METHOD AND DEVICE FOR PRECOOLING A CRYOSTAT
20170051874 ยท 2017-02-23
Inventors
Cpc classification
F17C3/08
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
G01R33/3804
PHYSICS
F17C3/085
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C13/007
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F25B9/10
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F25D19/006
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F25B2400/17
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
International classification
Abstract
A method is provided for precooling a cryostat having a hollow cold head turret into which a neck tube protrudes and connects an object to be cooled to the exterior of the cryostat, wherein a cold head having a cold head stage for cooling a cryogenic working medium may be introduced into the neck tube. During a condensation operation the cryogenic working medium flows through a heat pipe into an evaporator chamber which is thermally conductively connected to the object to be cooled. During a precooling phase a precisely fitting, thermally conductive short circuit block is inserted through the neck tube into the heat pipe to provide thermal conduction between the object to be cooled and a cooling device The short circuit block is removed from the heat pipe after the target temperature is reached, and heat is subsequently transmitted through the heat pipe during a condensation operation.
Claims
1. A method for operating a cryostat, comprising a vacuum container which houses a chamber containing at least one object to be cooled, the vacuum container having at least one hollow cold head turret which contains a neck tube which connects the chamber through the outer shell of the vacuum container to the area outside of the cryostat, the neck tube being geometrically configured in such a way that a cold head may be introduced, the cold head having a cold head stage via which a cryogenic working medium, which flows or drips through a heat pipe into an evaporator chamber during a condensation operation, may be cooled, and which is thermally conductively connected to the object to be cooled via a thermal contact surface, so that the cooled cryogenic working medium is able to absorb heat from the object to be cooled and transport it to the cold head stage via the heat pipe, wherein during a precooling phase the object to be cooled is precooled to a target temperature of the working range of the cryogenic working medium in which the heat pipe is able to operate efficiently, wherein for the precooling, a precisely fitting short circuit block with good thermal conductivity is inserted through the neck tube into the heat pipe, one free end of the short circuit block being thermally connected to a high-power cooling device, and its other end contacting the thermal contact surface, and in an intermediate phase the short circuit block is removed from the heat pipe after the target temperature is reached, and during an operating phase, heat is subsequently transmitted through the heat pipe during a condensation operation.
2. The method according to claim 1, wherein the cryogenic working medium is blown into the inner space of the neck tube during the removal of the short circuit block from the neck tube in the intermediate phase, and during insertion/placement of the cooling device or the cold head through the neck tube at the start of the operating phase, so that the heat pipe is loaded with the cryogenic working medium.
3. The method according to claim 1, wherein the cryogenic working medium is selected from helium, neon, nitrogen, hydrogen, or carbon dioxide, depending on the temperature range to be reached in the operating phase.
4. The method according to claim 1, wherein, in the intermediate phase, the high-power cooling device having the short circuit block is exchanged with a two-stage cryocooler having a cold head stage.
5. A cryostat for carrying out the method according to claim 1, wherein a gas supply device for blowing the cryogenic working medium into the shared inner space of the neck tube, heat pipe, and evaporator chamber is present, so that a gas flow in the direction of the neck tube may be provided which prevents air and/or moisture from penetrating into the cryostat during the removal of the short circuit block from the neck tube during the intermediate phase, and during insertion of the heat pipe through the neck tube at the start of the operating phase, and which at the same time loads the heat pipe.
6. The cryostat according to claim 5, wherein a sealing device is present which prevents gas exchange from the heat pipe to the ambient air.
7. The cryostat according to claim 5, wherein the short circuit block is manufactured so that its outer circumference makes a precise geometric fit with the outer circumference of the heat pipe.
8. The cryostat according to claim 5, wherein the short circuit block is made of a material having a thermal conductivity of >200 W/m.Math.K, in particular copper or aluminum.
9. The cryostat according to claim 5, wherein the high-power cooling device is protected from undesirable external heat input by a vacuum device and/or an insulating jacket.
10. The cryostat according to claim 5, wherein a tank containing liquid helium is present, with which the thermal contact surface may be cooled with respect to the object to be cooled, but the object to be cooled itself is not situated in a tank containing liquid helium.
