GB2455720A - Reworkable pressure vessel for a superconducting magnet - Google Patents

Reworkable pressure vessel for a superconducting magnet Download PDF

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Publication number
GB2455720A
GB2455720A GB0724573A GB0724573A GB2455720A GB 2455720 A GB2455720 A GB 2455720A GB 0724573 A GB0724573 A GB 0724573A GB 0724573 A GB0724573 A GB 0724573A GB 2455720 A GB2455720 A GB 2455720A
Authority
GB
United Kingdom
Prior art keywords
vessel
welding
fusion bonding
union
pressure vessel
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Granted
Application number
GB0724573A
Other versions
GB2455720B (en
GB0724573D0 (en
Inventor
Mark James Le Feuvre
Edgar Charles Malcolm Rayner
Matthew Hobbs
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Siemens PLC
Original Assignee
Siemens Magnet Technology Ltd
Siemens PLC
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Siemens Magnet Technology Ltd, Siemens PLC filed Critical Siemens Magnet Technology Ltd
Priority to GB0724573A priority Critical patent/GB2455720B/en
Publication of GB0724573D0 publication Critical patent/GB0724573D0/en
Priority to PCT/GB2008/051156 priority patent/WO2009077780A1/en
Priority to CNA200810184998XA priority patent/CN101464476A/en
Priority to US12/337,308 priority patent/US20090162584A1/en
Publication of GB2455720A publication Critical patent/GB2455720A/en
Application granted granted Critical
Publication of GB2455720B publication Critical patent/GB2455720B/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C13/00Details of vessels or of the filling or discharging of vessels
    • F17C13/005Details of vessels or of the filling or discharging of vessels for medium-size and small storage vessels not under pressure
    • F17C13/006Details of vessels or of the filling or discharging of vessels for medium-size and small storage vessels not under pressure for Dewar vessels or cryostats
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01RMEASURING ELECTRIC VARIABLES; MEASURING MAGNETIC VARIABLES
    • G01R33/00Arrangements or instruments for measuring magnetic variables
    • G01R33/20Arrangements or instruments for measuring magnetic variables involving magnetic resonance
    • G01R33/28Details of apparatus provided for in groups G01R33/44 - G01R33/64
    • G01R33/38Systems for generation, homogenisation or stabilisation of the main or gradient magnetic field
    • G01R33/3804Additional hardware for cooling or heating of the magnet assembly, for housing a cooled or heated part of the magnet assembly or for temperature control of the magnet assembly
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01RMEASURING ELECTRIC VARIABLES; MEASURING MAGNETIC VARIABLES
    • G01R33/00Arrangements or instruments for measuring magnetic variables
    • G01R33/20Arrangements or instruments for measuring magnetic variables involving magnetic resonance
    • G01R33/28Details of apparatus provided for in groups G01R33/44 - G01R33/64
    • G01R33/38Systems for generation, homogenisation or stabilisation of the main or gradient magnetic field
    • G01R33/381Systems for generation, homogenisation or stabilisation of the main or gradient magnetic field using electromagnets
    • G01R33/3815Systems for generation, homogenisation or stabilisation of the main or gradient magnetic field using electromagnets with superconducting coils, e.g. power supply therefor
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01FMAGNETS; INDUCTANCES; TRANSFORMERS; SELECTION OF MATERIALS FOR THEIR MAGNETIC PROPERTIES
    • H01F6/00Superconducting magnets; Superconducting coils
    • H01F6/04Cooling
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00Stock material or miscellaneous articles
    • Y10T428/13Hollow or container type article [e.g., tube, vase, etc.]

Abstract

A pressure vessel or a method of making a pressure vessel, suitable for a superconducting magnet, comprises first and second parts made from fibre-reinforced thermoplastic which are able to be repeatedly bonded together and/or separated apart by the application of a thermal process. The thermal process can be used to open or close the vessel such that the vessel can be reworked if a fault in the vessel assembly is identified. This can provide savings in the processing time required and the levels of waste material generated during the production of such an assembly. The thermoplastic material may be polypropylene or polyethylene. The thermoplastic material may be suitable for recycling via granulation and moulding processes. The thermal process may be hot tool welding, infra-red welding, laser welding, spin welding, ultrasonic welding, vibration welding or resistance welding forms of fusion bonding. The same or a different thermal process may be used for the bonding and separation of the vessel parts.

