阅读说明：本技术 超重力离心机 (Hypergravity centrifuge ) 是由 王亚林 杨毅 郭轶楠 丁德 余俊祥 于 2021-09-10 设计创作，主要内容包括：本申请提供了一种超重力离心机,超重力离心机包括绕竖直轴线转动的转子、罩设在转子外的实验舱、以及相应的降温系统转子带有与实验舱转动配合的轴部,轴部带有位于实验舱外部的轴顶端,降温系统包括液冷装置和蒸发冷却装置；液冷装置包括制冷源,以及与制冷源连通且与实验舱的舱壁热耦合的第一冷却介质循环管路；蒸发冷却装置包括设置于实验舱外部的冷凝室,以及与转子热耦合的热管散热器,热管散热器的吸热端固定于转子,热管散热器的散热端经过轴顶端伸入冷凝室。本申请的超重力离心机,通过液冷装置和蒸发冷装置的相互配合,有效降低转子在高速运转时所产生的温度,保障超重力离心机安全高效的工作。(The application provides a hypergravity centrifugal machine, the hypergravity centrifugal machine comprises a rotor rotating around a vertical axis, an experiment chamber covered outside the rotor, and a corresponding cooling system rotor, wherein the corresponding cooling system rotor is provided with a shaft part in rotating fit with the experiment chamber, the shaft part is provided with a shaft top end positioned outside the experiment chamber, and the cooling system comprises a liquid cooling device and an evaporative cooling device; the liquid cooling device comprises a refrigeration source and a first cooling medium circulating pipeline which is communicated with the refrigeration source and is thermally coupled with the cabin wall of the experiment cabin; the evaporative cooling device comprises a condensation chamber arranged outside the experimental cabin and a heat pipe radiator thermally coupled with the rotor, wherein the heat absorption end of the heat pipe radiator is fixed on the rotor, and the heat dissipation end of the heat pipe radiator extends into the condensation chamber through the top end of the shaft. The utility model provides a hypergravity centrifuge, through mutually supporting of liquid cooling device and evaporation cold charge, effectively reduce the produced temperature of rotor when high-speed operation, guarantee hypergravity centrifuge safety efficient work.)

1. The experimental device comprises a supergravity centrifugal machine, a cooling system and a control system, wherein the supergravity centrifugal machine comprises a rotor rotating around a vertical axis, an experimental cabin covered outside the rotor, and the cooling system is used for cooling the experimental cabin;

the liquid cooling device comprises a refrigeration source and a first cooling medium circulation pipeline which is communicated with the refrigeration source and is thermally coupled with the cabin wall of the experiment cabin;

the evaporative cooling device comprises a condensation chamber arranged outside the experimental cabin and a heat pipe radiator thermally coupled with the rotor, wherein the heat absorption end of the heat pipe radiator is fixed on the rotor, and the heat dissipation end of the heat pipe radiator extends into the condensation chamber through the top end of the shaft.

2. The hypergravity centrifuge of claim 1, wherein the liquid cooling device further comprises a second cooling medium circulation line thermally coupled to the condensing chamber.

3. The hypergravity centrifuge of claim 1 wherein the condensation chamber is located above the shaft tip such that condensate within the condensation chamber flows into the shaft tip by its own weight.

4. The hypergravity centrifuge of claim 3, wherein the heat pipe radiator is fixed to an outside of the rotor, and the condensate circulates bi-directionally within the heat pipe radiator to form a cooling medium circulation line.

5. The hypergravity centrifuge of claim 4 wherein the rotor itself is symmetrical about the vertical axis and has a high temperature end distal from the vertical axis, the heat pipe heat sink comprising:

a first duct extending vertically within the shaft portion, an upper end of the first duct being the heat dissipating end;

and one end of the second pipeline is communicated with the lower end of the first pipeline, and the other end of the second pipeline is the heat absorption end and extends to the high-temperature end.

6. The hypergravity centrifuge of claim 5, wherein the second conduit comprises:

the vertical section is close to the surface of the high-temperature end, and the lower end of the vertical section is the heat absorption end;

and one end of the inclined section is communicated with the bottom end of the first pipeline, and the other end of the inclined section is communicated with the upper end of the vertical section.

7. The hypergravity centrifuge of claim 6, wherein an upper end position of the vertical section is higher than a bottom end position of the first conduit.

