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MICE OsC – 22 nd June 2010 Liquid-hydrogen system and absorber M Hills T Bradshaw M Courthold S...
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Transcript of MICE OsC – 22 nd June 2010 Liquid-hydrogen system and absorber M Hills T Bradshaw M Courthold S...
MICE OsC – 22nd June 2010
Liquid-hydrogen system and absorber
M HillsT BradshawM CourtholdS IshimotoW LauI MullacraneP Warburton
MICE OsC – 22nd June 2010
Contents
1. Introduction2. Latest progress on R&D system manufacture3. The system safety case4. Control system5. Hall infrastructure6. Integration with the AFC module7. Summary & plans for 2010/11
MICE OsC – 22nd June 2010
The Hydrogen Delivery System and Absorber
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AFC Module(Tesla/Oxford/STFC)
Absorber (KEK/Mississippi)
Hydrogen Delivery System(STFC)
MICE OsC – 22nd June 2010
R&D System Manufacture (1)
Buffer Volume, Transfer Line and Test Cryostat all complete Gas Panel assembly well advanced Design of enclosure is being detailed
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MICE OsC – 22nd June 2010
R&D System Manufacture (2)
– Gas Panel manufacturing– Weld inspection and pipe cleaning complete– Final assembly of pipework underway– Flow meters (final item of instrumentation) procured and installed in the gas panel– Relief valves assembled into dedicated mounting frames
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MICE OsC – 22nd June 2010
Safety Approach
– The system must tolerate two things going wrong simultaneously without becoming unsafe
– Design philosophy• Maintain separation of hydrogen and oxygen atmospheres• Avoid sources of ignition (a hydrogen-oxygen mixture only needs 19µJ to ignite)
– Standards• Dangerous Substances and Explosive Atmospheres Regulations (DSEAR). This is the
UK implementation of the EU ATEX User Directive.• IEC 61508 (Functional safety of electrical/electronic/programmable electronic
systems)
– Passive safety concept• Relief valves will open to return gas to the hydride bed or high level vents in the
event of a rapid pressure rise (e.g. due to loss of insulating vacuum). This happens independently of the control system.
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MICE OsC – 22nd June 2010
MICE Safety Considerations
The design of the MICE AFC module creates particular requirements:
– Thin windows on absorber have a design pressure of 1.7bara (they will be burst pressure tested to 4x this).
– Hydrogen system consequently operates at low pressure (relief valves set at 1.5bara; burst discs at 1.9bara)
– Rapid pressure rise could result from large liquid-to-gas expansion ratio of hydrogen (approx. 780/1)
– Pipework, Buffer Volume and relief valves are sized for total loss of vacuum in the AFC module
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MICE OsC – 22nd June 2010
DSEAR Zoning11
Test Cryostat (or AFC absorber vacuum space)
Gas Panel Enclosure Pump Enclosure Connecting ductwork
...are Zone 2.(“A place in which an
explosive atmosphere....is not likely to occur in normal operation, but, if it does occur, will persist for a short period only.”)
The MICE Hall is not
MICE OsC – 22nd June 2010
Control System (1)
Control Panel assembled with (almost) all components needed for He testing
Barriers provide intrinsic safety (<19µJ in the circuit) for all wiring except the heaters.
PLC programmed Temperature logging Valve control tested Example control sequence
tested
Heater control implemented
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PLC
Barriers
GP & Cryostat Connectors
MICE OsC – 22nd June 2010
Control System (2)
– Cryostat monitoring complete (almost)– Sequences for gas panel operation currently being written– Design work underway for ventilation system and vacuum
system control.
MICE OsC – 22nd June 2010
Control System Safety Functions
Only three functions of the control system identified as ‘safety critical’:I. Operation of the ventilation system on detection of a
hydrogen leakII. Shut-off PV20* if there is pressure rise in the cryostat
during operation.III. Interlock the Gas Panel Enclosure with system returning to
‘safe state’ on breaking of interlock
These will all be hard-wired and separate from the PLC.
[*This isolates the vacuum system.]
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MICE OsC – 22nd June 2010
UPS Requirements
Recent discussions held amongst the Hydrogen System team on the UPS requirements for the system
Document currently being drafted for submission to MICE Technical Board
Key conclusions– In the event of a mains failure:
• System will fail to its pre-defined ‘safe-state’• Instrumentation and valve position information should
continue to be available from the control system• The hydrogen detection system should continue to function
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MICE OsC – 22nd June 2010
Hall Infrastructure
To install the R&D system in the MICE Hall requires:– Bottle store– Vacuum system with roughing pumps sited externally– Ventilation system to exhaust any leak in Gas Panel, Buffer Volume or
Hydride Bed.
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MICE OsC – 22nd June 2010
Hall Infrastructure17
Relief lines
Ventilation ducts
Fans
Test Cryostat
Gas Panel Enclosures
MICE OsC – 22nd June 2010
Ventilation System
H2 vented during operation of relief valves is separate form ventilation system
MICE OsC – 22nd June 2010
Ventilation System
Basis of safety– Eliminate sources of ignition
ATEX rated fans– Fans are specified such that one fan only is capable of providing sufficient flow to exhaust all three
systems– An explosive atmosphere from a small leak in the gas panel would only persist for a matter of
minutes– Fans have been purchased and are ready to install.
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MICE OsC – 22nd June 2010
Vacuum System
– Dedicated pump enclosure to be sited on MICE Hall roof– Will house backing pumps
required for all 3 hydrogen systems
– Will also have capacity to house backing pumps required for other cooling channel modules
– Designated Hydrogen Zone 2 (same as Gas Panel Enclosures) for DSEAR purposes
– Turbo pumps for AFC modules’ safety vacuum shown on South Wall (must be behind magnetic shield wall)
Turbo pumps
Backing pump
MICE OsC – 22nd June 2010
– Located opposite the MLCR
– Virtually all preparation for rack installation complete: – room cleaned out– new door fitted– redundant pipes
removed– Cabinet support frames
installed– cable routes
established
Hydrogen Control Room
MICE OsC – 22nd June 2010
Integration with the AFC
– Working with Oxford, KEK and Tesla to ensure that the R&D system is compatible with the AFC module– Instrumentation – Process line connections
– Aim to test absorber in R&D test cryostat to check interfaces and instrumentation
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MICE OsC – 22nd June 2010
Summary and Future Plans– R&D System components complete with exception of Gas Panel and Enclosure; these
are due for installation at start of long ISIS shutdown.– Control system well advanced– Safety principles of system well established, but implementation and documentation of
these are still ongoing. Results from helium testing will be an important input to a pre-operation safety review.
– Design work underway for hall infrastructure requirements, but lots to do.– Need to continue to work closely with KEK, Oxford and Tesla to ensure compatibility with
AFC.– Aim to take advantage of the long ISIS shutdown and delays to the Spectrometer
Solenoids to install as much infrastructure as possible in the rest of this financial year.– Several tasks:
• Install R&D system components on south mezzanine• Build pumping enclosure and install vacuum system• Position fans, install ductwork and construct access platforms• Route vent lines outside hall• Install hydrogen detection system• Route cabling and install control racks in H2 Control Room
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