Coherent satellite thermal vacuum experiment device
By designing thermal component partitions in satellite thermal vacuum test devices and remotely operating thermal components using components such as conductive blocks, the problem of liquid nitrogen and hot oil energy neutralization inside the tank is solved, and more efficient experimental preparation and energy utilization are achieved.
Patent Information
- Application Number
- CN202411942270.4
- Authority / Receiving Office
- CN · China
- Patent Type
- Applications(China)
- Current Assignee / Owner
- Filing Date
- 2024-12-27
- Publication Date
- 2025-04-11
AI Technical Summary
The existing satellite thermal vacuum test device has the same change in the tank body, resulting in the energy of liquid nitrogen and hot oil neutralization inside the tank body when the experimental ambient temperature changes, increasing the experimental preparation time and causing energy loss.
By designing thermally conductive component partitions, using components such as conductive blocks, fixed partitions, mobile partitions and positioning blocks, remote operation of different thermally conductive components corresponding to different experimental environments is achieved to avoid neutralization of liquid nitrogen and hot oil energy.
It effectively reduces the phenomenon that liquid nitrogen and hot oil energy are neutralized inside the tank, reduces the experimental preparation time, avoids energy loss, and improves the experimental efficiency.
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Figure CN119796541A_ABST
Abstract
Description
Technical Field
[0001] The invention relates to the technical field of thermal vacuum experiments, and in particular to a continuous satellite thermal vacuum experiment device. Background Art
[0002] Thermal vacuum experiments refer to thermal experiments conducted in a vacuum environment, which are usually used to study the behavior of materials under extreme temperature and pressure conditions. Such experiments are widely used in aerospace, materials science, physics and other fields.
[0003] Existing satellite thermal vacuum test equipment often generates the target ambient temperature by transporting flowing liquid nitrogen and hot oil inside the tank. However, since the tank is unchanging, when the required experimental ambient temperature changes, the energy of the liquid nitrogen and hot oil will be neutralized inside the tank, which will not only increase the preparation time of the experiment but also cause energy loss problems for the liquid nitrogen and hot oil. Summary of the invention
[0004] Therefore, the present invention is made in view of the above problems. The purpose of the present invention is to realize remote operation of different heat-conducting components corresponding to different experimental environments through the design of heat-conducting component partitions, and solve the problem that the existing satellite thermal vacuum test device often generates the target ambient temperature by transporting flowing liquid nitrogen and hot oil inside the tank body, but because the tank body is unchanged, when the required experimental ambient temperature changes, the energy of liquid nitrogen and hot oil will be neutralized inside the tank body, which will not only increase the preparation time of the experiment but also cause the energy loss of liquid nitrogen and hot oil. The present invention achieves the above purpose through the following technical solutions:
[0005] A continuous satellite thermal vacuum experiment device, comprising: a bottom plate, an outer wall, an exhaust device, a conduction device, an adjustment device, a storage tank 1, a shell device, an electric telescopic rod, a box door, and a storage tank 2. The conduction device comprises: a conduction block, a fixed partition, a movable partition 1, a movable partition 2, a movable partition 3, and a positioning block. The conduction block is composed of a plurality of heat-conducting circular rings of annular structure. The outer side of the fixed partition is fixedly arranged on the inner wall surface of the outer wall, and the inner side is close to the conduction block. The left and right sides of the movable partition 1, the movable partition 2, and the movable partition 3 are close to the inner wall surface of the outer wall and the outer wall surface of the conduction block. The movable partition 1, the movable partition 2, and the movable partition 3 are arranged in sequence between two fixed partitions. The positioning block is cylindrical, and four are provided, which are arranged in pairs on both sides. On the fixed partition, the adjustment device includes: a guide tube 1, an upper guide port 1, an upper guide port 2, an elastic telescopic rod, a guide tube 2, a moving rod, a lower guide port 1, and a lower guide port 2. The guide tube 1 is a hollow cavity structure, and there are two of them, which are respectively located at the upper and lower ends of the outer wall. The upper guide port 1 and the upper guide port 2 are both located on the upper guide tube 1. There are two elastic telescopic rods, which are respectively arranged on one side of the two groups of guide tubes 1 through connecting rods. The moving rod is arranged on the output ends of the two elastic telescopic rods. There are two guide tubes 2, one end of which can be connected to the guide tube 1, and the other end is respectively connected to the storage tank 2 and the two storage tanks 1. The moving rod is arranged on the output ends of the two elastic telescopic rods. The lower guide port 1 and the lower guide port 2 are arranged on the guide tube 1 located below.
