Temperature chamber and method
A temperature chamber for conditioning air includes a temperature-insulated space which receives test material, and a temperature control device for controlling the temperature of the test space. The temperature control device allows a temperature in a range of −50° C. to +180° C. to be established within the space, and has a cooling device including a cooling circuit with a refrigerant, a heat exchanger, a compressor, a condenser, and an expansion element. A jet device is connected to a low-pressure side of the cooling circuit downstream of the heat exchanger and upstream of the compressor, a first bypass is connected to a high-pressure side of the cooling circuit downstream of the compressor, and the refrigerant is suppliable to the jet device from the high-pressure side via the first bypass as a driving fluid.
1. A temperature chamber for conditioning air, in particular a test chamber or the like, comprising a temperature-insulated space which can be closed off from the surroundings and which serves to receive test material and a temperature control device for controlling the temperature of the space, the temperature control device allowing a temperature in a temperature range of −50° C. to +180° C. to be established within the space, the temperature control device having a cooling device comprising a cooling circuit with a refrigerant, a heat exchanger, a compressor, a condenser, and an expansion element, wherein
a jet device is connected to a low-pressure side of the cooling circuit downstream of the heat exchanger and upstream of the compressor, a first bypass being connected to a high-pressure side of the cooling circuit downstream of the compressor, the refrigerant being suppliable to the jet device from the high-pressure side via the first bypass as a driving fluid, wherein the first bypass is connected to the high-pressure side of the cooling circuit upstream of the condenser.
2. The temperature chamber according to claim 1 , wherein the jet device has a drive nozzle, which is connected to the first bypass, and a mixing chamber, the driving fluid being introduced into the mixing chamber in the flow direction of the cooling circuit via the drive nozzle, the mixing chamber forming a conduit section of the cooling circuit of the low-pressure side.
3. The temperature chamber according to claim 1 , wherein the first bypass is provided with at least one first control element.
4. The temperature chamber according to claim 1 , wherein the first bypass is connected to the high-pressure side of the cooling circuit downstream of the condenser.
5. The temperature chamber according to claim 1 , wherein another bypass having at least one other control element is formed in the cooling circuit, the other bypass being connected to the cooling circuit upstream of the jet device and downstream of the heat exchanger and upstream of the compressor and downstream of the jet device and bypassing the jet device.
6. The temperature chamber according to claim 1 , wherein the cooling circuit has an internal heat exchanger, the internal heat exchanger being connected to the high-pressure side of the cooling circuit upstream of the expansion element and downstream of the condenser and to the low-pressure side of the cooling circuit upstream of the compressor and downstream of the heat exchanger, the refrigerant of the high-pressure side being coolable by the refrigerant of the low-pressure side by means of the internal heat exchanger.
7. The temperature chamber according to claim 6 , wherein the internal heat exchanger is connected to the low-pressure side upstream of the compressor and downstream of the jet device.
8. The temperature chamber according to claim 6 , wherein the internal heat exchanger is connected to the low-pressure side upstream of the jet device and downstream of the heat exchanger.
9. The temperature chamber according to claim 1 , wherein the heat exchanger is disposed in the space.
10. The temperature chamber according to claim 1 , wherein the heat exchanger forms a cascade heat exchanger for another cooling circuit of the cooling device.
11. The temperature chamber according to claim 1 , wherein the condenser is realized as a cascade heat exchanger of another cooling circuit of the cooling device.
12. The temperature chamber according to claim 1 , wherein the expansion element and/or a control element has a throttle element and a magnetic valve, refrigerant being meterable via the throttle element and the magnetic valve.
13. A temperature chamber for conditioning air, in particular a test chamber or the like, comprising a temperature-insulated space which can be closed off from the surroundings and which serves to receive test material and a temperature control device for controlling the temperature of the space, the temperature control device allowing a temperature in a temperature range of −50° C. to +180° C. to be established within the space, the temperature control device having a cooling device comprising a cooling circuit with a refrigerant, a heat exchanger, a compressor, a condenser, and an expansion element,
wherein
a jet device is connected to a low-pressure side of the cooling circuit downstream of the heat exchanger and upstream of the compressor, a first bypass being connected to a high-pressure side of the cooling circuit downstream of the compressor, the refrigerant being suppliable to the jet device from the high-pressure side via the first bypass as a driving fluid, and wherein a second bypass having at least one second control element is formed in the cooling circuit, the second bypass being connected to the cooling circuit upstream of the expansion element and downstream of the condenser and bypassing the expansion element, refrigerant being meterable via the second control element in such a manner that a suction gas temperature and/or a suction gas pressure of the refrigerant on the low-pressure side of the cooling circuit is controllable upstream of the compressor.
14. The temperature chamber according claim 13 , wherein the second bypass is connected to the cooling circuit downstream of the heat exchanger and upstream of the jet device.
15. The temperature chamber according to claim 13 , wherein the second bypass is connected to the first bypass.
16. A method for conditioning air in a temperature-insulated space of a temperature chamber, in particular a test chamber or the like, which can be closed off from the surroundings and which serves to receive test material, a temperature in a temperature range of −50° C. to +180° C. being established within the space by means of a cooling device of a temperature control device of the temperature chamber, comprising a cooling circuit with a refrigerant, a heat exchanger, a compressor, a condenser and an expansion element, wherein
a jet device is connected to a low-pressure side of the cooling circuit downstream of the heat exchanger and upstream of the compressor, the refrigerant being supplied to the jet device from the high-pressure side as a driving fluid via a first bypass connected to a high-pressure side of the cooling circuit downstream of the compressor, and wherein a second bypass having at least one second control element is formed in the cooling circuit, the second bypass being connected to the cooling circuit upstream of the expansion element and downstream of the condenser and bypassing the expansion element, refrigerant being meterable via the second control element in such a manner that a suction gas temperature and/or a suction gas pressure of the refrigerant on the low-pressure side of the cooling circuit is controllable upstream of the compressor.
17. The method according to claim 16 , wherein the driving fluid is introduced into a mixing chamber of the jet device in the flow direction of the cooling circuit via a drive nozzle of the jet device, said drive nozzle being connected to the first bypass, the refrigerant being aspirated into the mixing chamber as a suction fluid upstream of the jet device and being ejected from the mixing chamber downstream of the jet device at a higher pressure than that of the suction fluid.