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EVAPORATIVE COOLING - CONCEPTUAL DESIGN FOR ATLAS SCT
The conceptual design of an evaporative two-phase flow cooling system for the ATLAS SCT detector is described, using perfluorinated propane (C3F8) as a coolant. Comparison with perfluorinated butane (C4F10) is made, although the detailed design is presented only for C3F8. The two-phase pressure drop...
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Lenguaje: | eng |
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1998
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Acceso en línea: | http://cds.cern.ch/record/683728 |
_version_ | 1780901337065586688 |
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author | Niinikoski, T O |
author_facet | Niinikoski, T O |
author_sort | Niinikoski, T O |
collection | CERN |
description | The conceptual design of an evaporative two-phase flow cooling system for the ATLAS SCT detector is described, using perfluorinated propane (C3F8) as a coolant. Comparison with perfluorinated butane (C4F10) is made, although the detailed design is presented only for C3F8. The two-phase pressure drop and heat transfer coefficient are calculated in order to determine the dimensions of the cooling pipes and module contacts for the Barrel SCT. The region in which the flow is homogeneous is determined. The cooling cycle, pipework, compressor, heat exchangers and other main elements of the system are calculated in order to be able to discuss the system control, safety and reliability. Evaporative cooling appears to be substantially better than the binary ice system from the point of view of safety, reliability, detector thickness, heat transfer coefficient, cost and simplicity. |
id | cern-683728 |
institution | Organización Europea para la Investigación Nuclear |
language | eng |
publishDate | 1998 |
record_format | invenio |
spelling | cern-6837282019-09-30T06:29:59Zhttp://cds.cern.ch/record/683728engNiinikoski, T OEVAPORATIVE COOLING - CONCEPTUAL DESIGN FOR ATLAS SCTDetectors and Experimental TechniquesThe conceptual design of an evaporative two-phase flow cooling system for the ATLAS SCT detector is described, using perfluorinated propane (C3F8) as a coolant. Comparison with perfluorinated butane (C4F10) is made, although the detailed design is presented only for C3F8. The two-phase pressure drop and heat transfer coefficient are calculated in order to determine the dimensions of the cooling pipes and module contacts for the Barrel SCT. The region in which the flow is homogeneous is determined. The cooling cycle, pipework, compressor, heat exchangers and other main elements of the system are calculated in order to be able to discuss the system control, safety and reliability. Evaporative cooling appears to be substantially better than the binary ice system from the point of view of safety, reliability, detector thickness, heat transfer coefficient, cost and simplicity.ATL-INDET-98-214oai:cds.cern.ch:6837281998-10-15 |
spellingShingle | Detectors and Experimental Techniques Niinikoski, T O EVAPORATIVE COOLING - CONCEPTUAL DESIGN FOR ATLAS SCT |
title | EVAPORATIVE COOLING - CONCEPTUAL DESIGN FOR ATLAS SCT |
title_full | EVAPORATIVE COOLING - CONCEPTUAL DESIGN FOR ATLAS SCT |
title_fullStr | EVAPORATIVE COOLING - CONCEPTUAL DESIGN FOR ATLAS SCT |
title_full_unstemmed | EVAPORATIVE COOLING - CONCEPTUAL DESIGN FOR ATLAS SCT |
title_short | EVAPORATIVE COOLING - CONCEPTUAL DESIGN FOR ATLAS SCT |
title_sort | evaporative cooling - conceptual design for atlas sct |
topic | Detectors and Experimental Techniques |
url | http://cds.cern.ch/record/683728 |
work_keys_str_mv | AT niinikoskito evaporativecoolingconceptualdesignforatlassct |