[0006] Preferably, the outer wall is fixedly arranged on the upper wall surface of the bottom plate through a connecting rod, the exhaust device is fixedly arranged on one side end of the shell device, the exhaust device is connected to the inside of the shell device, the conduction device is arranged on the adjustment device, one end of the adjustment device is fixedly arranged on the output end of the electric telescopic rod, the number of storage tanks one is two, which are used to store hot oil, and the number of storage tanks two is two, which are used to store liquid nitrogen.
[0007] Preferably, the conduction block is arranged on the guide tube one, and the connection between adjacent heat-conducting rings is provided with insulation material to block the transfer of heat energy. The fixed partitions are semicircular ring structures and are arranged opposite to each other on both sides of the guide tube one. The two oppositely arranged fixed partitions can form an approximately full circle.
[0008] Preferably, the movable baffle 1, movable baffle 2 and movable baffle 3 are all semicircular ring structures, two of which are provided, and are arranged opposite to each other on both sides of the guide pipe 1 to form an approximately full circle structure.
[0009] Preferably, the movable partition plate 2 and the movable partition plate 3 are provided with openings for the left positioning block to pass through, and the movable partition plate 2 and the movable partition plate 1 are provided with openings for the right positioning block to pass through.
[0010] Preferably, one end of the upper guide tube 1 is set on the electric telescopic rod, and the other end is connected to the guide tube 2. One side of the guide tube 1 located at the bottom is fixed on the upper wall surface of the base plate through a connecting rod, and the other side is connected to the guide tube 2. The two guide tubes 1 respectively contain the delivery pipelines of two storage tanks 2 and two storage tanks 1.
[0011] Preferably, the upper guide port one and the upper guide port two are respectively connected to the delivery pipelines of the two storage tanks two; the upper guide port one and the upper guide port two are adjacently arranged on the upper guide pipe one, and the lower guide port one and the lower guide port two are respectively connected to the delivery pipelines of the two storage tanks one, and the lower guide port one and the lower guide port two are adjacently arranged on the lower guide pipe one.
[0012] Preferably, the openings of the upper guide port 1, the upper guide port 2, the lower guide port 1, and the lower guide port 2 are provided with electrically controlled valves, the upper guide port 2 is used for discharging liquid nitrogen, and the upper guide port 1 is responsible for reflux of liquid nitrogen.
[0013] Preferably, the shell device includes: an annular shell, a protrusion, and an isolation zone. The annular shell is a hollow cavity structure and is arranged on the upper wall surface of the base plate through a connecting rod. Multiple annular protrusions are arranged on the outer wall surface of the annular shell. The isolation zone is a cavity and is arranged between two adjacent protrusions. The width of the isolation zone is the same as the width of the protrusion and the width of the heat conductive ring of the conduction block.
[0014] The beneficial effects of the present invention are as follows:
[0015] 1. By blocking the movement of the movable partition 1 and the movable partition 3 with the positioning block, different partition spacing differences can be formed, and liquid nitrogen and hot oil can quickly fill the space with a small partition spacing difference, avoiding the problem that when liquid nitrogen is added from top to bottom, the liquid nitrogen will be preferentially gathered at the lower part of the outer wall of the vacuum tank due to its own gravity, resulting in a temperature difference between the upper and lower ends of the vacuum tank in the early stage;
[0016] 2. The electric telescopic rod drives the flow guide tube and the conduction block to move from the low-temperature experimental environment to the high-temperature experimental environment. The distance moved is the same as the width of the heat-conducting ring of the conduction block, the width of the protrusion, and the width of the isolation zone. The heat-conducting ring of the conduction block overlaps with the protrusion in the experimental environment, so that during the transition between the low-temperature experimental environment and the high-temperature experimental environment, the heat-conducting ring of the conduction block will also be converted, that is, the heat-conducting ring of the conduction block that overlaps with the protrusion in the original experimental environment will be driven by the electric telescopic rod to move to the isolation zone position between two adjacent protrusions after the experimental environment is changed; thereafter, the residual energy of the heat-conducting ring of the conduction block cannot continue to be transferred to the protrusion, and on the other hand, the heat-insulating material that blocks the heat energy transfer is provided at the connection of multiple heat-conducting rings, which will also reduce the influence of energy transfer to adjacent heat-conducting rings;
[0017] 3. The raised separation arrangement and the conduction block being composed of a plurality of heat-conducting rings and the connection of the plurality of rings being provided with heat-insulating materials for blocking the transfer of heat energy can effectively reduce the problem of energy loss caused by the mutual neutralization of the hot oil and liquid nitrogen energy when multiple experiments are carried out alternately. BRIEF DESCRIPTION OF THE DRAWINGS
[0018] Figure 1 The overall structure of the present invention is shown in FIG. Figure 1 .