Description

RE-WORKABLE PRESSURE VESSELS FOR SUPERCONDUCTING MAGNET
ARRANGEMENTS.
This invention relates to re-workable pressure vessels for superconducting magnet arrangements, and to methods of making such vessels. It relates especially, though not exclusively, to pressure vessels utilised in magnetic resonance imaging (MRI) systems.
It is well known that, in order to fully test the superconducting magnets which are used in MRI systems, they need to be sealed, as for operation, in a cryostatic environment, within a pressure vessel, usually referred to as an outer vacuum chamber (OVC), which provides thermal isolation from room temperature.
Ideally, if the test is successful, the OVC and the cryogenic magnet assembly which it contains can be fitted into the MRI system for which it is intended. If, however, the test is unsuccessful, the chamber has to be opened in order to provide access to facilitate the repair or re-working of the magnets.
Where the OVC is made of metallic material, it is usual for the sealing to be effected by welding, and opening such an OVC requires the welds to be cut.
Since this removes material from the vicinity of the welds, the original OVC cannot generally be re-used and, whilst some at least of the metallic material can be recycled, and does not therefore pose a significant disposal problem, as regards landfill for example, the operation as a whole is wasteful of material and rather costly. In this latter respect, it will be appreciated that the time and cost involved in the assembly of a metallic OVC is considerable, requiring several hours of skilled coded weld time.
It has thus been proposed to fabricate OVC enclosures from fibre-reinforced composite thermoseffing plastics materials. However, OVCs so fabricated need, like their metallic counterparts, to be cut open when testing indicates that magnet repairs are called for, and the situation is thus little improved. Furthermore the OVC, having been cut open, cannot be re-used and the scrapped OVC has to be disposed of. Fibre-reinforced thermosetting plastics materials are generally non-recyclable, however, and it is becoming increasingly unacceptable, as well as expensive, to send such materials to landfill sites for disposal.
It will further be appreciated that, whether or not a magnet system contained in an OVC made of thermosetting plastics needs re- working after test, the problem of acceptably disposing of the OVC still arises at the end of the product's working life.
There are thus requirements for improved demountable pressure vessels for superconducting magnet arrallgements and for improved methods of manufacturing, opening and re-closing such vessels, and it is an object of the present invention to address these requirements.
According to the invention from one aspect, there is provided a reworkable pressure vessel adapted to contain superconducting magnet arrangements; at least first and second separate parts of the vessel being fabricated from fibre-reinforced thermoplastic material; wherein said first and second parts comprise facing end surfaces adapted for fusion bonding together to form a union closing said vessel such that said vessel can be opened and re-closed by repeated application of fusion bonding to said union. Parts of such pressure vessels are thus readily secured together by --3-means of fusion bonding, which is a reversible process, thereby permitting the vessel to be opened so as to provide access to superconducting magnet components enclosed therein, and its subsequent re-closure, again by fusion bonding.
D
In some preferred embodiments, the fusion bonding processes used to open and/or re-close the vessel comprises a re-application of the same process used to effect the original bond. In other embodiments, different fusion bonding processes from that used for the original bond may be used for opening and/or re-closure.
It is preferred that the fusion bonding process used is chosen from a group of processes comprising: hot tool welding; infra-red welding; laser welding; spin welding; ultrasonic welding; vibration welding; and resistance welding.
It is preferred that the thermoplastics material comprises polypropylene or polyethylene.
In some preferred embodiments, at least an outer shell of the pressure vessel is formed entirely of said reinforced thermoplastics material.
The invention thus provides that pressure vessels opened to permit the repair of magnets that fail during testing can be re-sealed. Moreover, pressure vessels constructed of fibre reinforced thermoplastics materials can be recycled at the end of the product life using standard plastic recycling methods. One example of such a method comprises the removal of any metallic inserts followed by grinding of the remaining fibres and plastics material which is then shredded into small pieces and fed into a granulator, ultimately producing small pellets that can be used as raw material in a standard extrusion/compression moulding apparatus.
According to the invention from another aspect, there is provided a method of manufacturing a pressure vessel that can subsequently be opened and re-closed, and which is adapted to contain superconducting magnet arrangements, the method comprising the steps of: fabricating first and second separate parts of the vessel from fibre-reinforced thermoplastjcs material; said first and second parts comprising facing end surfaces adapted to abut in fitting relationship; fusion bonding said abutting end surfaces together to form a union closing said vessel; and repeatedly applying thermal bonding to said union to open and re-close said vessel.