8. The hypergravity centrifuge of claim 1, wherein the cooling system further comprises a vacuum pump connected to the laboratory chamber through a vacuum line to adjust the vacuum level in the laboratory chamber.

9. The hypergravity centrifuge of claim 2, wherein the cooling system further comprises a cold storage tank in communication with the first cooling medium circulation line for storing the cooling medium generated by the refrigeration source.

10. The hypergravity centrifuge of claim 1, wherein the first cooling medium circulation line passes through the inside of the laboratory chamber side wall.

Technical Field

The application relates to the technical field of hypergravity, in particular to a hypergravity centrifugal machine.

Background

The basic principle of the supergravity engineering technology is to utilize the unique flow behavior of a multi-phase flow system under the supergravity condition to strengthen the relative speed and mutual contact between phases, thereby realizing the efficient mass and heat transfer process and the efficient chemical reaction process. On the earth, a simple method for realizing a hypergravity environment is realized by simulation through generating centrifugal force by rotation. Such a rotary apparatus is called a supergravity centrifuge.

The supergravity centrifugal machine mainly comprises a rotor rotating around a vertical axis and an experiment cabin covered outside the rotor, and the rotor is driven to rotate at a high speed by a driving motor to generate huge centrifugal force, so that the requirement of a supergravity experiment is met. In the process, the rotation of the rotor drives the air in the experiment chamber to flow, so that the rotor and the ambient air, and the flowing air and the experiment chamber rub with each other to generate heat. If the part of heat is not dissipated in time, the temperature in the experiment chamber is rapidly increased, the safe operation of the whole experiment device is endangered, and the safety performance and the measurement precision of electronic elements such as a measurement sensor and the like are greatly influenced. Therefore, there is a need to design a cooling system for a hypergravity centrifuge.

When the supergravity centrifugal machine runs, the rotor rotates at a high speed, and the heating power can reach 5 MW. For example, the rotor tip has the highest speed of movement relative to air, the temperature is higher, and the heat dissipation requirements are greater. What present hypergravity centrifuge's cooling system generally adopted is the static pipeline that is fixed in the experiment cabin, and static pipeline is convenient direct and the bulkhead of experiment cabin or the air heat transfer in the experiment cabin, and nevertheless inconvenient carries out direct heat transfer cooling to the rotor of high-speed motion, and the cooling effect remains to be improved.

Disclosure of Invention

The application provides a hypergravity centrifuge can improve the cooling ability, and the operation is more reliable.

The application provides a hypergravity centrifuge, hypergravity centrifuge includes around vertical axis pivoted rotor, cover establish outside the rotor experiment cabin and corresponding cooling system, the rotor have with experiment cabin normal running fit's axial region, the axial region has the axle top that is located the experiment cabin outside, cooling system includes liquid cooling device and evaporation cooling device;

the liquid cooling device comprises a refrigeration source and a first cooling medium circulation pipeline which is communicated with the refrigeration source and is thermally coupled with the cabin wall of the experiment cabin;

the evaporative cooling device comprises a condensation chamber arranged outside the experimental cabin and a heat pipe radiator communicated with the condensation chamber and extending into the rotor through the top end of the shaft to exchange heat.

Several alternatives are provided below, but not as an additional limitation to the above general solution, but merely as a further addition or preference, each alternative being combinable individually for the above general solution or among several alternatives without technical or logical contradictions.

Optionally, the liquid cooling device further comprises a second cooling medium circulation pipeline thermally coupled to the condensation chamber.

Optionally, the condensation chamber is located above the shaft tip so that condensate within the condensation chamber flows into the shaft tip by its own weight.

Optionally, the heat pipe radiator is a non-closed loop structure formed by communicating multiple sections of pipelines and has a heat dissipation end and a heat absorption end, wherein the heat dissipation end extends into the condensation chamber, the heat absorption end is thermally coupled with the rotor, and a cooling medium flows in the same section of pipeline in two directions to form a cooling medium circulation pipeline.

Optionally, the rotor itself is of a symmetrical structure with respect to the vertical axis and has a high temperature end far away from the vertical axis, and the heat pipe radiator includes:

a first duct extending vertically within the shaft portion, an upper end of the first duct being the heat dissipating end;

and one end of the second pipeline is communicated with the lower end of the first pipeline, and the other end of the second pipeline is the heat absorption end and extends to the high-temperature end of the rotor.