[0019] Figure 2 The overall structure of the present invention is shown in FIG. Figure 2 .
[0020] Figure 3 It is a structural schematic diagram of the main internal devices of the present invention.
[0021] Figure 4 It is a schematic structural diagram of the housing device of the present invention.
[0022] Figure 5 The structure of the regulating device of the present invention is shown in FIG. Figure 1 .
[0023] Figure 6 For the present invention Figure 5 Enlarged view of area A in the middle.
[0024] Figure 7 For the present invention Figure 5 Enlarged view of area B in the middle.
[0025] Figure 8 The structure of the regulating device of the present invention is shown in FIG. Figure 2 .
[0026] Fig. 9 For the present invention Figure 8 Magnified view of area C in the middle.
[0027] Fig.10 For the present invention Figure 8 Magnified view of area D in the middle.
[0028] Among them, 100, bottom plate; 200, outer wall; 300, exhaust device; 400, conduction device; 410, conduction block; 420, fixed partition; 430, movable partition one; 440, movable partition two; 450, movable partition three; 460, positioning block; 500, adjustment device; 510, guide tube one; 520, upper guide port one; 530, upper guide port two; 540, elastic telescopic rod; 550, guide tube two; 560, mobile rod; 570, lower guide port one; 580, lower guide port two; 600, storage tank one; 700, shell device; 710, annular shell; 720, protrusion; 730, isolation belt; 800, electric telescopic rod; 900, box door; 1000, storage tank two. DETAILED DESCRIPTION
[0029] The present invention is further described below in conjunction with the embodiments and the accompanying drawings, but the protection scope of the present invention is not limited to the following embodiments. Any modifications and changes made to the present invention within the spirit of the present invention and the protection scope of the claims fall within the protection scope of the present invention.
[0030] like Figure 1-3 As shown, a coherent satellite thermal vacuum experimental device includes: a bottom plate 100, an outer wall 200, an exhaust device 300, a conduction device 400, an adjustment device 500, a storage tank 1 600, a shell device 700, an electric telescopic rod 800, a box door 900, and a storage tank 2 1000;
[0031] The outer wall 200 is fixedly arranged on the upper wall surface of the bottom plate 100 through a connecting rod;
[0032] The air extraction device 300 is fixedly arranged at one side end of the housing device 700, the air extraction device 300 is connected to the inside of the housing device 700 and is provided with a pump, which can discharge the air inside the housing device 700 during specific implementation;
[0033] The conducting device 400 is arranged on the adjusting device 500;
[0034] One end of the adjustment device 500 is fixedly arranged on the output end of the electric telescopic rod 800;
[0035] The storage tank 1 600 is two in number and is used to store unused hot oil and hot oil after energy transfer respectively; a pump is built into the storage tank 1 600 to drive the hot oil contained therein to move;
[0036] The housing device 700 is a hollow structure fixed on the upper wall of the bottom plate 100 by a connecting rod, and its interior can be used as an operating place for thermal vacuum experiments;
[0037] The electric telescopic rod 800 is fixed to the outer wall 200 via a connecting rod;
[0038] The box door 900 is arranged at one end of the housing device 700 through a rotating bearing;
[0039] The storage tank 1000 is two in number and is used to store unused liquid nitrogen and liquid nitrogen after energy conduction respectively; the storage tank 1000 is equipped with a pump to drive the liquid nitrogen contained therein to move;
[0040] like Figure 5-10 As shown, the conducting device 400 includes: a conducting block 410, a fixed partition 420, a movable partition 1 430, a movable partition 2 440, a movable partition 3 450, and a positioning block 460;
[0041] The conducting device 400 is mainly composed of a conducting block 410 and a plurality of combined partition blocks arranged on the outer wall of the conducting block 410. The number of combined partition blocks can be adjusted in real time according to the specific length of the conducting block 410 during implementation. The following is an introduction based on one combined partition block.