In order that the present invention may be clearly understood and readily carried into effect, one embodiment thereof will now be described.
In accordance with* one example of the invention from one aspect, a reworkable pressure vessel formed with or containing internal fitments associated with the retention and operation of a superconducting magnet arrangement, and thus constituting an OVC, comprises two identical housing parts, both made entirely of fibre-reinforced thermoplastics material. Essentially, the two parts each form a half of the OVC, and they are formed with identical end surfaces designed to accurately match one another, and to be placed into abutting relationship when the OVC is to be closed.
Upon closure, these end surfaces are fusion bonded together to form a union closing the OVC, which can then be submitted to tests in the usual way to determine, inter alia, the functional and operational status of the magnet assembly housed therein.
The thermal bonding process used to form the union is reversible and thus, in accordance with a principal feature of the invention, the OVC can be opened and re-closed by repeated application of fusion bonding to the union. Such pressure vessels are thus readily opened, so as to provide access to the superconducting magnet components enclosed therein for repair or reconfiguration, and subsequently re-closed, again by the application of fusion bonding without loss or damage to the existing vessel components.
The fusion bonding process comprises an application of heat to the two abutting surfaces to be united, and a suitably timed application of pressure by means of opposing forces. These operations are well known to those skilled in the art, and are readily applied to the present context.
Typical fusion bonding processes usable in embodiments of the invention include: hot tool welding; infra-red welding; laser welding; spin welding; ultrasonic welding; vibration welding; and resistance welding. In this connection, it will be appreciated that the process used at any stage, and in any given embodiment of the invention, may be dictated by factors such as the dimensions of the OVC, by operational requirements or simply by process availability and/or by the degree of familiarity of available personnel with certain processes.
Indeed, in some embodiments, the fusion bonding process used to open and/or re-close the vessel may comprise a re-application of the same process used to effect the original bond. In other embodiments, however, different fusion bonding processes from that used for the original bond may be used for opening and/or re-closure.
It is preferred that the thermoplastics material comprises polypropylene or polyethylene. The fibre reinforcement preferably comprises multidirectional fibre matting in order to cope with the forces which a pressure vessel adapted to contain a superconducting magnet is subjected to.
The two halves of the OVC described above are preferably formed entirely of said reinforced thermoplastics material. If operational or other requirements so dictate, however, the OVC may contain, or be partially formed of, metallic or other materials.
As previously mentioned, pressure vessels constructed of fibre reinforced thermoplastics materials can be recycled at the end of the product life using standard plastic recycling methods.
The invention further provides a method of manufacturing a pressure vessel that can subsequently be opened and re-closed, and which is adapted to contain superconducting magnet arrangements. In one embodiment, the method requires fabricating, from fibre-reinforced thermoplastics material, first and second separate parts of the vessel, the parts having respective facing end surfaces; bringing the end surfaces into abutting relationship; fusion bonding the abutting end surfaces together to form a union closing the vessel; and repeated applications of fusion bonding to the union to open and re-close the vessel.
While polypropylene and polyethylene have been suggested as suitable thermoplastic materials, other thermoplastic materials may be employed, according to the required mechanical strength and thermal properties of the vessel. Similarly, the fibre reinforcement will typically comprise glass fibres, but may alternatively or in addition comprise carbon fibres, aramid fibres or any other fibrous material considered to have suitable thermal and mechanical properties.
It has been proposed, in WO 2003/031860 Al, to construct a laminated pressure vessel, such as a water storage tank, from a cylindrical portion and two somewhat hemispherical end caps; each portion comprising an inner layer of non fibre-reinforced thermoplastics material and an outer layer of fthre-reinforced thermoplastics material. The portions are jointed together by thermal bonding but, although access to the interior of the tank is needed in some embodiments, no consideration is given to opening the joints and re-closing them. Rather, access is provided through an opening in one of the end caps. However, the descrthed vessel is very specific to water containment including bafflers and internal features designed specifically for holding water. The body of the tank is formed by filament winding. The present invention prefers the use of fibre matting, rather than wound continuous filaments.

