Development of Fused S ilica S uspension Fibres for Advanced - - PowerPoint PPT Presentation
Development of Fused S ilica S uspension Fibres for Advanced - - PowerPoint PPT Presentation
Development of Fused S ilica S uspension Fibres for Advanced Gravitational Wave Detectors TAUP S endai 11 th S eptember 2007 Alastair Heptonstall Institute for Gravitational Research University of Glasgow Hept onst all, Bart on, Cagnoli,
Hept onst all, Bart on, Cagnoli, Cumming, Faller, Hough, Jones, Mart in, Rowan, S t rain, Veggel, Zech
Monolithic suspensions for advanced detectors
- Development of monolithic suspensions
is based on experience from the GEO600 suspensions
- This talk will cover aspects of
production and testing of suspension elements suitable for Adv. LIGO and upgrades to Virgo
- The criteria that must be met by ribbon
fibres for Adv. LIGO:
S
trength (x3 safety margin)
Thermal noise performance
- To meet these criteria we require
Breaking stress > 2.4 GPa Intrinsic loss <3 x 10-11/ t, where t is
the thickness of the ribbon
Hept onst all, Bart on, Cagnoli, Cumming, Faller, Hough, Jones, Mart in, Rowan, S t rain, Veggel, Zech
Improving fibre pulling technology
- Advanced LIGO suspensions require ±1.9%
tolerance on fibre dimensions.
- This is a slight increase on the ±2.1%
achieved in GEO600.
- Repeatability and tolerance in flame
pulling machines is limited by gas regulation and slack in mechanical parts.
- A new machine was developed in
Glasgow using a CO2 laser and high precision drive systems
- Designed for both ribbon and cylindrical
fibre production to be suitable for both LIGO and Virgo upgrades.
- The machine is also capable of welding
fibres.
Hept onst all, Bart on, Cagnoli, Cumming, Faller, Hough, Jones, Mart in, Rowan, S t rain, Veggel, Zech
Pulling fibres using the CO2 laser
Hept onst all, Bart on, Cagnoli, Cumming, Faller, Hough, Jones, Mart in, Rowan, S t rain, Veggel, Zech
Virgo laser pulling machine installation
Hept onst all, Bart on, Cagnoli, Cumming, Faller, Hough, Jones, Mart in, Rowan, S t rain, Veggel, Zech
Diameter of CO2 pulled fibre in region of taper
500 1000 1500 2000 1 2 3 4 5 6 7 8 9 10 Travel /mm Diameter (micron)
1 2 3 4 5 Length (mm) Diameter (µm) 1000 1500 2000 500
Controlled shaping of the neck
1 2 3 4 Length (mm) 200 600 1000 1400 Diameter (µm)
Hept onst all, Bart on, Cagnoli, Cumming, Faller, Hough, Jones, Mart in, Rowan, S t rain, Veggel, Zech
Mechanical loss in CO2 laser pulled fibres
0.E+00 2.E-07 4.E-07 6.E-07 8.E-07 1.E-06 1 10 100 1000 10000 Frequency (Hz) Loss
0.E+00 2.E-07 4.E-07 6.E-07 8.E-07 1.E-06 1 10 100 1000 10000 Frequency (Hz) Loss
m 10 05 . 6
12 −
× =
surface
hφ
- Four S
uprasil 300 fibres of diameter ~470µm were measured
- Initial analysis of losses shows a surface loss consistent with:
- S
uprasil 300 is not necessarily expect ed to be similar to 312 or 311 as it has a different manufacturing process and a lower OH content
- From Penn et al we can calculate values:
m 10 3.25
- 12
× =
surface
hφ m 10 7 . 4
12 −
× =
surface
hφ
for suprasil 312 for suprasil 2
Hept onst all, Bart on, Cagnoli, Cumming, Faller, Hough, Jones, Mart in, Rowan, S t rain, Veggel, Zech
Where does dissipation arise in our material?
- In order to reduce thermal noise we need to reduce
dissipation.
- To do this we must first understand where it arises.
- Loss in fused silica is normally split into two categories
- Bulk
A very low level dissipation in the body of the material recently shown to be due to the residual effects of dissipation due to a two level system
- S
urface A much higher level of dissipation in the damaged surface layer
- The dominant loss mechanism depends on surface to volume
ratio.
