Contamination Control Study: BSC Chamber LIGO Observatory Project Number: FVMS0506-01 Parametric-1 Results August 14, 2006.

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Presentation transcript:

Contamination Control Study: BSC Chamber LIGO Observatory Project Number: FVMS Parametric-1 Results August 14, 2006

Objectives  Modify the thermal/airflow FLOVENT model of the BSC Chamber such that the airflow speed from the core area matches that of the annular area: –Baseline Scenario 2: –Core Flow: 1.0 m 3 /sec; ~0.4 m/sec –Annular Flow: 2.0 m 3 /sec; ~2.0 m/sec –Extract duct size;QTY: 6”x6”;1 –Parametric-1: –Core Flow: 5.5 m 3 /sec; ~2.0 m/sec –Annular Flow: 2.0 m 3 /sec; ~2.0 m/sec –Extract duct size;QTY: 12”x12”;4 The speeds stated above are for comparison purposes and are based on the flow surface area of the particular device and does not include the acceleration of the flow through the perforation

Personnel Assumptions  Personnel: –4 personnel: 2 in BSC Chamber, 2 in surrounding cleanroom –Contamination Generation rate: 3950 particles/sec (≥ 0.5um) –Heat Generation rate: 85 W sensible heat Uniform heat and particle generation Contamination rate based on: high quality cleanroom clothing systems at 25 washes and moderate personnel activity (Cleanroom Clothing Systems: People as a Contamination Source, Ljungqvist and Reinmuller)

Personnel Locations Only open door Purge Airflow

Cleanroom Overview HEPA Filters: 400 cfm (0.188 m 3 /s) each, QTY: 20 Curtain opening: 8.5” height 17.33’ 18.58’ 17.42’ HEPA Filters outlined in red

BSC Airflow Overview Extract Flow: 1.83 m 3 /s (QTY 4) Flow direction Perforated Floor:20% Open Purge Airflow: m 3 /s (25 cfm) Flow direction

Air Shower Overview Annular Flow: 2.0 m 3 /s No Flow Area (Support rod hidden for clarity) Core Flow: 5.5 m 3 /s Core Flow and Annular Flow approximated with flow accelerated through 3/8” holes on 1” pitch (11% Open)

Simulation Results Parametric-1

View Orientation Design Comparison-Speed Plane taken at centerline of the chamber Baseline-Scenario 2 Parametric-1 Open door Annular Section hidden High flow rate due to entrainment

Design Comparison-Velocity Plane taken at centerline of the chamber View Orientation Baseline-Scenario 2 Parametric-1 Open door Annular Section hidden High flow rate due to entrainment

Design Comparison-Speed-2 Plane taken at centerline of the chamber View Orientation Baseline-Scenario 2 Parametric-1 Open door Annular Section hidden High flow rate due to entrainment

Design Comparison-Velocity-2 Plane taken at centerline of the chamber View Orientation Baseline-Scenario 2 Parametric-1 Open door Annular Section hidden High flow rate due to entrainment

Air Shower Flow Paths

Speed Profile through the Chamber Door z y x Maximum Outward Flow Maximum Inward Flow Plane taken at the cross-section of the chamber door

Extraction Pressure The above plane is taken at the inlet to the extraction nozzle, and illustrates the pressure required to achieve a flow of 1.83 m 3 /sec and assumes the nozzle is venting to atmosphere Mean pressure at extract: -260 PA

ISO Class Specifications 0.5 um diameter particles The following slides show the areas of the space at various uniform concentration levels. Maximum concentration: 184,928 Particles/m 3 (ISO 7)

Design Comparison- ISO Class 5 ISO 7 ISO 6 ISO 5 ISO 4 Chamber doors hidden for visualization purposes Baseline-Scenario 2 Parametric-1

Design Comparison- ISO Class 6 ISO 7 ISO 6 ISO 5 ISO 4 Location of maximum concentration Baseline-Scenario 2 Parametric-1

Summary  The thermal/airflow FLOVENT model of the BSC Chamber has been modified such that the airflow speed from the core area matches that of the annular area. A comparison between the Baseline-Scenario 2 and Parametric-1 simulations has been shown. Some conclusions are drawn below: –The increase in air flow resulted in a slight decrease in maximum particle concentration and the location of the maximum has moved outside the BSC Chamber. –Extracting flow through 4 -12” exhaust ducts has decreased the required work to move the air flow. –A more uniform airflow was obtained when increasing the core flow to match the speeds exiting the annular ring area. Any reduction/increase in overall airflow should maintain a consistent air speed from each delivery point.