[0042] The conduction block 410 is disposed on the guide tube 1 510, which is an annular structure and is composed of a plurality of heat-conducting rings. The connection between adjacent heat-conducting rings is provided with a heat-insulating material for blocking the transfer of heat energy. The width of the heat-conducting ring is the same as the width of the protrusion 720 and the width of the isolation zone 730. The conduction block 410 mainly plays the role of transferring the energy of the hot oil or liquid nitrogen to the protrusion 720 in specific implementation.
[0043] The fixed baffles 420 are semicircular ring structures and are arranged on a combined baffle. Four of them are arranged opposite to each other on both sides of the guide tube 510. The two oppositely arranged fixed baffles 420 can form an approximately full circle. The outer side of the fixed baffles 420 is fixedly arranged on the inner wall surface of the outer wall 200, and the inner side is close to the conductive block 410.
[0044] The movable partition 1 430 is a semicircular ring structure, and two of them are arranged on a combined partition, and are arranged opposite to each other on both sides of the guide tube 1 510 to form an approximately full circle structure; the movable partition 1 430 is arranged on the movable rod 560, and the left and right sides are close to the inner wall surface of the outer wall 200 and the outer wall surface of the conductive block 410;
[0045] The second movable partition 440 is a semicircular ring structure. Two movable partitions 440 are arranged on a combined partition, and are arranged opposite to each other on both sides of the first flow guide tube 510 to form an approximately full circle structure. The second movable partition 440 is arranged on the first flow guide tube 510, and the left and right sides are close to the inner wall surface of the outer wall 200 and the outer wall surface of the conductive block 410.
[0046] The movable partition plate 3 450 is a semicircular ring structure, and two of them are arranged on a combined partition plate, and are arranged opposite to each other on both sides of the guide tube 1 510 to form an approximately full circle structure; the movable partition plate 1 430 is arranged on the movable rod 560, and the left and right sides are close to the inner wall surface of the outer wall 200 and the outer wall surface of the conductive block 410;
[0047] On either side of the guide tube 1 510 , the movable baffle 1 430 , the movable baffle 2 440 , and the movable baffle 3 450 are all located between the two fixed baffles 420 ;
[0048] The positioning blocks 460 are cylindrical and are provided in four on a combined partition, and are respectively provided in pairs on the fixed partitions 420 on both sides of the guide tube 1 510; the two positioning blocks 460 on one side of the guide tube 1 510 are provided up and down and face inwards relatively;
[0049] The second movable partition 440 and the third movable partition 450 are provided with openings for the left positioning block 460 to pass through, and the second movable partition 440 and the first movable partition 430 are provided with openings for the side positioning block 460 to pass through, so that the left positioning block 460 will block the movement of the first movable partition 430, and the right positioning block 460 will block the movement of the third movable partition 450;
[0050] like Figure 5-10 As shown, the regulating device 500 includes: a guide tube 1 510, an upper guide port 1 520, an upper guide port 2 530, an elastic telescopic rod 540, a guide tube 2 550, a moving rod 560, a lower guide port 1 570, and a lower guide port 2 580;
[0051] The guide tube 1 510 is a hollow cavity structure, and there are two of them; one end of the guide tube 1 510 located at the top is set on the electric telescopic rod 800, and the other end is connected to the guide tube 2 550, and a deformable rubber tube is set at the connection position; one side of the guide tube 1 510 located at the bottom is fixed on the upper wall of the bottom plate 100 through a connecting rod, and the other side is connected to the guide tube 2 550, and a deformable rubber tube is set at the connection position; the two guide tubes 1 510 respectively contain the conveying pipelines of the two storage tanks 2 1000 and the two storage tanks 1 600;
[0052] The plurality of upper flow guide ports 520 are arranged on the flow guide pipe 510;
[0053] The plurality of upper guide ports 530 are arranged on the guide pipe 1 510 located above; the upper guide port 1 520 and the upper guide port 2 530 are respectively connected to the delivery pipelines of the two storage tanks 1000; the upper guide port 1 520 and the upper guide port 2 530 are arranged adjacent to each other on the guide pipe 1 510; the upper guide port 2 530 is used for discharging liquid nitrogen, and the upper guide port 1 520 is responsible for the reflux of liquid nitrogen;
[0054] The elastic telescopic rods 540 are two in number and are respectively arranged on both sides of the guide tube 1 510 via connecting rods.
