heat transfer working temperature (30℃ to 90℃), the orbit storage temperature (such as -40℃ to +90℃), the ground environment of the application scenario (humidity, mold, salt spray, etc.), the use space position (inside or outside the satellite cabin), etc. The heat pipe external dimensions are used to describe the shape (round tube, flattened tube, bent tube, etc.) and size (heat pipe diameter, heat pipe length, heat pipe flattening thickness, heat pipe bending radius, etc.) of the copper-water heat pipe for space application to be manufactured. The test index parameters refer to the performance parameters that the space application copper water heat pipe to be manufactured needs to achieve, which may include the corresponding index parameters of heat transfer performance (such as the maximum heat transfer capacity Qmax ≥ 40W of a 5mm diameter round tube, Qmax ≥ 16W of a 5mm diameter flattened tube; Qmax ≥ 50W of a 6mm diameter round tube, Qmax ≥ 32W of a 6mm diameter flattened tube; Qmax ≥ 65W of a 8mm diameter round tube, Qmax ≥ 38W of a 8mm diameter flattened tube), the corresponding index parameters of anti-gravity operation capability (such as hydraulic climbing height not less than 250mm), static freeze-thaw cycle Corresponding index parameters (such as meeting the index requirements that the heat transfer performance change is less than 10% after 1000 cycles and there is no obvious change in appearance), corresponding index parameters for working freeze-thaw cycles (such as meeting the index requirements that the heat transfer performance change is less than 10% after 1000 cycles and there is no obvious change in appearance), corresponding index parameters for startup performance (such as meeting the first-level derating requirements for the controlled chip temperature, the maximum working section temperature ≤85℃), corresponding index parameters for accelerated life (such as not less than 7 years), corresponding index parameters for burst strength (such as meeting the requirement that the burst pressure is greater than or equal to 2 times the maximum working pressure), corresponding index parameters for sinusoidal vibration and corresponding index parameters for random vibration, etc.
[0046] Among them, the manufacturing process parameters are used to control the manufacturing process flow so that the manufactured copper-water heat pipe for space applications can work under the application scenario corresponding to the application scenario parameters, and meet the requirements of the heat pipe external dimension parameters and the test index parameters; the manufacturing process parameters include one or more of the sintering process parameters, the degassing process parameters and the filling working fluid process parameters.
[0047] S102, manufacturing a space application copper water heat pipe according to the manufacturing process and manufacturing process parameters.
[0048] In the implementation manner of the present application, the manufacturing process includes, in sequence, an incoming material inspection process, a tube cutting process, a cleaning and drying process, a necking process, a sintering process, a correction process, a sealing process (large mouth), an inspection process, an annealing process, a degassing process, a filling process, a sealing process (small mouth), a molding process, a temperature resistance test process, a quality loss process, a thermal performance test process, an environmental test process, a thermal performance retest process, and a final inspection process.
[0049] Incoming material inspection process: After the purchased copper tube arrives, use a vernier caliper to check whether the diameter of the copper tube (i.e. the heat pipe diameter) and the wall thickness of the copper tube (i.e. the heat pipe thickness) meet the requirements; check whether the composition of the copper tube meets the corresponding requirements; use instruments to test the purity of water to see whether it meets the corresponding requirements.
[0050] Tube cutting process: When starting the tube cutting machine, first check whether the process parameters meet the requirements, adjust the tube cutting machine equipment, select the copper tube according to the outer size parameters of the heat pipe, fill the V-groove of the tube cutting machine, align the cut tube end slightly, and open the tube cutting machine to cut the tube.
[0051] Cleaning and drying process: After cutting, the copper tube is washed with acid and alkali to remove the residual milling fluid and other impurities on the heat pipe. After cleaning, put it into the drying box, bake it for half an hour, and take it out after drying.
[0052] Shrinking process: After adjusting the shrinking machine equipment, put the cleaned and dried copper tube into the hopper; turn on the power switch of the operation panel, set the corresponding shrinking parameters and shrink the copper tube to be shrunken; check whether the length of the heat pipe after shrinking meets the outer dimensions of the heat pipe; if yes, proceed to the next process.