Optionally, the second duct includes:

the vertical section is close to the surface of the high-temperature end, and the lower end of the vertical section is the heat absorption end;

and one end of the inclined section is communicated with the bottom end of the first pipeline, and the other end of the inclined section is communicated with the upper end of the vertical section.

Optionally, the upper end position of the vertical section is higher than the bottom end position of the first pipeline.

Optionally, the cooling system further comprises a vacuum pump, and the vacuum pump is connected to the experiment chamber through a vacuum pipeline to adjust the vacuum degree in the experiment chamber.

Optionally, the cooling system further includes a cold storage tank communicated with the first cooling medium circulation pipeline, and configured to store the cooling medium generated by the refrigeration source.

Optionally, the first cooling medium circulation pipeline penetrates through the side wall of the experiment chamber.

The utility model provides a hypergravity centrifuge, through mutually supporting of liquid cooling device and evaporation cold charge, effectively reduce the produced temperature of rotor when high-speed operation, guarantee hypergravity centrifuge safety efficient work.

Drawings

FIG. 1 is a schematic structural diagram of a high gravity centrifuge according to an embodiment of the present disclosure;

fig. 2 is a schematic structural diagram of an evaporative cooling device according to an embodiment of the present application.

The reference numerals in the figures are illustrated as follows:

100. a hypergravity centrifuge;

200. a rotor; 201. a shaft portion; 202. a shaft top end; 203. a high temperature end;

300. an experiment cabin; 301. a bulkhead;

400. a cooling system;

500. a liquid cooling device; 501. a refrigeration source; 502. a first cooling medium circulation line; 503. a second cooling medium circulation line;

600. an evaporative cooling device; 601. a condensing chamber; 602. a heat pipe radiator; 603. a heat dissipation end; 604. a heat absorption end; 605. a first conduit; 606. a second conduit; 607. a vertical section; 608. an inclined section; 609. an air flow channel;

700. a vacuum pump; 701. a vacuum valve;

800. a cold storage tank;

900. and a circulating pump.

Detailed Description

The technical solutions in the embodiments of the present application will be clearly and completely described below with reference to the drawings in the embodiments of the present application, and it is obvious that the described embodiments are only a part of the embodiments of the present application, and not all of the embodiments. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present application.

It will be understood that when an element is referred to as being "connected" to another element, it can be directly connected to the other element or intervening elements may also be present. When a component is referred to as being "disposed on" another component, it can be directly on the other component or intervening components may also be present.

Unless defined otherwise, all technical and scientific terms used herein have the same meaning as commonly understood by one of ordinary skill in the art to which this application belongs. The terminology used in the description of the present application herein is for the purpose of describing particular embodiments only and is not intended to be limiting of the application. As used herein, the term "and/or" includes any and all combinations of one or more of the associated listed items.

The application discloses a hypergravity centrifuge 100, the hypergravity centrifuge 100 includes the rotor 200 rotating around the vertical axis, the experiment chamber 300 covered outside the rotor 200, and the corresponding cooling system 400, the rotor 200 has the shaft part 201 matching with the experiment chamber 300, the shaft part 201 has the shaft top 202 outside the experiment chamber 300, the cooling system 400 includes the liquid cooling device 500 and the evaporation cooling device 600;

liquid cooling device 500 includes a refrigeration source 501, and a first cooling medium circulation line 502 in communication with refrigeration source 501 and thermally coupled to bulkhead 301 of experiment chamber 300;

the evaporative cooling device 600 includes a condensation chamber 601 disposed outside the laboratory chamber 300, and a heat pipe radiator 602 communicating with the condensation chamber 601 and extending into the interior of the rotor 200 via the shaft top end 202 for heat exchange.

In this embodiment, the huge centrifugal force generated by the high-speed rotation of the rotor 200 is used to satisfy the relevant requirements of the supergravity experiment; the experiment chamber 300 is used for installing experiment instruments or placing experiment articles; when the supergravity centrifuge 100 operates, a large amount of heat is generated by friction between the rotor 200 rotating at a high speed and the flowing air and between the flowing air and the bulkhead 301, and the heat generated between the rotor 200 and the bulkhead 301 is absorbed through the first cooling medium circulation pipeline 502 of the liquid cooling device 500, so that the temperature of the supergravity centrifuge 100 is reduced; when the supergravity centrifuge 100 is in operation, a large amount of heat is generated inside the rotor 200 due to high-speed movement, and the heat inside the rotor 200 is absorbed by the heat pipe radiator 602 of the evaporative cooling device 600, so that the influence of the rotor 200 on the use effect due to too high temperature is prevented, and the centrifugation degree of the supergravity centrifuge 100 is reduced.