11. The cryostat for carrying out the method according to claim 1, wherein the high-power cooling device has a cooling power of at least 300 W, preferably at least 500 W, at 80 K.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
[0035] The invention is illustrated in the drawings and is explained in greater detail with reference to exemplary embodiments, as follows:
[0036]
[0037]
[0038]
[0039]
DETAILED DESCRIPTION
[0040]
[0041] All cryostats illustrated in the drawings have a vacuum container which houses a chamber containing at least one object 10; 10 to be cooled, the vacuum container having at least one hollow cold head turret 12 into which a neck tube 4, which connects the chamber through the outer shell 8; 8 of the vacuum container to the area outside of the cryostat, protrudes, the neck tube 4 being geometrically configured in such a way that a cold head 1 may be introduced, the cold head having a (generally, second) cold head stage 7 via which a cryogenic working medium, which flows or drips through a heat pipe 5 into an evaporator chamber 6 during a condensation operation, may be cooled, and which is thermally conductively connected to the object 10; 10 to be cooled via a thermal contact surface 9; 9, so that the cooled cryogenic working medium is able to absorb heat from the object 10; 10 to be cooled and transport it to the cold head stage 7 via the heat pipe 5.
[0042] The chamber containing the object 10; 10 to be cooled is surrounded by a radiation shield 2; 2 inside the vacuum container.
[0043] A connection 11 having good thermal conductivity is provided between the radiation shield 2; 2 and a first stage of the cold head 1.
[0044] The object 10; 10 to be cooled is generally a superconducting NMR coil system mounted on or in a coil body 3.
[0045] According to the invention, in the cryostats shown in
[0046] The cryogenic working medium is blown into the inner space of the neck tube 4 during the removal of the short circuit block 14 from the neck tube 4 in the intermediate phase, and during insertion/placement of the cooling device 13 or the cold head 1 through the neck tube 4 at the start of the operating phase, so that the heat pipe 5 is loaded with the cryogenic working medium.
[0047] The cryogenic working medium is selected from helium, neon, nitrogen, hydrogen, or carbon dioxide, depending on the temperature range to be reached in the operating phase.
[0048] In the intermediate phase, the high-power cooling device 13 having the short circuit block 14 is replaced by a two-stage cryocooler having a cold head stage 7.
[0049] The cryostat according to the invention is characterized in that a gas supply device 15 for blowing the cryogenic working medium into the shared inner space of the neck tube 4, heat pipe 5, and evaporator chamber 6 is present, so that a gas flow in the direction of the neck tube may be provided which prevents air and/or moisture from penetrating into the cryostat during the removal of the short circuit block 14 from the neck tube 4 during the intermediate phase, and during insertion of the heat pipe 5 through the neck tube 4 at the start of the operating phase, and which at the same time loads the heat pipe 5.
[0050] A sealing device is generally present which prevents gas exchange from the heat pipe 5 to the ambient air.
[0051] The short circuit block 14 is made of a material having a thermal conductivity of >200 W/m.Math.K, in particular copper or pure aluminum, so that its outer circumference makes a precise geometric fit with the outer circumference of the heat pipe 5.
[0052] The high-power cooling device 13 has a cooling power of at least 300 W, preferably at least 500 W, at 80 K, and is protected from undesirable external heat input by a vacuum device and/or an insulating jacket, since the cooling device protrudes from the neck tube, and in this area must be shielded from lateral heat input from the surroundings.
[0053] In the embodiments of the invention illustrated in the drawings, a tank containing liquid helium is present, with which the thermal contact surface 9; 9 may be cooled with respect to the object 10; 10 to be cooled, but the object 10; 10 to be cooled itself is not situated in a tank containing liquid helium.
[0054] In the embodiment shown in
[0055] In comparison,
[0056] The embodiments of the cryostat according to the invention illustrated in
[0057]
[0058] In one advantageous design, the high-power cooling device 13 is a Stirling cooler, not a Gifford-McMahon cooler. These coolers are even more efficient, but require a dedicated compressor and are more costly.
[0059] The high-power cooling device 13 and the pulse tube cooler are preferably operated with the same compressor unit.
LIST OF REFERENCE NUMERALS
[0060] 1 Cold head [0061] 2; 2 Radiation shield [0062] 3 Coil body [0063] 4 Neck tube [0064] 5 Heat pipe [0065] 6 Evaporator chamber [0066] 7 Cold head stage (second stage) [0067] 8; 8 Outer shell [0068] 9; 9 Thermal contact surface [0069] 10; 10Object to be cooled [0070] 11 Radiation shield-cold head connection (first stage) [0071] 12 Cold head turret [0072] 13 Cooling device [0073] 14 Short circuit block [0074] 15 Gas supply device