[0053] Sintering process: sintering process parameters include copper powder size, weight ratio between copper powders of each copper powder size, and wick parameters; then a copper-water heat pipe for space application is manufactured according to the manufacturing process flow and the manufacturing process parameters, including: if the current manufacturing process is the sintering process in the manufacturing process flow, the center rod after drying and cleaning is inserted into the copper tube to be sintered; the copper powders of each copper powder size are mixed according to the weight ratio; the mixed copper powder is filled into the copper tube after the center rod is inserted; the copper tube filled with copper powder is inserted into the graphite carrier; and the bell jar and the graphite carrier are locked to keep airtight and then pushed into the sintering furnace, and the copper tube filled with copper powder is sintered according to the sintering procedure corresponding to the wick parameters (such as wick thickness, wick porosity, wick permeability, wick pore size, etc.) so that the sintered copper tube meets the requirements of the wick parameters; after sintering, the bell jar is pushed to the cooling zone for cooling, and the center rod in the cooled copper tube is pulled out and placed in the material box.
[0054] Correction process: If the outer diameter of the copper tube to be corrected meets the external dimensions of the heat pipe, adjust the interval of the straightening machine and place the copper tube to be corrected on the straightening machine for straightening; check the flatness of the tube-rolling splint to see if there are any impurities remaining; if no impurities are left, place the straightened copper tube on the tube-rolling splint for tube-rolling correction; if there are impurities, after removing the impurities, place the straightened copper tube on the tube-rolling splint for tube-rolling correction.
[0055] Sealing process (large mouth): After adjusting the sealing machine equipment, install the corresponding sealing mold; place the shrinking section of the copper tube to be sealed on the pusher with the shrinking mold facing the shrinking mold; open the sealing machine equipment to shrink the mouth, and after the shrinking is completed, use the spot welder to weld and seal.
[0056] Leak detection process: Check whether there is any leakage in the heat pipe after welding and sealing; if there is any leakage, re-weld it; if there is no leakage, proceed to the next process.
[0057] Annealing process: The annealing process can reduce the hardness of the material due to work hardening, making the heat pipe material easier to process and form.
[0058] Degassing process: After adjusting the degassing machine equipment, turn on the power switch, vacuum pump switch and oil pressure switch in sequence; make the vacuum gauge below 0.1pa, set the heat pipe degassing time and vacuum degree, and then start degassing the copper pipe to be degassed. Specifically, the degassing process parameters include degassing temperature, degassing vacuum degree, flushing pressure and replacement times; according to the manufacturing process flow and the manufacturing process parameters, the copper-water heat pipe for space application is manufactured, including: if the current manufacturing process is the degassing process in the manufacturing process flow, the copper pipe to be degassed will be heated and degassed according to the degassing temperature; the copper pipe to be degassed will be degassed at a reduced pressure according to the degassing vacuum degree; the copper pipe to be degassed will be replaced and degassed according to the flushing pressure and replacement times.
[0059] Here, temperature increase degassing: by increasing the temperature, the non-condensable gas contained in and adsorbed inside the metal and porous materials is removed. Pressure reduction degassing: by reducing the pressure, the non-condensable gas contained in and adsorbed inside the metal and porous materials is removed. Displacement degassing: by flushing and replacing with a working fluid, the non-condensable gas contained in and adsorbed inside the metal and porous materials is removed. The present application adopts a process method combining the above three methods for degassing. After the degassing process test, the composition of the working fluid after degassing is detected to obtain the optimized process parameters. Then, according to the optimized process parameters, the copper-water heat pipe product is developed, and an accelerated life test is carried out to determine whether the process parameters can meet the requirements of product performance, life and reliability. Finally, the process flow and process parameters are confirmed and solidified.
[0060] Filling working fluid process: First check whether the process filling working fluid parameters meet the requirements. Use a caliper to measure the outer diameter and length of the copper tube to be filled with the working fluid, and check whether the copper tube to be filled with the working fluid meets the external dimensions of the heat pipe; if it does, determine whether there is any blockage at the injection port, and confirm that the injection tube is not deformed before starting the filling. Specifically, the filling working fluid process parameters include the opening adjustment range of the flow meter regulating valve, the flow meter adjustment accuracy, the pipeline length, the pipe diameter, the relationship between the mass change value and the opening range; the space application copper-water heat pipe is manufactured according to the manufacturing process and the manufacturing process parameters, including: if the current manufacturing process is the filling working fluid process in the manufacturing process, the working fluid to be filled in the heat pipe is charged according to the opening adjustment range of the flow meter regulating valve, the flow meter adjustment accuracy, the pipeline length, the pipe diameter, the relationship between the mass change value and the opening range.
[0061] In the implementation manner of the present application, a flow meter corresponding to the flow meter adjustment accuracy is used to measure the filling flow, and the opening of the flow meter regulating valve is adjusted based on the opening adjustment range of the flow meter regulating valve to ensure that the flow during the filling process is controllable and accurately measured.