[0055] The number of the second guide pipe 550 is two, one end of which is connected to the first guide pipe 510 through a deformable rubber tube, and the other end is connected to the second storage tank 1000 and the two first storage tanks 600;
[0056] The moving rod 560 is arranged on the output ends of the two elastic telescopic rods 540;
[0057] The lower guide port 1 570 and the lower guide port 2 580 are arranged on the guide pipe 1 510 located below; the lower guide port 1 570 and the lower guide port 2 580 are respectively connected to the conveying pipelines of the two storage tanks 1 600; the lower guide port 1 570 and the lower guide port 2 580 are arranged adjacent to each other on the lower guide pipe 1 510; the upper guide port 1 520, the upper guide port 2 530, the lower guide port 1 570, and the lower guide port 2 580 are provided with electric control valves at the openings to control the closing state of the openings;
[0058] like Figure 4 As shown, the housing device 700 includes: an annular housing 710, a protrusion 720, and an isolation belt 730;
[0059] The annular housing 710 is a hollow cavity structure and is arranged on the upper wall of the bottom plate 100 through a connecting rod;
[0060] The protrusions 720 are arranged in a plurality of ring shapes on the outer wall of the ring-shaped housing 710, and mainly play a role in conducting energy in specific implementation;
[0061] The isolation zone 730 is a partition space, which is mainly arranged between the protrusions 720 on the conductive block 410, so as to form a gap between the conductive block 410 and the annular shell 710 to prevent the residual energy on the conductive block 410 from continuing to be transmitted to the annular shell 710; the width of the isolation zone 730 between adjacent protrusions 720 is the same as the width of the protrusion 720 and the width of the heat conductive ring of the conductive block 410.
[0062] Working principle of the present invention:
[0063] like Figure 1-4 As shown, when a vacuum thermal test is performed on a satellite, the box door 900 is first opened to transport the object to be tested into the shell device 700. Then, after the box door 900 is closed, the exhaust device 300 is started to exhaust the air inside the shell device 700 to make it reach a vacuum state in preparation for the experiment.
[0064] When a low temperature experiment is required, the electric telescopic rod 800 contracts to drive the guide tube 1 510 to move, and the guide tube 1 510 drives the movable partition 2 440 on it to move closer to the electric telescopic rod 800, so that the movable partition 2 440, the movable partition 3 450 and the fixed partition 420 are attached together. Figure 6 At this time, the movable partition 1 430 is blocked by the left positioning block 460 and cannot move the same distance with the fixed partition 420, which makes the distance between the fixed partition 420 and the movable partition 1 430 smaller than the distance between the movable partition 1 430 and the movable partition 2 440;
[0065] At the same time, the upper guide port 1 520 will be located exactly between the movable partition 1 430 and the movable partition 2 440, and the upper guide port 2 530 will be located between the fixed partition 420 and the movable partition 1 430; then, driven by the built-in pump of the storage tank 2 1000, the liquid nitrogen is discharged from the upper guide port 2 530 into the space between the fixed partition 420 and the movable partition 1 430. Since the spacing between the above partitions is small, the liquid nitrogen can quickly fill the space between the two partitions, thereby avoiding the problem that when the liquid nitrogen is added from the top to the bottom, the liquid nitrogen will be preferentially gathered at the lower part of the outer wall of the vacuum tank due to its own gravity, resulting in a temperature difference between the upper and lower ends of the vacuum tank in the early stage;
[0066] A small hole is provided at the bottom of the movable partition 1 430, so that the liquid nitrogen at the bottom between the fixed partition 420 and the movable partition 1 430 can flow through the small hole into the space between the movable partition 1 430 and the movable partition 2 440 and finally flow back to the storage tank 2 1000 through the upper guide port 1 520 to wait for further processing and application;
[0067] When a high temperature experiment is required, the electric telescopic rod 800 drives the guide tube 1 510 to move in the reverse direction and reset, driving the movable partition 2 440 to move away from the electric telescopic rod 800, so that the movable partition 2 440, the movable partition 1 430 and the fixed partition 420 are attached together; at this time, the distance between the fixed partition 420 and the movable partition 3 450 is smaller than the distance between the movable partition 3 450 and the movable partition 2 440 due to the blocking of the positioning block 460;