- This can now be controlled to a level acceptable for next
generation detectors
- However a better understanding of the physics of these loss
mechanisms is needed to reduce thermal noise for future detectors
Hept onst all, Bart on, Cagnoli, Cumming, Faller, Hough, Jones, Mart in, Rowan, S t rain, Veggel, Zech
Recent measurements at Glasgow (1)
0.0E+00 5.0E-08 1.0E-07 1.5E-07 2.0E-07 2.5E-07 3.0E-07 3.5E-07 0.05 0.1 0.15 1/ Length Measured loss minus thermoelastic
- Loss measurements made on laser
pulled fused silica fibres have shown a length dependence to dissipation
- This is consistent with a source of
loss close to the top of the fibre
- This has been shown analytically and
using finite element modelling
- S
- urce of loss thought to be due to
welding
- This is a previously unknown source
- f loss – highly relevant for
development of detector suspensions
Hept onst all, Bart on, Cagnoli, Cumming, Faller, Hough, Jones, Mart in, Rowan, S t rain, Veggel, Zech
Recent measurements at Glasgow (2)
0.E+00 2.E-07 4.E-07 6.E-07 8.E-07 1.E-06 0.02 0.04 0.06 0.08 0.1 0.12 1/ length residual loss
470um welded directly on fibre 470um welded directly on fibre 470um welded directly on fibre 345um welded with a few mm above the neck
welded with a neck
- Each weld gives different
value for loss
- When viewed under a
microscope possible loss mechanisms can be seen
- Fibre attached using thick
neck shows lowest loss as less energy stored in weld
Hept onst all, Bart on, Cagnoli, Cumming, Faller, Hough, Jones, Mart in, Rowan, S t rain, Veggel, Zech
Recent measurements at Glasgow (3)
1.00E-07 1.20E-07 1.40E-07 1.60E-07 1.80E-07 2.00E-07 2.20E-07 2.40E-07 500 1000 1500 2000 2500 3000 3500 4000 Frequency (Hz) Measured loss minus thermoelastic
- Analysis of dissipation in fibres has shown evidence of a
frequency dependent bulk loss seen at a higher than expected level
- Approximately 10 times that seen in bulk samples
- At higher frequencies this contributes as much as 25%
- f loss
Hept onst all, Bart on, Cagnoli, Cumming, Faller, Hough, Jones, Mart in, Rowan, S t rain, Veggel, Zech
Ribbon fibre development
Hept onst all, Bart on, Cagnoli, Cumming, Faller, Hough, Jones, Mart in, Rowan, S t rain, Veggel, Zech
Ribbon cross-sectional shape development
- First ribbon fibres pulled had a non-
rectangular cross-section due to heat loss from edges.
- Laser was run at close to maximum power
due to heat loss.
- Polished aluminium heat shield was
developed to reflect heat back at edges.
- Further improvements to the symmetry of the
fibre neck and cross section were achieved by using slides on either side to reduce the edge effects.
- Laser stabilisation has been significantly
improved
Fast sensor Wedged Brewster window for pick-off
- Profile of pull has been investigated to create
good shapes for the neck regions Initial cross-section Using heat shield Using heat shield & side slides
Hept onst all, Bart on, Cagnoli, Cumming, Faller, Hough, Jones, Mart in, Rowan, S t rain, Veggel, Zech
Profiling of ribbon dimensions
Hept onst all, Bart on, Cagnoli, Cumming, Faller, Hough, Jones, Mart in, Rowan, S t rain, Veggel, Zech
S trength and bounce frequency testing
Hept onst all, Bart on, Cagnoli, Cumming, Faller, Hough, Jones, Mart in, Rowan, S t rain, Veggel, Zech
Welding technology
Hept onst all, Bart on, Cagnoli, Cumming, Faller, Hough, Jones, Mart in, Rowan, S t rain, Veggel, Zech
Bonding test mass ears at LAS TI (1)
Hept onst all, Bart on, Cagnoli, Cumming, Faller, Hough, Jones, Mart in, Rowan, S t rain, Veggel, Zech
Bonding test mass ears at LAS TI (2)
Hept onst all, Bart on, Cagnoli, Cumming, Faller, Hough, Jones, Mart in, Rowan, S t rain, Veggel, Zech
Conclusions
- Based on the experience of the flame pulling machines used for the GEO600 suspensions
we have designed and built new fibre pulling machines using CO2 lasers
- Laser pulled cylindrical fibres have a surface loss at a similar level to flame pulled fibres
- Data shows evidence of length dependent loss which appears to be related to the quality
- f weld
- There is strong evidence of frequency dependence in residual loss of fibres st udied
- This appears to arise due t o dissipation in the bulk of the fibre material but at a higher
level of loss than is seen for larger ‘ bulk’ samples
- Both the above effects need included in any model of suspension thermal noise in
monolithic silica suspensions
- Further studies in progress
- The construction of the monolithic pendulum stage for LAS