Test chamber and method
A method for conditioning a fluid in a temperature-insulated test space and a test space of a test chamber for receiving test materials. A cascading cooling device creates a particular temperature range within the test space, and the cooling device has a first cooling circuit including a cascading heat exchanger, a first compressor, a condenser and a first expanding element, and a second cooling circuit including a heat exchanger, a second compressor, the cascading heat exchanger and a second expanding element The cascading heat exchanger is cooled by the first cooling circuit, the heat exchanger is cooled by a bypass passing through the heat exchanger and bridging the cascading heat exchanger, the first compressor is turned off, and a first refrigerant is conducted and condensed in a gaseous state in the cascading heat exchanger on a low-pressure side of the bypass.
1. A method for conditioning a fluid in a temperature-insulated test space ( 14 ) of a test chamber for receiving test materials, said test space ( 14 ) being sealable against an environment and having a temperature ranging from −60° C. to +180° C. realized within the test space by a cascading cooling device ( 10 ) of a temperature controller of the test space, the test space having a first cooling circuit ( 11 ) having a first refrigerant, a cascading heat exchanger ( 15 ), a first compressor ( 16 ), a condenser ( 17 ) and a first expander ( 18 ), and having a second cooling circuit ( 12 ) having a second refrigerant, a heat exchanger ( 13 ) arranged in the test space, a second compressor ( 27 ), the cascading heat exchanger and a second expander ( 28 ), said cascading heat exchanger being cooled by the first cooling circuit, wherein the method comprises cooling the heat exchanger by a bypass ( 35 ) of the first cooling circuit by the first cooling circuit, said bypass passing through the heat exchanger and bridging the cascading heat exchanger, the first compressor being turned off, the first refrigerant being conducted and condensed in a gaseous state in the cascading heat exchanger on a low-pressure side ( 22 ) of the bypass.
2. The method according to claim 1 , wherein a expander ( 36 ) is arranged in the bypass ( 35 ) and liquid first refrigerant from a high-pressure side ( 21 ) of the first cooling circuit is expanded to gaseous first refrigerant in the first cooling circuit ( 11 ) by the third expander and is conducted to the low-pressure side ( 22 ) via the heat exchanger ( 13 ).
3. The method according to claim 2 , wherein the second compressor ( 27 ) is stopped in a first step, the first compressor ( 16 ) being operated for condensing first refrigerant from a high-pressure side ( 21 ) of the first cooling circuit being expanded to gaseous first refrigerant in the first cooling circuit ( 11 ) by the first expander ( 18 ) and being conducted to the low-pressure side ( 22 ) via the cascading heat exchanger.
4. The method according to claim 3 , wherein thermal energy is emitted from the second refrigerant of the second cooling circuit ( 12 ) to the first refrigerant of the first cooling circuit ( 11 ) and is stored in the cascading heat exchanger ( 15 ).
5. The method according to claim 3 , wherein the first compressor ( 16 ) is turned off in a second step, and a difference in pressure is realized in the cascading heat exchanger ( 15 ) between the low-pressure side ( 22 ) and the high-pressure ( 21 ) by the first refrigerant condensing to the liquid first refrigerant.
6. The method according to claim 5 , wherein liquid first refrigerant from the high-pressure side ( 21 ) of the first cooling circuit is expanded to gaseous first refrigerant in the first cooling circuit ( 11 ) by a third expander ( 36 ) and is conducted to the low-pressure side ( 22 ) via the heat exchanger ( 13 ).
7. The method according to claim 5 , wherein the first compressor ( 16 ) is operated in a third step, and a pressure on the low-pressure side ( 22 ) is reduced enough for the liquid first refrigerant to be evaporated to gaseous first refrigerant in the cascading heat exchanger ( 15 ).
8. The method according to claim 5 , wherein first refrigerant is supplied to the low-pressure side via a fourth expander by an adjustable first internal supplementary refrigeration line ( 37 ) in the first cooling circuit ( 11 ), having a second bypass ( 38 ), which is connected to a high-pressure side ( 21 ) in the flow direction upstream of the first expanding element ( 18 ) and downstream of the condenser ( 17 ) and is connected to the low-pressure side ( 22 ) in the flow direction upstream of the first compressor ( 16 ) and downstream of the cascading heat exchanger ( 15 ), and the fourth expander ( 39 ).
9. The method according to claim 8 , wherein refrigerant is supplied to the low-pressure side via a fifth expander by an adjustable second internal supplementary refrigeration line ( 40 ) in the second cooling circuit ( 12 ), having a third bypass ( 41 ), which is connected to a high-pressure side ( 29 ) in the flow direction upstream of the second expander ( 28 ) and downstream of the cascading heat exchanger ( 15 ) and is connected to the low-pressure side ( 30 ) in the flow direction upstream of the second compressor ( 27 ) and downstream of the heating exchanger ( 13 ), and by the fifth expander ( 42 ).
10. The method according to claim 9 , wherein first refrigerant is supplied to the low-pressure side via a sixth expander by an adjustable first back-injector ( 43 ) for first refrigerant in the first cooling circuit ( 11 ), having a fourth bypass ( 44 ), which is connected to a high-pressure side ( 21 ) in the flow direction downstream of the first compressor ( 16 ) and upstream of the condenser ( 17 ) and is connected to the low-pressure side ( 22 ) in the flow direction upstream of the first compressor and downstream of the cascading heat exchanger ( 15 ), and by the sixth expander ( 45 ).
11. The method according to claim 10 , wherein second refrigerant is supplied to the low-pressure side via a seventh expander by an adjustable second back-injector ( 46 ) for second refrigerant in the second cooling circuit ( 12 ), having a fifth bypass ( 47 ), which is connected to a high-pressure side ( 29 ) in the flow direction downstream of the second compressor ( 27 ) and upstream of the cascading heat exchanger ( 15 ) and is connected to the low-pressure side ( 30 ) in the flow direction upstream of the second compressor and downstream of the heat exchanger ( 13 ), and by the seventh expander ( 48 ).
12. The method according to claim 11 , wherein the temperature controller comprises an adjuster having at least one pressure sensor or at least one temperature sensor in cooling circuits ( 11 , 12 ), and magnetic valves ( 20 ) of each expander ( 18 , 28 , 36 , 39 , 42 , 45 , 48 ) are actuated by the adjuster as a function of a measured temperature or pressure.
13. The method according to claim 1 , wherein a suction gas temperature and/or a suction gas pressure of the first and/or second refrigerant is adjusted on a low-pressure side ( 22 , 30 ) of the cooling circuits ( 11 , 12 ) upstream of compressors ( 16 , 27 ), or in that a difference in pressure is compensated between a high-pressure side ( 21 , 29 ) and the low-pressure side of the cooling circuits.
14. The method according to claim 1 , wherein a temperature ranging from −70° C. to +180° C. is realized within the test space ( 14 ) by the temperature controller.