[0062] Sealing process (small mouth): Place the heat pipe filled with working fluid on the automatic welding machine, set the parameters of the sealing machine, and then weld and seal it.
[0063] Forming process: the straight tubes after the sealing process (small mouth) are classified, the bent tubes are bent with an automatic bending machine, and the flat tubes are flattened and formed with corresponding molds.
[0064] Temperature resistance process: The welded heat pipe is subjected to a temperature resistance test to check whether there is any leakage during the welding of the heat pipe.
[0065] Quality damage process: Use a high-precision electronic scale to measure the heat pipe and check whether it has leakage.
[0066] Thermal performance testing process: Adjust the machine equipment, conduct temperature difference and power tests on the formed heat pipes, and detect heat pipes with poor performance.
[0067] Environmental testing process: For heat pipes that pass the performance test, wet heat and chemical resistance tests are carried out to detect whether the performance of the heat pipes meets the requirements under specific conditions.
[0068] Thermal performance retest process: After the environmental test of the heat pipe is completed, the temperature difference and power are retested to ensure the performance of the heat pipe is good.
[0069] Final inspection process: inspect the appearance and size of the inspected heat pipes, and pack and ship them out if there are no problems.
[0070] Here, the present application strictly controls each process through sintering process parameters, degassing process parameters and filling working fluid process parameters, so that the manufactured copper-water heat pipe for space applications meets the corresponding index parameters of heat transfer performance, the corresponding index parameters of anti-gravity operation capability, the corresponding index parameters of static freeze-thaw cycle, the corresponding index parameters of working freeze-thaw cycle, the corresponding index parameters of starting performance, the corresponding index parameters of accelerated life, the corresponding index parameters of blasting strength, the corresponding index parameters of sinusoidal vibration and the corresponding index parameters of random vibration, etc.
[0071] S103. Test the manufactured space-application copper-water heat pipe based on the test index parameters to obtain the target space-application copper-water heat pipe.
[0072] In the implementation manner of the present application, one or more tests of freeze-thaw and mechanical environment test, pressure test and accelerated life test are performed on the manufactured copper-water heat pipe for space application based on the test index parameters; and the copper-water heat pipe for space application that passes the test is determined as the target copper-water heat pipe for space application.
[0073] Here, since the working environment of copper-water heat pipes for space applications is more extreme, it is necessary to conduct one or more tests of freeze-thaw and mechanical environment tests, pressure tests and accelerated life tests on the copper-water heat pipes for space applications to ensure the quality of the copper-water heat pipes for space applications.
[0074] Specifically, the test process of freeze-thaw and mechanical environment test includes: leak detection, heat transfer performance test, start-up performance test, anti-gravity height test, first static freeze-thaw cycle test, leak detection, heat transfer performance test, start-up performance test, anti-gravity height test, first working freeze-thaw cycle test for copper-water heat pipes for space application; leak detection, heat transfer performance test, start-up performance test, anti-gravity height test, second static freeze-thaw cycle test, leak detection, heat transfer performance test, start-up performance test, anti-gravity height test, second working freeze-thaw cycle test for copper-water heat pipes for space application; leak detection, heat transfer performance test, start-up performance test, anti-gravity height test, sinusoidal vibration test, random vibration test, impact test, acceleration test, leak detection, heat transfer performance test, start-up performance test, anti-gravity height test for copper-water heat pipes for space application.
[0075] Specifically, the test process of the pressure test includes: conducting the first appearance inspection, yield strength test, second appearance inspection, bursting pressure test and third appearance inspection on the space application copper-water heat pipe in sequence.
[0076] Specifically, the test process of the accelerated life test includes: conducting heat transfer performance test, startup performance test, anti-gravity height test, accelerated life test, heat transfer performance test, startup performance test and anti-gravity high-speed test on the copper-water heat pipe for space application in sequence.
[0077] Here, temperature is selected as the acceleration factor, and 80°C high temperature aging is used for accelerated life testing.
[0078] The embodiment of the present application provides a process method for a copper-water heat pipe for space application, the method comprising: obtaining a manufacturing process flow, manufacturing process parameters and test index parameters determined based on application scenario parameters of the copper-water heat pipe for space application and the outer dimension parameters of the heat pipe; the manufacturing process parameters are used to control the manufacturing process flow; manufacturing the copper-water heat pipe for space application according to the manufacturing process flow and the manufacturing process parameters; testing the manufactured copper-water heat pipe for space application based on the test index parameters to obtain a target copper-water heat pipe for space application. Through the method of the present application, a heat pipe that meets the application scenario of the copper-water heat pipe for space application can be manufactured.
