external forces from heat links in cryogenic suspensions
DESCRIPTION
External forces from heat links in cryogenic suspensions. D1, ICRR, Univ. Tokyo Takanori Sekiguchi. GWADW in Hawaii. About this Talk. Estimate seismic noise introduced from heat links. Discuss how to achieve cooling and seismic isolation at the same time. Seismic Noise from Heat Links. - PowerPoint PPT PresentationTRANSCRIPT
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External forces from heat links in cryogenic suspensions
D1, ICRR, Univ. Tokyo
Takanori Sekiguchi
GWADW in Hawaii
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GWADW 2012 2
About this Talk
2012/5/15
Estimate seismic noise introduced from heat links. Discuss how to achieve cooling and seismic isolation at
the same time.
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GWADW 2012 3
Seismic Noise from Heat Links
2012/5/15
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GWADW 2012 4
Attenuate seismic noise
Cool down test masses
Basic Requirement forKAGRA Test Mass
Suspension
2012/5/15
Test Mass Displacement< 3 x 10-20 m/√Hz @ 10 Hz
Mirror Temp. ~ 20 K
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GWADW 2012 5
Seismic Attenuation System for KAGRA Test Mass
2012/5/15
~14 m
Seismic vibration transmits to the mirror in two different paths
1. From the top through the attenuation chain
2. From the wall of the cryostat through heat links
①
②
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GWADW 2012 6
Heat transferred via pure aluminum heat links.
Cryogenics
2012/5/15
We need 1 mm, L=1 m heat links Φ x 7~8
Thermal simulationDone by Y. Sakakibara
( 1.6 mm, L=30cm)Φ
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GWADW 2012 7
Mechanical Property of Heat Links
2012/5/15
A heat link works as a soft spring (f0~10 mHz)
with violin modes above ~1 Hz
FEM Simulation Done by Y. Aso, (JGW-G1000108)
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Estimation of Seismic Noise via Heat Links
2012/5/158
Simulation Tool: 3-D rigid-body model simulationT. Sekiguchi, Master Thesis (JGW-P1200770)
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Calculation Result
2012/5/159
①
②
Polluting detector sensitivity above 10 Hz !!
* Assuming 1% couplingfrom vertical
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To Make Matters Worse ..
2012/5/1510
There is no guarantee that the wall inside the cryostat is vibrating at the same level as the ground.
???
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Vibration Insidethe Cryostat in CLIO
2012/5/1511
10-100 times larger !!
GWADW 2012
K. Yamamoto et al, J. Phys.: Conf. Ser. 32 418 (2006)
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In Worse Case
2012/5/1512
①
②* Assuming 1% couplingfrom vertical
If the attachment point of heat links is vibrating at the same level as cryostat vibration in CLIO..
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Improved Design
2012/5/1513
Add one more “cushion” between the cryostat and mirror
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Consideration on Cooling
2012/5/1514
These two masses are thermally well connected by heat links*
* Pure aluminum 3 mm, L=63 cm,Φ
Number: 5
( 1.6 mm, L=30cm)Φ
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After Improving Wiring
2012/5/1515GWADW 2012
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After Improving Wiring
2012/5/1516
Several peaks exceed the target sensitivity, but the flour level is OK.
GWADW 2012
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Possible Ideas ofFurther Improvement
2012/5/1517
Suppress the cryostat vibration passively/actively. Put additional filters between suspension and cryostat.
Add vertical springs for test mass suspension.
GWADW 2012
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Another Consideration
2012/5/15
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Effect on Angular Motion
2012/5/1519
SAS is very soft in yaw motion (~ 10 mHz). Low frequency yaw motion can be easily excited.
GWADW 2012
Single wire suspension
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Effect on Angular Motion
2012/5/1520
If one employs asymmetric wiring of heat links..
RMS: 2 radμ
Microseismic peak
Yaw resonance
* Eddy current damping for yaw modes is appliedT. Sekiguchi, Master Thesis (JGW-P1200770)
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Symmetric Configuration
2012/5/1521
Symmetric wiring does not subject any torque. If you admit 10% thickness difference in two connections
Blue Curve
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1.1 mmΦ
1.Φ 0 mm
RMS: 0.5 radμ
Not small, but in a controllable level
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GWADW 2012 22
Summary
2012/5/15
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GWADW 2012 23
Careful wiring of heat links is required, in order to mitigate the seismic noise introduced from them.
Further isolation, or improvement of the suspension design may be necessary.
Yaw excitation by heat links would be not so huge (be in a controllable level).
Summary
2012/5/15
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GWADW 2012 24
Transfer function measurement of heat links.(How to ??)
Vibration measurement inside the cryostat. L. Naticchioni and D. Chen will start this autumn
Future Works
2012/5/15
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GWADW 2012 25 2012/5/15
The END
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GWADW 2012 26 2012/5/15
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Appendices
2012/5/15
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GWADW 2012 28
Seismic noise should be much lower (at least 10 times smaller) than other noises at the detector observation band (> 10 Hz).