[0068] At the same time, the lower guide port 1 570 will be located exactly between the movable partition 3 450 and the movable partition 2 440, and the lower guide port 2 580 will be located between the fixed partition 420 and the movable partition 3 450; then, driven by the built-in pump of the storage tank 1 600, the hot oil is discharged from the lower guide port 2 580 into the space between the fixed partition 420 and the movable partition 3 450, and a small hole is provided on the top of the movable partition 3 450, so that the hot oil at the bottom between the fixed partition 420 and the movable partition 3 450 can flow through the small hole into the space between the movable partition 3 450 and the movable partition 2 440 and finally flow back to the storage tank 1 600 through the lower guide port 1 570;
[0069] The energy of the hot oil and liquid nitrogen is transferred to the protrusion 720 through the conductive block 410, and then transferred to the annular housing 710 through the protrusion 720 to form a target temperature environment; in specific implementation, the electric telescopic rod 800 drives the guide tube 1 510 and the conductive block 410 to move from a low-temperature experimental environment to a high-temperature experimental environment. The distance moved is the same as the width of the heat-conducting ring of the conductive block 410, the width of the protrusion 720, and the width of the isolation zone 730, and the heat-conducting ring of the conductive block 410 in the experimental environment coincides with the protrusion 720;
[0070] This allows the heat-conducting ring of the conductive block 410 to be transformed during the transition between the low-temperature experimental environment and the high-temperature experimental environment, that is, the heat-conducting ring of the conductive block 410 that overlaps with the protrusion 720 in the original experimental environment will be driven by the electric telescopic rod 800 to move to the isolation zone 730 after the experimental environment is changed;
[0071] Afterwards, on the one hand, the residual energy of the heat-conducting circle of the conduction block 410 cannot continue to be transferred to the protrusion 720. On the other hand, the influence of the heat-conducting material that blocks the heat energy transfer arranged at the connection between the multiple heat-conducting rings will also reduce the influence of energy transfer to the adjacent heat-conducting rings. The above-mentioned segmented arrangement of the protrusions 720 and the partitioned arrangement of the heat-conducting rings of the conduction block 410 can effectively reduce the problem of energy loss caused by the mutual neutralization of hot oil and liquid nitrogen energy when multiple experiments are carried out alternately.
Claims
1. A coherent satellite thermal vacuum experiment device, comprising: The invention relates to a bottom plate (100), an outer wall (200), an exhaust device (300), a conduction device (400), an adjustment device (500), a storage tank 1 (600), a shell device (700), an electric telescopic rod (800), a box door (900), and a storage tank 2 (1000); the conduction device (400) comprises a conduction block (410), a fixed partition (420), a movable partition 1 (430), a movable partition 2 (440), a movable partition 3 (450), and a positioning block (460); the conduction block (410) is composed of a plurality of heat conduction ring structures. The fixed partition (420) is composed of a circular splicing, the outer side of the fixed partition (420) is fixedly arranged on the inner wall surface of the outer wall (200), and the inner side is close to the conductive block (410). The left and right sides of the movable partitions 1 (430), 2 (440), and 3 (450) are close to the inner wall surface of the outer wall (200) and the outer wall surface of the conductive block (410). The movable partitions 1 (430), 2 (440), and 3 (450) are arranged in sequence between the two fixed partitions (420). The positioning blocks (460) are cylindrical and are provided with four, which are arranged in pairs on both sides. The regulating device (500) comprises: a flow guide tube 1 (510), an upper flow guide port 1 (520), an upper flow guide port 2 (530), an elastic telescopic rod (540), a flow guide tube 2 (550), a moving rod (560), a lower flow guide port 1 (570), and a lower flow guide port 2 (580). The flow guide tube 1 (510) is a hollow cavity structure, and there are two of them, which are respectively located at the upper and lower ends of the outer wall (200). The upper flow guide port 1 (520) and the upper flow guide port 2 (530) are both located on the upper flow guide tube 1 (510). The elastic telescopic rod (540) ) are two in number and are respectively arranged on one side of the two groups of guide tubes 1 (510) through connecting rods, the moving rod (560) is arranged on the output ends of the two elastic telescopic rods (540), the guide tube 2 (550) is two in number, one end of which can be connected to the guide tube 1 (510) and the other end of which is respectively connected to the storage tank 2 (1000) and the two storage tanks 1 (600), the moving rod (560) is arranged on the output ends of the two elastic telescopic rods (540), and the lower guide port 1 (570) and the lower guide port 2 (580) are arranged on the guide tube 1 (510) located below.