[0079] Reference Figure 2 As shown, it is a schematic diagram of a process method of another space application copper-water heat pipe provided in an embodiment of the present application. The exemplary steps of the embodiment of the present application are described below:
[0080] S201, inserting the dried and cleaned center rod into the copper tube to be sintered.
[0081] S202, mixing copper powders of different copper powder sizes according to a weight ratio.
[0082] S203, filling the mixed copper powder into the copper tube after the center rod is inserted.
[0083] S204, inserting the copper tube filled with copper powder into the graphite carrier; locking the bell jar and the graphite carrier to keep airtightness and then pushing it into the sintering furnace, and sintering the copper tube filled with copper powder according to the sintering program corresponding to the wick parameters.
[0084] S205, after sintering is completed, push the bell jar to the cooling zone for cooling, pull out the center rod in the cooled copper tube and put it into the material box.
[0085] An embodiment of the present application provides another process method for copper-water heat pipes for space applications. The method performs high-quality sintering on the sintering process through sintering process parameters to produce heat pipes that meet the application scenarios of copper-water heat pipes for space applications.
[0086] With the same inventive concept, an embodiment of the present application also provides a process device for copper-water heat pipes for space applications that corresponds to the process method for copper-water heat pipes for space applications. Since the principle of solving the problem by the device in the embodiment of the present application is similar to the process method for copper-water heat pipes for space applications mentioned above in the embodiment of the present application, the implementation of the device can refer to the implementation of the method, and the repeated parts will not be repeated.
[0087] Reference Figure 3FIG. 1 is a schematic diagram of a process device for a space-based copper-water heat pipe provided in an embodiment of the present application. The process device for a space-based copper-water heat pipe includes:
[0088] An acquisition module 301 is used to acquire a manufacturing process flow, manufacturing process parameters and test index parameters determined based on application scenario parameters of the space application copper-water heat pipe and heat pipe shape dimension parameters; the manufacturing process parameters are used to control the manufacturing process flow;
[0089] A manufacturing module 302, for manufacturing a copper-water heat pipe for space application according to the manufacturing process and the manufacturing process parameters;
[0090] The test module 303 is used to test the manufactured space-application copper-water heat pipe based on the test index parameters to obtain the target space-application copper-water heat pipe.
[0091] In a possible implementation manner, the manufacturing process parameters include one or more of sintering process parameters, degassing process parameters, and filling medium process parameters.
[0092] In one possible embodiment, the sintering process parameters include copper powder size, weight ratio between copper powders of each copper powder size, and wick parameters; the manufacturing module 302 is specifically used for inserting the dried and cleaned center rod into the copper tube to be sintered if the current manufacturing process is a sintering process in the manufacturing process flow; mixing copper powders of each copper powder size according to the weight ratio; filling the mixed copper powder into the copper tube after the center rod is inserted; inserting the copper tube filled with copper powder into a graphite carrier; and locking the bell jar and the graphite carrier to keep airtight and then pushing it into a sintering furnace, and sintering the copper tube filled with copper powder according to the sintering procedure corresponding to the wick parameters; after sintering, pushing the bell jar to the cooling zone for cooling, pulling out the center rod from the cooled copper tube and putting it into a material box.
[0093] In a possible implementation, the test module 303 is specifically used to perform one or more tests of freeze-thaw and mechanical environment tests, pressure tests, and accelerated life tests on the manufactured copper-water heat pipes for space applications based on the test index parameters.
[0094] In a possible implementation, the test process of freeze-thaw and mechanical environment test includes:
[0095] The space application copper-water heat pipe is subjected to leak detection, heat transfer performance test, startup performance test, anti-gravity height test, first static freeze-thaw cycle test, leak detection, heat transfer performance test, startup performance test, anti-gravity height test, and first working freeze-thaw cycle test in sequence;
[0096] The space application copper-water heat pipe is subjected to leak detection, heat transfer performance test, startup performance test, anti-gravity height test, second static freeze-thaw cycle test, leak detection, heat transfer performance test, startup performance test, anti-gravity height test, and second working freeze-thaw cycle test in sequence;
[0097] The space application copper-water heat pipe is subjected to leak detection, heat transfer performance test, startup performance test, anti-gravity height test, sinusoidal vibration test, random vibration test, impact test, acceleration test, leak detection, heat transfer performance test, startup performance test, and anti-gravity height test in sequence.