The liquid cooling device 500 and the evaporative cooling device 600 absorb heat, so that the accuracy of each instrument in the supergravity centrifuge 100 is not influenced by the rise of temperature, and the supergravity centrifuge 100 can safely and effectively run.

The liquid cooling device 500 is connected to the condensation chamber 601 in such a way that the liquid cooling device 500 further comprises a second cooling medium circulation line 503 thermally coupled to the condensation chamber 601. The port of the second cooling medium circulation pipeline 503 entering the condensation chamber 601 is lower than the port of the outgoing condensation chamber 601, so that the cooling medium flowing out of the refrigeration source 501 and other devices can be fully filled around the condensation chamber 601, and the condensation chamber 601 can be fully cooled. The cooling medium enters the refrigeration source 501 through the circulation pump 900, the cooling medium is cooled, and the cooled cooling medium is conveyed to the second cooling medium circulation pipeline 503 again to start the next circulation.

To facilitate the flow of condensate into the shaft tip 202, the condensation chamber 601 is positioned above the shaft tip 202 such that condensate within the condensation chamber 601 flows into the shaft tip 202 by its own weight.

The condensate flows through the heat pipe radiator 602 to cool the rotor 200, the heat pipe radiator 602 is a non-closed loop structure formed by communicating a plurality of sections of pipelines and is provided with a heat dissipation end 603 and a heat absorption end 604, wherein the heat dissipation end 603 extends into the condensation chamber 601, the heat absorption end 604 is thermally coupled with the rotor 200, and the cooling medium flows in the same section of pipeline in a bidirectional way to form a cooling medium circulation pipeline. The cooling medium in the second cooling medium circulation pipeline 503 cools the condensate in the heat dissipation end 603, and the cooled condensate flows through the heat absorption end 604 by virtue of self gravity and centrifugal force to absorb the heat inside the rotor 200, so as to cool the inside of the rotor 200. The heat pipe radiator 602 is fixed outside the rotor 200, which facilitates maintenance and replacement by maintenance personnel.

The specific structure of the heatpipe radiator 602 is that the rotor 200 is a symmetrical structure with respect to the vertical axis and has a high temperature end 203 far away from the vertical axis, and the heatpipe radiator 602 includes: a first duct 605 extending vertically in the shaft portion 201, an upper end of the first duct 605 being a heat dissipating end 603; and a second pipe 606 having one end communicating with the lower end of the first pipe 605 and the other end serving as a heat absorbing end 604 and extending to the high temperature end 203 of the rotor 200. Preferably, the number of the rotors 200 is 2, and the rotors are located at both ends of the shaft 201. When the hypergravity centrifuge 100 works, the rotor 200 rotates at a high speed, the bottom of the rotor 200 is almost vertical to the bottom surface of the experiment chamber 300, the condensate is thrown to the heat absorption end 604 of the second pipeline 606 due to the centrifugal force when flowing from the heat dissipation end 603 to the shaft top end 202 through the first pipeline 605, the condensate absorbs heat generated by friction between the rotor 200 and flowing air at the heat absorption end 604 through phase-change heat exchange and is evaporated into gas, the condensate evaporated into gas returns to the heat dissipation end 603 through the air flow channel 609 inside the heat pipe radiator 602, the condensate in the second cooling medium circulation pipeline 503 is cooled into liquid at the heat dissipation end 603, and enters the shaft top end 202 again through the first pipeline 605 to start the next circulation. As a preferred solution, the heat dissipating end 603 may be a cylindrical cavity, and the heat dissipating end 603 rotates with the rotor 200 in the condensing chamber 601. The heat sink end 604 is fixed to the high temperature end 203 outside the rotor 200.

