Next Linear Collider – U.S. Collaboration
SLAC – FNAL – LBNL - LLNL 1 of 35 - Asiri 09-03-021
Next Linear Collider U.S. Collaboration SLAC FNAL LBNL - LLNL - - PowerPoint PPT Presentation
Next Linear Collider U.S. Collaboration SLAC FNAL LBNL - LLNL ICFA Nanobeams 02 Workshop Sessions 3 At SLAC 1 of 35 - Asiri 09-03-021 Next Linear Collider U.S. Collaboration SLAC FNAL LBNL - LLNL ICFA Nanobeams
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QP
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Far-Field Excitation (Ambient Ground Motion Measurement)
Acceptance Criteria
Select a Location (Representative Site) Good Geology and Quiet Estimate Near-Field Excitation (At Their Footings) Geotechnical Studies (Soil/Rock Classification) Attenuation Characteristics of Soil/Rock
Proceed With Concept Design
Estimate Technical Foundation Vibration ( Response to Near and Far Fields Sources) Select and Locate Near-Field (Chillers, Pumps, etc.)
No Yes
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The chiller rotating equipment rotating speed is 3600 RPM (60Hz). .
The chiller equipment weighs 21,400 pounds.
If a limit of 0.1 g is met at rotating equipment, the inertia force on rce on skid is about 2,140 lb. skid is about 2,140 lb.
The chiller equipment mounted on a spring isolated skid. Generally, they have a natural frequency in the range of Generally, they have a natural frequency in the range of 4 Hz to 6 4 Hz to 6 Hz Hz which corresponds to; which corresponds to; a reduction factor of about 1%. a reduction factor of about 1%. Thus, one percent of this force is transmitted to chiller equipm Thus, one percent of this force is transmitted to chiller equipment ent foundation. foundation.
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Soil Damping Ratio
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Klystron Gallery Klystron Gallery
Soil fundamental frequency
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S2 S1 R1 R2 R3 R4 R5 Plan Layout of Sector 9 and 10 at SLAC Typical Cross Section of Typical Cross Section of Accelerator Housing and Accelerator Housing and Klystron Gallery at SLAC Klystron Gallery at SLAC
50 100 150 200
100 200 Source Receiver Beam CL S1 S2 R1 R2 R3 R4 R5
Location Plan View of Sources S# and Receptors R# Location Plan View of Sources S# and Receptors R#
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At Drive Point S1 At Tunnel Receiver Location R1
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0.00001 0.0001 0.001 0.01 0.1 1 25 50 75 100 125
Frequency, Hz Change in Amplitude
Change in Amplitude, dB
0.01 0.1 1 10 100 1000 25 50 75 100 125 Frequency, Hz RMS Velocity, P in/s
10 20 30 40 50 60 RMS Velocity Level, dB (re 1 P in/s)
R1 - Response Ambient (R1)
0.0 0.2 0.4 0.6 0.8 1.0 25 50 75 100 125
Frequency, Hz Coherence
Drive Point Receiver
Typical Response at R1 due to Hammer Force at S1 Typical Response at R1 due to Hammer Force at S1, with Ambient at R1
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0.00001 0.0001 0.001 0.01 0.1 1 1 10 100 Frequency, Hz Change in Amplitude
Change in Amplitude, dB
R1/S1 R2/S1 R3/S1 R4/S1 R5/S1
Log Mean Transmission From Drive Point S! Log Mean Transmission From Drive Point S!
The figures in the above table represent the attenuation Factor A for a vibration with its source near Sn propagating along the same path. Example 1: Suppose a pump is installed at S1, and it produces a vibration at 30 Hz with an amplitude of X. The amplitude at 30 Hz that we measure at R5 would be the greater of either ambient or 0.009X. Example2: If we want to place a pump at S1 and not to exceed ambient at R5 (06Mic in/sec), then we need to impose a limit on the resulting vibration at S1 of 0.6/0.009=67 Mic in /sec.
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A cross A cross-
section through the Santa Monica mountains showing the different geological conditions. geological conditions. Reach 6 might be a potential test site. Reach 6 might be a potential test site.
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