[0098] In a possible implementation, the test process of the pressure test includes:
[0099] The space-application copper-water heat pipe is subjected to a first appearance inspection, a yield strength test, a second appearance inspection, a bursting pressure test and a third appearance inspection in sequence.
[0100] In a possible implementation, the test process of the accelerated life test includes:
[0101] The space application copper-water heat pipe is subjected to a heat transfer performance test, a startup performance test, an anti-gravity height test, an accelerated life test, a heat transfer performance test, a startup performance test and an anti-gravity high-speed test in sequence.
[0102] The embodiment of the present application provides a process device for copper-water heat pipes for space applications, the device comprising: an acquisition module 301, used to obtain a manufacturing process flow, manufacturing process parameters and test index parameters determined based on application scenario parameters of copper-water heat pipes for space applications and heat pipe external dimension parameters; the manufacturing process parameters are used to control the manufacturing process flow; a manufacturing module 302, used to manufacture copper-water heat pipes for space applications according to the manufacturing process flow and the manufacturing process parameters; a test module 303, used to test the manufactured copper-water heat pipes for space applications based on the test index parameters to obtain target copper-water heat pipes for space applications. Through this application, heat pipes that meet the application scenarios of copper-water heat pipes for space applications can be manufactured.
[0103] like Figure 4 As shown, an electronic device 400 provided in an embodiment of the present application includes: a processor 401, a memory 402 and a bus, wherein the memory 402 stores machine-readable instructions executable by the processor 401. When the electronic device is running, the processor 401 communicates with the memory 402 through the bus, and the processor 401 executes the machine-readable instructions to perform the steps of the process method for space application of copper-water heat pipes as described above.
[0104] Specifically, the above-mentioned memory 402 and processor 401 can be general-purpose memories and processors, which are not specifically limited here. When the processor 401 runs the computer program stored in the memory 402, it can execute the above-mentioned process method for space application copper-water heat pipes.
[0105] Corresponding to the above-mentioned process method for applying copper-water heat pipes in space, an embodiment of the present application also provides a computer-readable storage medium, on which a computer program is stored. When the computer program is executed by a processor, the steps of the above-mentioned process method for applying copper-water heat pipes in space are executed.
[0106] Those skilled in the art can clearly understand that, for the convenience and simplicity of description, the specific working process of the system and device described above can refer to the corresponding process in the method embodiment, and will not be repeated in this application. In the several embodiments provided in this application, it should be understood that the disclosed system, device and method can be implemented in other ways. The device embodiments described above are merely schematic. For example, the division of the modules is only a logical function division. There may be other division methods in actual implementation. For example, multiple modules or components can be combined or integrated into another system, or some features can be ignored or not executed. Another point is that the mutual coupling or direct coupling or communication connection shown or discussed can be through some communication interfaces, indirect coupling or communication connection of devices or modules, which can be electrical, mechanical or other forms.
[0107] The modules described as separate components may or may not be physically separated, and the components shown as modules may or may not be physical units, that is, they may be located in one place or distributed on multiple network units. Some or all of the units may be selected according to actual needs to achieve the purpose of the solution of this embodiment.
[0108] In addition, each functional unit in each embodiment of the present application may be integrated into one processing unit, or each unit may exist physically separately, or two or more units may be integrated into one unit.
[0109] If the functions are implemented in the form of software functional units and sold or used as independent products, they can be stored in a non-volatile computer-readable storage medium that is executable by a processor. Based on this understanding, the technical solution of the present application, or the part that contributes to the prior art or the part of the technical solution, can be embodied in the form of a software product, which is stored in a storage medium and includes several instructions for a computer device (which can be a personal computer, server, or network device, etc.) to perform all or part of the steps of the information processing method described in each embodiment of the present application. The aforementioned storage medium includes: various media that can store program codes, such as USB flash drives, mobile hard drives, ROM, RAM, magnetic disks, or optical disks.
[0110] The above are only specific implementations of the present application, but the protection scope of the present application is not limited thereto. Any technician familiar with the technical field can easily think of changes or substitutions within the technical scope disclosed in the present application, which should be included in the protection scope of the present application. Therefore, the protection scope of the present application should be based on the protection scope of the claims.