In order to make the condensate reach the heat absorption end 604 better by centrifugal force, the second conduit 606 comprises: a vertical section 607 proximate to the surface of the high temperature end 203, the lower end of the vertical section 607 being a heat absorbing end 604; an inclined section 608 having one end communicating with the bottom end of the first conduit 605 and the other end communicating with the upper end of the vertical section 607. Wherein the upper end position of the vertical section 607 is higher than the bottom end position of the first conduit 605. The inclined section 608 gradually rises from the bottom end of the first pipeline 605, and the vertical section 607 is close to the high-temperature section, so that the condensate can better take away heat through phase-change heat exchange.

In order to reduce the resistance of the rotor 200 during rotation, the cooling system 400 further comprises a vacuum pump 700, and the vacuum pump 700 is connected to the experiment chamber 300 through a vacuum pipeline to adjust the vacuum degree in the experiment chamber 300. When the vacuum level in the experiment chamber 300 is reduced, the resistance of the air to the rotation of the rotor 200 is significantly reduced, and the resistance between the flowing air and the bulkhead 301 is also reduced. The vacuum pump 700 is used for vacuumizing the experiment chamber 300 by opening the vacuum valve 701, and the experiment chamber 300 is enabled to reach a certain vacuum degree, and the vacuum degree can be determined according to the difference value between the actually measured temperature in the experiment chamber 300 and the experiment requirement.

In order to ensure sufficient use of the cooling medium during the operation of the supergravity centrifuge 100, the cooling system 400 further includes a cold storage tank 800 communicated with the first cooling medium circulation pipeline 502 for storing the cooling medium generated by the refrigeration source 501. In order to allow the cooling medium to better absorb heat in the experiment chamber 300, a first cooling medium circulation line 502 passes through the side wall of the experiment chamber 300. The first cooling medium circulation line 502 is located at the inlet end of the bulkhead 301 lower than the outlet end, and can be used for distributing the cooling medium around the experiment chamber 300, so as to effectively absorb heat generated by friction between flowing air and the bulkhead 301. The cooling medium flowing through the outlet end is delivered into the cooling source 501 by the circulation pump 900 to be cooled, and then the next circulation is performed.

When the overweight centrifuge starts to operate, the refrigeration source 501 and/or the cold storage tank 800 deliver the cooling medium through the first cooling medium circulation line 502 and the second cooling medium circulation line 503. When the cooling medium passing through the first cooling medium circulation line 502 flows through the side wall of the experiment chamber 300, the heat generated between the flowing air and the bulkhead 301 and between the rotor 200 and the bulkhead 301 is absorbed, and the cooling medium after absorbing the heat is delivered into the cooling source 501 through the circulation pump 900 to be cooled again. Meanwhile, the condensate absorbs heat generated before the rotor 200 and the flowing air through the heat pipe radiator 602, the condensate after heat absorption is cooled by the cooling medium flowing through the second cooling medium circulation pipeline 503, and the cooling medium heated in the three cooling medium circulation pipelines is also conveyed into the refrigeration source 501 through the circulation pipelines to be cooled. Meanwhile, the vacuum pump 700 is started to reduce the vacuum degree in the experiment chamber 300 so as to reduce the heat generated by the friction of each device.

Second cooling medium and circulating pump 900 also can be saved to this device, adopts the direct refrigerated mode of first cooling medium in second cooling medium circulation pipeline 503, heat dissipation end 603, takes away the heat of experiment under-deck and heat pipe heat dissipation end: at this time, the refrigeration source 501 is equivalent to a refrigerant compressor and a condensation heat dissipation device in a refrigeration system, and the cold storage tank 800 is a high-pressure refrigerant storage tank; the first cooling medium, i.e. the refrigerant, passes through the throttling device, enters the second cooling medium circulation pipeline 503 and the heat dissipation end 603 for direct evaporation and refrigeration, and then enters the next circulation through the refrigeration source 501.

The technical features of the embodiments described above may be arbitrarily combined, and for the sake of brevity, all possible combinations of the technical features in the embodiments described above are not described, but should be considered as being within the scope of the present specification as long as there is no contradiction between the combinations of the technical features. When technical features in different embodiments are represented in the same drawing, it can be seen that the drawing also discloses a combination of the embodiments concerned.

The above-mentioned embodiments only express several embodiments of the present application, and the description thereof is more specific and detailed, but not construed as limiting the claims. It should be noted that, for a person skilled in the art, several variations and modifications can be made without departing from the concept of the present application, which falls within the scope of protection of the present application. Therefore, the protection scope of the present patent shall be subject to the appended claims.