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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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Autor principal: Niinikoski, T O
Lenguaje:eng
Publicado: 1998
Materias:
Acceso en línea:http://cds.cern.ch/record/683728
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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
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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