Claims
1. A process for making copper-water heat pipes for space applications, characterized in that: The method comprises: Obtaining a manufacturing process flow, manufacturing process parameters and test index parameters determined based on application scenario parameters of space application copper-water heat pipes and heat pipe shape and size parameters; the manufacturing process parameters are used to control the manufacturing process flow; Manufacturing a copper-water heat pipe for space application according to the manufacturing process and the manufacturing process parameters; Based on the test index parameters, the manufactured space-application copper-water heat pipe is tested to obtain the target space-application copper-water heat pipe.
2. The process for producing a copper-water heat pipe for space application according to claim 1, characterized in that: The manufacturing process parameters include one or more of sintering process parameters, degassing process parameters and filling medium process parameters.
3. The process for producing a copper-water heat pipe for space application according to claim 2, characterized in that: The sintering process parameters include copper powder size, weight ratio of copper powders of different copper powder sizes, and wick parameters; Manufacturing a copper-water heat pipe for space application according to the manufacturing process and the manufacturing process parameters includes: If the current manufacturing process is a sintering process in the manufacturing process flow, the dried and cleaned center rod is inserted into the copper tube to be sintered; Mixing copper powders of various copper powder sizes according to the weight ratio; Fill the mixed copper powder into the copper tube after inserting the center rod; Inserting the copper tube filled with copper powder into the graphite carrier; locking the bell jar and the graphite carrier tightly to keep airtightness and then pushing it into the sintering furnace, sintering the copper tube filled with copper powder according to the sintering program corresponding to the wick parameters; After sintering is completed, the bell jar is pushed to the cooling zone for cooling, and the center rod in the cooled copper tube is pulled out and placed in the material box.
4. The process for producing a copper-water heat pipe for space application according to any one of claims 1 to 3, characterized in that: The test process of freeze-thaw and mechanical environmental testing includes: The space application copper-water heat pipe is subjected to leak detection, heat transfer performance test, startup performance test, anti-gravity height test, first static freeze-thaw cycle test, leak detection, heat transfer performance test, startup performance test, anti-gravity height test, and first working freeze-thaw cycle test in sequence; The space application copper-water heat pipe is subjected to leak detection, heat transfer performance test, startup performance test, anti-gravity height test, second static freeze-thaw cycle test, leak detection, heat transfer performance test, startup performance test, anti-gravity height test, and second working freeze-thaw cycle test in sequence; The space application copper-water heat pipe is subjected to leak detection, heat transfer performance test, startup performance test, anti-gravity height test, sinusoidal vibration test, random vibration test, impact test, acceleration test, leak detection, heat transfer performance test, startup performance test, and anti-gravity height test in sequence.
5. The process for producing a copper-water heat pipe according to claim 4, characterized in that: The test process of pressure test includes: The space-application copper-water heat pipe is subjected to a first appearance inspection, a yield strength test, a second appearance inspection, a bursting pressure test and a third appearance inspection in sequence.
6. The process for producing a copper-water heat pipe according to claim 5, characterized in that: The test process of accelerated life test includes: The space application copper-water heat pipe is subjected to a heat transfer performance test, a startup performance test, an anti-gravity height test, an accelerated life test, a heat transfer performance test, a startup performance test and an anti-gravity high-speed test in sequence.
7. A process device for space application of copper-water heat pipe, characterized in that: The device comprises: An acquisition module is used to acquire a manufacturing process flow, manufacturing process parameters and test index parameters determined based on application scenario parameters of the space application copper-water heat pipe and the outer dimension parameters of the heat pipe; the manufacturing process parameters are used to control the manufacturing process flow; A manufacturing module, used for manufacturing a copper-water heat pipe for space application according to the manufacturing process and the manufacturing process parameters; The test module is used to test the manufactured space-application copper-water heat pipe based on the test index parameters to obtain the target space-application copper-water heat pipe.
8. The process device for the space application copper-water heat pipe according to claim 7, characterized in that: The manufacturing process parameters include one or more of sintering process parameters, degassing process parameters and filling medium process parameters.
9. An electronic device, characterized in that: include: A processor, a storage medium and a bus, wherein the storage medium stores machine-readable instructions executable by the processor, and when the electronic device is running, the processor communicates with the storage medium through the bus, and the processor executes the machine-readable instructions to perform the steps of the process method for space application copper-water heat pipes as described in any one of claims 1 to 6.
10. A computer-readable storage medium, characterized in that: The computer-readable storage medium stores a computer program, and when the computer program is executed by a processor, the steps of the process method for making copper-water heat pipes for space applications as described in any one of claims 1 to 6 are executed.