Claims (11)

  1. CLAIMS: 1. A reworkable pressure vessel adapted to contain superconducting magnet arrangement; at least first and second separate parts of the vessel being fabricated from fibre-reinforced thermoplastics material; wherein said first and second parts comprise facing end surfaces adapted for fusion bonding together to form a union closing said vessel such that said vessel can be opened and re-closed by repeated application of fusion bonding to said union.
  2. 2. A vessel according to claim 1, wherein the thermoplastics material comprises polypropylene or polyethylene.
  3. 3. A vessel according to claim 1 or claim 2, wherein the fusion bonding process used to form said union is chosen from the group comprising: hot tool welding; infra-red welding; laser welding; spin welding; ultrasonic welding; vibration welding; and resistance welding.
  4. 4. A vessel according to claim 3, wherein the same fusion bonding process used to form said union is utilised for one at least of said repeated applications.
  5. 5. A vessel according to any preceding claim, wherein at least an outer shell of the pressure vessel is formed entirely of said reinforced thermoplastics material.
  6. 6. A reworkable pressure vessel substantially as herein described and adapted to contain superconducting magnet arrangements.
  7. 7. A method of manufacturing a pressure vessel that can subsequently be opened and re-closed, and which is adapted to contain superconducting magnet arrangements, the method comprising the steps of: fabricating first and second separate parts of the vessel from fibre-reinforced thermoplastics material; said first and second parts comprising facing end surfaces adapted to abut in fitting relationship; fusion bonding said abutting end surfaces together to form a union closing said vessel; and repeatedly applying thermal bonding to said union to open and re-close said vessel.
  8. 8. A method according to claim 7, wherein the fusion bonding process used to open and/or re-close the vessel comprises a re- application of the same process used to effect the original bond.
  9. 9. A method according to claim 7, wherein a different fusion bonding process from that used for the original bond is used for opening and/or re-closure of the vessel.
  10. 10. A method according to any of claims 7 to 9, further comprising recycling the material of the vessel to produce pellets that can be used as raw material in a standard extrusion/compression moulding apparatus.
  11. 11. A method according to claim 10 wherein the step of recycling comprises the steps of removing any metallic inserts; grinding of the remaining fibres and plastics material, thereby shredding them into small pieces; and feeding said small pieces into a granulator.
    11. A method according to claim 10 wherein the step of recycling comprises the steps of removing any metallic inserts; grinding of the remaining fibres and plastics material, thereby shredding them into small pieces; and feeding said small pieces into a granulator. %0
    --Amendments to the Claims have been filed as follows 1. A reworkable pressure vessel for containing a superconducting magnet arrangement; at least first and second separate parts of the vessel being fabricated from fibre-reinforced thermoplastics material; wherein said first and second parts comprise facing end surfaces adapted for fusion bonding together to form a union dosing said vessel such that said vessel can be opened and re-dosed by repeated application of fusion bonding to said union.
    2. A vessel according to claim 1, wherein the thermoplastics material comprises polypropylene or polyethylene.
    3. A vessel according to claim 1 or claim 2, wherein the fusion bonding process used to form said union is chosen from the group comprising: hot tool welding; infra-red welding; laser welding; spin welding; ultrasonic welding; vibration welding; and resistance welding.
    4. A vessel according to daini 3, wherein the same fusion bonding process used to form said union is utilised for one at least of said repeated applications. * .. * *.**
    5. A vessel according to any preceding claim, wherein at least an outer shell of the pressure vessel is formed entirely of said reinforced *r 25 thermoplastics material. S...
    S *..
    *:*. 6. A reworkable pressure vessel substantially as herein described and adapted to contain superconducting magnet arrangements.
    7. A method of manufacturing a pressure vessel for containing a superconducting magnet arrangement, which pressure vessel can subsequently be opened and re-dosed, the method comprising the steps of: fabricating first and second separate parts of the vessel from fibre-reinforced thermoplasti material; said first and second parts comprising fadng end surfaces adapted to abut in fitting relationship; fusion bonding said abutting end surfaces together to form.a union dosing said vessel; and repeatedly applying thermal bonding to said union to open and re-close said vessel.
    8. A method according to claim 7, wherein the fusion bonding process used to open and/or re-dose the vessel comprises a re-application of the same process used to effect the original bond.
    9. A method according to claim 7, wherein a different fusion bonding process from that used for the original bond is used for opening and/or Fe-closure of the vessel.
    10. A method according to any of claims 7 to 9, further comprising recycling the material of the vessel to produce pellets that can be used as raw material in a standard extrusionjcompression moulding apparatus.
GB0724573A 2007-12-18 2007-12-18 Re-workable pressure vessels for superconducting magnet arrangements Expired - Fee Related GB2455720B (en)

Priority Applications (4)