Requirement for KAGRA Test-Mass Suspensions (1)
2012/5/15
KAGRA Design Sensitivity
Seismic Noise Requirement:< 3 x 10-20 m/√Hz @ 10 Hz
And rolls off steeper than f-3
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GWADW 2012 29
Mirror temperature should be as low as 20 K to suppress thermal noise.
Requirement for KAGRA Test-Mass Suspensions (2)
2012/5/15
Substrate thermoelastic noise ( T∝ 2.5) gets lower than coating Brownian noise( T∝ 0.5) at < 23 K
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GWADW 2012 30
Seismic Attenuation System
(SAS) for KAGRA
2012/5/15
7-stage pendulum + 5-stages vertical spring
~13 m
(horizontal attenuation) (vertical attenuation)
Last 3 stages are cooled at cryogenic temperature (<20 K) to suppress thermal noise
Cryostat * Beam splitter and other optics are suspended by smaller vibration isolation systems
Mirror (Test Mass)
Metal cantilever springs
Geometric Anti-Spring (GAS) Filter
f0 ~ 0.3 Hz
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Vibration Isolation System
Disposition
2012/5/1531GWADW 2012
Expected Performance
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SAS Status
2012/5/1532GWADW 2012
Prototype Experiment:Standard filter (GASF): Performance was measured @NIKHEFPre-isolator (IP&GASF): Now Measuring @ KashiwaDesign:Type-B Payload: Now Designing
MeasuredTransfer Function(Feb. 16th, 2011)
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Cryogenics
2012/5/15
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Initial Cooling Time
2012/5/15
Thermal simulationwith Y. Sakakibara’s Method
* The inner shield and the masses except for the test mass are DLC-coated ( =0.41).ε
** Radiation cooling is dominant before 15th day.
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GWADW 2012 35
Initial Cooling Time Calculation Diagram
2012/5/15
By Y. Sakakibara
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GWADW 2012 36
Heat Load
2012/5/15
Absorption in mirrorCoating: 0.4 W (1ppm)Substrate: 0.6 W (50 ppm/cm)Total: 1.0 W
Inner shieldRadiation from 80 K: 1.3 WConductance: 0.8 WScattered Light: 5 W (10 ppm)Total: 7.1 W
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GWADW 2012 37
Heat Extraction Scheme
2012/5/15
In the new heat extraction scheme, mirror temperature would not be raised, even if large scattered light attacks the shield.
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GWADW 2012 38 2012/5/15
Thermal Conductivity of High Pure Aluminum
40,000 W/m/K @ 6K
6N Aluminum
2N Aluminum~Type A-1070 For inner shield
For outer shield
5N up AlRRR=3000
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GWADW 2012 39
Heat Link TF Calculation
2012/5/15
Pure aluminum (E=68 GPa), 1 mmΦ Half-ellipsoid (a=400 mm, b=200 mm) Loss angle: 10-4
FEM Simulation Done by Y. Aso, (JGW-G1000108)
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GWADW 2012 40 2012/5/15
Heat LinkTransfer Functions
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GWADW 2012 41 2012/5/15
Heat Link TFs
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Seismic Noise via Heat Links
2012/5/1542
Couplings from the vertical motion is dominant above 3 Hz.
GWADW 2012
* Assuming 1% couplingfrom vertical
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Heat Links with Half Diameters
2012/5/1543
How about decreasing the fiber thickness,from 1.0 mm Φ to 0.5 mmΦ ?
GWADW 2012
Heat conductivity per link: x 1/4 Necessary number of links: x 4 Spring constant per link: x 1/16 Total stiffness: 1/4 Heat link total mass: Same
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Hot Platform Design
2012/5/1544
Push heavy Platform to the room temperature part.
GWADW 2012
Decrease the initial cooling time.
Another vibration shortcut occurs between IM and IRM
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Hot PlatformInitial Cooling Time
2012/5/1545GWADW 2012
Current Design Hot Platform
1 week earlier!!
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Hot PlatformSeismic Noise
2012/5/1546GWADW 2012
Due to the vibration shortcut, seismic noise gets larger above 10 Hz in ~1 order of magnitude
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Heat Links with Half Diameters
2012/5/1547
Only better at 1-3 Hz, not so good above 10 Hz
GWADW 2012
* Assuming 1% couplingfrom vertical
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Torsion Mode Damping
2012/5/1548
Eddy current damping for yaw modes
GWADW 2012
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Torsion Mode Damping
2012/5/1549
Torsion modes of the single wire suspensions would be sufficiently damped by the eddy current damper.
GWADW 2012
Damping time: 1~2 min.
Mirror yaw angle response to applied torque
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Effect on Angular Motion
2012/5/1550
RMS: 0.5 radμ
GWADW 2012