This disclosure relates generally to a magnetic resonance imaging (MRI) system, and more particularly to a superconducting magnet cooling system.
This disclosure relates generally to a magnetic resonance imaging (MRI) system, and more particularly to a superconducting magnet cooling system.
As is well known, a superconducting magnet can be made superconducting by placing it in an extremely cold environment, such as by enclosing it in a cryostat or pressure vessel containing liquid helium or other liquid cryogen. A cryorefrigerator is widely used to keep a cryogenic temperature. The extreme cold can ensure that the magnet coils are maintained in superconducting operation, such that when a power source is initially connected to the magnet coils (for a period, for example, of 10 minutes) to introduce a current flow through the coils, the current will continue to flow through the coils even after the power source is removed due to the absence of electrical resistance in the coils, thereby maintaining a strong magnetic field. Superconducting magnet cooling system finds wide application in the field of MRI.
However, when the cryorefrigerator is in operation, the cryorefrigerator may introduce mechanical vibrations which can also affect image quality of MRI. In a conventional superconducting magnet cooling system, a second stage of the cryorefrigerator is usually rigidly connected to a recondenser and bellow tubes are used to provide vibration isolation of the recondenser from the superconducting magnet. But the bellow tubes cannot endure high pressure, only low pressure cryogen can be used in cooling the superconducting magnet, so the conventional superconducting magnet cooling system limits the superconducting magnet cooling to low pressure cryogen.
In one aspect of embodiments of the present invention, a superconducting magnet cooling system is provided. The superconducting magnet cooling system comprises a superconducting magnet; a liquid cryogen vessel for cooling the superconducting magnet; a heat exchanger device in fluid communication with the liquid cryogen vessel; a cryorefrigerator for heat exchange with the heat exchanger device; and a flexible connection device having high thermal conductivity and thermally connecting the cryorefrigerator and the heat exchanger device to provide vibration isolation of the cryorefrigerator from the heat exchange device.
These and other features, aspects, and advantages of the present disclosure will become better understood when the following detailed description is read with reference to the accompanying drawings in which like characters represent like parts throughout the drawings, wherein:
Embodiments of the present disclosure will be described hereinbelow with reference to the accompanying drawings. In the following description, well-known functions or constructions are not described in detail to avoid obscuring the disclosure in unnecessary detail.
Unless defined otherwise, technical and scientific terms used herein have the same meaning as is commonly understood by one of ordinary skill in the art to which this disclosure belongs. The terms “first”, “second”, and the like, as used herein do not denote any order, quantity, or importance, but rather are used to distinguish one element from another. Also, the terms “a” and “an” do not denote a limitation of quantity, but rather denote the presence of at least one of the referenced items. The term “or” is meant to be inclusive and mean either or all of the listed items. The use of “including,” “comprising” or “having” and variations thereof herein are meant to encompass the items listed thereafter and equivalents thereof as well as additional items.
In this embodiment, the liquid cryogen vessel 2 may be for example a liquid helium storage 2 which may be formed from one or more liquid helium reservoirs, and the heat exchanger device 3 may be for example a remote recondenser 3. The fluid communication between the recondenser 3 and the liquid helium storage 2 may be provided via one or more passageways 91.
With reference to
Continuing to refer to
The recondenser 3 draws He gas from the helium gas storage 6 that operates to form a free convection circulation loop to cool the superconducting magnet coils 14 and the coil support shell 12 to a cryogenic temperature, as well as fills the liquid helium storage 2 with liquid He via one or more passageways 91. The liquid He in the liquid helium storage 2 may be used to provide cooling of the superconducting magnet coils 14 during power interruptions or shut down of the cryorefrigerator 4, such as for service (e.g., for 10-12 hours).
As shown in
In the superconducting magnet cooling system 100 of the present invention having two stage cooling arrangement, cooling with the thermal shield 7 may provide a first stage of cooling by direct contact with the first stage of the cryorefrigerator 4 at a temperature of about 40-50 K and may also provide pre-cooling for example, at a temperature between about 77 K and 80 K using the LN2. The second stage of cooling is provided using the He cooling so as to provide an operation temperature of about 4.2 K.
The superconducting magnet cooling system 100 is located within a vacuum vessel 8. The cryorefrigerator 4 comprises a coldhead (not shown), a motor 42 for driving the coldhead to operate, and a coldhead sleeve 44. The coldhead of the cryorefrigerator 4 may be positioned within the coldhead sleeve 44 without affecting the vacuum within the vacuum vessel 8. The coldhead of the cryorefrigerator 4 is inserted (or received) and secured with the coldhead sleeve 44 using any suitable means, such as one or more flanges and bolts, or other suitable means. Moreover, the motor 42 of the cryorefrigerator 4 is provided outside the vacuum vessel 8.
Because the reconderser 3 and the cryorefrigerator 4 are thermally connected via the flexible connection device 5, all of the passageways 91, 92, 94 and the vapor return manifold 93 use a rigid high pressure piping so that the superconducting magnet cooling system 100 may be hermetically sealed with high pressure charged helium gas which is cooled directly by the cryorefrigerator 4 from an ambient temperature to a cryogenic temperature.
Referring to
The flexible connection device 5 is made of braid structure for providing a flexible connection. In one embodiment, the flexible connection device 5 comprises copper braids.
In the superconducting magnet cooling system 100 of the present invention, by adopting the flexible connection device 5 having high thermal conductivity, not only a thermal connection between the cryorefrigerator 4 and the recondenser 3 is established, but also vibration isolation of the cryorefrigerator 4 from the recondenser 3 is also provided because of flexibility of the flexible connection device 5. Therefore, the vibration of the cryorefrigerator 4 cannot be transmitted to the superconducting magnet 1. The vibration isolation of the superconducting magnet 1 can be accomplished by the flexible connection device 5 thermally connecting the cryorefrigerator 4 to the recondenser 3.
Furthermore, because the reconderser 3 and the cryorefrigerator 4 are thermally connected via the flexible connection device 5, this design of the superconducting magnet cooling system 100 enables the use of high pressure piping between the liquid cryogen vessel 2 and superconducting magnet 1 that is inherently rigid and is able to use a hermetically sealed high pressure charged helium gas which is cooled directly by the cryorefrigerator 4 from the ambient temperature to the cryogenic temperature.
While the disclosure has been illustrated and described in typical embodiments, it is not intended to be limited to the details shown, since various modifications and substitutions can be made without departing in any way from the spirit of the present disclosure. As such, further modifications and equivalents of the disclosure herein disclosed may occur to persons skilled in the art using no more than routine experimentation, and all such modifications and equivalents are believed to be within the spirit and scope of the disclosure as defined by the following claims.
Number | Date | Country | Kind |
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201510236104.7 | May 2015 | CN | national |
This is a national stage application under 35 U.S.C. § 371 (c) of PCT Patent Application No. PCT/US2016/029713, filed on Apr. 28, 2016, which claims priority to Chinese Patent Application No. 201510236104.7, filed on May 11, 2015, the disclosures of which are incorporated herein by reference in their entireties.
Filing Document | Filing Date | Country | Kind |
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PCT/US16/29713 | 4/28/2016 | WO | 00 |