Application Number Priority Date Filing Date Title
GB0724573A GB2455720B (en) 2007-12-18 2007-12-18 Re-workable pressure vessels for superconducting magnet arrangements
PCT/GB2008/051156 WO2009077780A1 (en) 2007-12-18 2008-12-05 An outer vacuum chamber for a cryogenically cooled mri magnet
CNA200810184998XA CN101464476A (en) 2007-12-18 2008-12-17 Reworkable pressure vessel for a superconducting magnet
US12/337,308 US20090162584A1 (en) 2007-12-18 2008-12-17 Re-workable pressure vessels for superconducting magnet arrangements

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB0724573A GB2455720B (en) 2007-12-18 2007-12-18 Re-workable pressure vessels for superconducting magnet arrangements

Publications (3)

Publication Number Publication Date
GB0724573D0 GB0724573D0 (en) 2008-01-23
GB2455720A true GB2455720A (en) 2009-06-24
GB2455720B GB2455720B (en) 2010-01-06

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GB0724573A Expired - Fee Related GB2455720B (en) 2007-12-18 2007-12-18 Re-workable pressure vessels for superconducting magnet arrangements

Country Status (4)

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US (1) US20090162584A1 (en)
CN (1) CN101464476A (en)
GB (1) GB2455720B (en)
WO (1) WO2009077780A1 (en)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8598872B2 (en) * 2011-07-27 2013-12-03 General Electric Company End flange for a magnetic resonance imaging system and method of manufacturing
GB2529244B (en) * 2014-08-15 2017-03-08 Siemens Healthcare Ltd A cooling arrangement for a superconducting magnet structure for an MRI system

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Publication number Priority date Publication date Assignee Title
US3176473A (en) * 1963-04-09 1965-04-06 Andonian Associates Inc Modular dewar vessel for cryogenic use
GB1156833A (en) * 1965-08-07 1969-07-02 Siemens Ag Improvements in or relating to a Cryostat.
US6281773B1 (en) * 1998-07-17 2001-08-28 Picker International, Inc. Magnetizing magnet
US20070014946A1 (en) * 2005-07-15 2007-01-18 Xianrui Huang Thin metal layer vacuum vessels with composite structural support

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US5020358A (en) * 1988-07-05 1991-06-04 Sharp Bruce R Double walled fibrous reinforced resinous storage tanks with common rib supports
JPH03182232A (en) * 1989-12-11 1991-08-08 Toshiba Corp Magnetic resonance imaging device
SE468649B (en) * 1991-05-24 1993-02-22 Kb Komposit Foersaeljnings Ab ARMED PLASTIC CONTAINER, SATISFIED TO ASTAD A COMBUSTION BODY FOR THIS AND APPLIANCE BEFORE IMPLEMENTING THE SET
US5349297A (en) * 1992-03-27 1994-09-20 Picker International Inc. Combined self shielded gradient coil and shimset
US5304934A (en) * 1993-01-04 1994-04-19 General Electric Company Superconducting magnet for imaging human limbs
GB2401346B (en) * 2003-05-07 2005-04-13 Oxford Magnet Tech A structural composite material for acoustic damping
JP4639763B2 (en) * 2004-11-12 2011-02-23 三菱電機株式会社 Magnetic resonance imaging system
DE102006000923B4 (en) * 2006-01-05 2009-10-29 Siemens Ag Magnetic resonance device, comprising a, preferably substantially cylindrical vacuum housing containing a magnet and a cooling device
GB2437964B (en) * 2006-05-06 2009-03-25 Siemens Magnet Technology Ltd An annular enclosure provided with an arrangement of recesses or protrustions to reduce mechanical resonance

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3176473A (en) * 1963-04-09 1965-04-06 Andonian Associates Inc Modular dewar vessel for cryogenic use
GB1156833A (en) * 1965-08-07 1969-07-02 Siemens Ag Improvements in or relating to a Cryostat.
US6281773B1 (en) * 1998-07-17 2001-08-28 Picker International, Inc. Magnetizing magnet
US20070014946A1 (en) * 2005-07-15 2007-01-18 Xianrui Huang Thin metal layer vacuum vessels with composite structural support

Also Published As

Publication number Publication date
WO2009077780A1 (en) 2009-06-25
GB2455720B (en) 2010-01-06
US20090162584A1 (en) 2009-06-25
GB0724573D0 (en) 2008-01-23
CN101464476A (en) 2009-06-24

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COOA Change in applicant's name or ownership of the application

Owner name: SIEMENS PLC

Free format text: FORMER OWNER: SIEMENS MAGNET TECHNOLOGY LIMITED

PCNP Patent ceased through non-payment of renewal fee

Effective date: 20111218