2. A continuous satellite thermal vacuum experiment device according to claim 1, characterized in that: The outer wall (200) is fixedly arranged on the upper wall surface of the bottom plate (100) through a connecting rod, the air extraction device (300) is fixedly arranged on one side end of the shell device (700), the air extraction device (300) is connected to the inside of the shell device (700), the conduction device (400) is arranged on the adjustment device (500), one end of the adjustment device (500) is fixedly arranged on the output end of the electric telescopic rod (800), the number of storage tanks (600) is two, which are used to store hot oil, and the number of storage tanks (1000) is two, which are used to store liquid nitrogen.
3. A continuous satellite thermal vacuum experiment device according to claim 1, characterized in that: The conduction block (410) is arranged on the guide tube (510), and the connection between adjacent heat-conducting circular rings is provided with a heat-insulating material for blocking the transfer of heat energy. The fixed partitions (420) are semi-circular ring structures and are arranged opposite to each other on both sides of the guide tube (510). The two oppositely arranged fixed partitions (420) can form an approximately full circle.
4. A continuous satellite thermal vacuum experiment device according to claim 1, characterized in that: The movable baffle 1 (430), movable baffle 2 (440), and movable baffle 3 (450) are all semicircular ring structures, and two of them are provided. They are arranged opposite to each other on both sides of the guide tube 1 (510) to form a nearly full circle structure.
5. A continuous satellite thermal vacuum experiment device according to claim 1, characterized in that: The movable partition plate 2 (440) and the movable partition plate 3 (450) are provided with openings for the left positioning block (460) to pass through, and the movable partition plate 2 (440) and the movable partition plate 1 (430) are provided with openings for the right positioning block (460) to pass through.
6. A continuous satellite thermal vacuum experiment device according to claim 1, characterized in that: One end of the upper guide pipe 1 (510) is arranged on the electric telescopic rod (800), and the other end is connected to the guide pipe 2 (550). One side of the lower guide pipe 1 (510) is fixedly arranged on the upper wall surface of the bottom plate (100) through a connecting rod, and the other side is connected to the guide pipe 2 (550). The two guide pipes 1 (510) respectively contain the conveying pipelines of the two storage tanks 2 (1000) and the two storage tanks 1 (600).
7. A continuous satellite thermal vacuum experiment device according to claim 1, characterized in that: The upper flow guide port 1 (520) and the upper flow guide port 2 (530) are respectively connected to the delivery pipelines of the two storage tanks 1000; the upper flow guide port 1 (520) and the upper flow guide port 2 (530) are adjacently arranged on the upper flow guide pipe 1 (510), and the lower flow guide port 1 (570) and the lower flow guide port 2 (580) are respectively connected to the delivery pipelines of the two storage tanks 1 (600), and the lower flow guide port 1 (570) and the lower flow guide port 2 (580) are adjacently arranged on the lower flow guide pipe 1 (510).
8. A continuous satellite thermal vacuum experiment device according to claim 7, characterized in that: The openings of the upper guide port 1 (520), the upper guide port 2 (530), the lower guide port 1 (570), and the lower guide port 2 (580) are provided with electric control valves. The upper guide port 2 (530) is used for discharging liquid nitrogen, and the upper guide port 1 (520) is responsible for the reflux of liquid nitrogen.
9. A continuous satellite thermal vacuum experiment device according to claim 1, characterized in that: The shell device (700) comprises: an annular shell (710), a protrusion (720), and an isolation zone (730); the annular shell (710) is a hollow cavity structure and is arranged on the upper wall surface of the bottom plate (100) through a connecting rod; a plurality of protrusions (720) are arranged in annular shapes on the outer wall surface of the annular shell (710); and the isolation zone (730) is a cavity and is arranged between two adjacent protrusions (720).
10. A continuous satellite thermal vacuum experiment device according to claim 9, characterized in that: The width of the isolation zone (730) is the same as the width of the protrusion (720) and the width of the heat conduction ring of the conductive block (410).