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ATF2: final doublet support Andrea JEREMIE B.Bolzon, N.Geffroy, G.Gaillard, J.P.Baud, F.Peltier With constant interaction with colleagues from KEK, SLAC.

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Presentation on theme: "ATF2: final doublet support Andrea JEREMIE B.Bolzon, N.Geffroy, G.Gaillard, J.P.Baud, F.Peltier With constant interaction with colleagues from KEK, SLAC."— Presentation transcript:

1 ATF2: final doublet support Andrea JEREMIE B.Bolzon, N.Geffroy, G.Gaillard, J.P.Baud, F.Peltier With constant interaction with colleagues from KEK, SLAC and KNU

2 A.Jeremie CLIC'082 Outline FD support specifications Initial active support study Rigid support on intermediate feet Final rigid support Measurements with water flow Installation photos Conclusion

3 A.Jeremie CLIC'083 Shintake Monitor: information on the beam size ATF2 Layout Final doublets

4 A.Jeremie CLIC'084 FD layout SBPM QC3 SBPM FFTB 2.13 S3.00 SF1QF1 76.2 450.1 575 200 180 311.9 785380 456553.1 SBPM QC3 SBPM FFTB 2.13 S3.00 SD0QD0 76.2 450.1 200 180 311.9 575 450.1 456553.1 785380 IP 1940 mm 1225 What is needed to support all these components?

5 A.Jeremie CLIC'085 For QD0 at ATF2: 6-7nm tolerance Two solutions possible: 1.Isolate/cut vibrations in the desired frequency range 2.Push the first resonance peaks at higher frequencies where ground motion is lower 0.1Hz ~50Hz Repetition rate 1Hz=> need a “mechanical” stabilisation from 0.1Hz (below, the beam based alignment works) 6-7nm ATF2 specifications ATF ground motion

6 A.Jeremie CLIC'086 FD support specifications Desired frequency range : 0.1Hz-50Hz Support that can evolve as Final Focus design evolves (should be able to change support) 6-7nm jitter tolerance 1.2m beam height Honeycomb table Isolator: Passive => turned OFF Active => turned ON Initial suggestion: CERN wanted to contribute by sending the commercial TMC table

7 A.Jeremie CLIC'087 Vibrations of the passive TMC table Vertical direction: Integrated RMS Above 0.5Hz: Amplification Above 30Hz: damping begins Below 0.5Hz: No amplification or damping on the table 27 Amplification 0.5 ~Same response Amplification Damping 30

8 A.Jeremie CLIC'088 Vibrations of the active TMC table Above 0.8Hz: Damping on the table  Factor 7 of damping above 1.5Hz Vertical direction: integrated RMS Below 0.8Hz: Amplification on the table

9 A.Jeremie CLIC'089 Ground Shintake monitor Final doublets Beam Interference fringes We want the measurement to have a coherent behaviour with respect to the “beam” => Relative motion between Shintake monitor and final doublets: 6-7nm in the vertical axis above 0.1Hz 4m Good ground motion coherence: measured on KEK site  Separate stiff supports rigidly fixed to the floor Specifications Study the honeycomb block but without feet If Shintake Monitor and FD on separate active supports, coherence is lost

10 A.Jeremie CLIC'0810  Without any masses: 56.2Hz  Lower than in free configuration!  With masses: 26.2Hz  Fall of the eigenfrequency Boundary conditions: table put on / fixed to 4 rigid supports at its corners “simple” Simulation: just a block with the right boundary conditions => to see the evolution First resonance peak in free-free configuration: 230Hz Too low! velocity sensors Microphones accelerometers Table without any masses Table with masses simulating the weight of FD

11 A.Jeremie CLIC'0811 Transfer functions of the table with its feet First resonance (phase: 90°) No masses: 74Hz With masses: 46Hz Higher displacements because increase of ground motion with decrease of frequency  Impact of the different vibration peaks on relative motion

12 A.Jeremie CLIC'0812 Integrated RMS of relative motion between table and floor to predict on the ATF site Calculation performed for these specific needs: Calculation to perform by integrating the vibratory behaviour of the table measured at LAPP and the data of ATF ground motion Relative motion between table and floor

13 A.Jeremie CLIC'0813 Total relative motion ([0.17; 100]Hz): 6.7nm  Above tolerances (6nm)! Contribution of the peak alone: [30; 100]Hz: 4.6nm Integrated RMS of relative motion at ATF 6.7nm  Need to push resonances to higher frequencies where ground motion is lower Relative motion between table and floor 4.6nm

14 A.Jeremie CLIC'0814 Is the honeycomb table rigid enough? Impact hammer on table Modal deformations  for each resonance (up to 150Hz)  In the three axis Modes1) T-X2) T-Y3) R-Z4) T-Z5) R-Y6) R-X Frequency (Hz)34.841.860.680.6103.9136.0 Damping (%)2.82.62.42.32.14.0 6 first modes: rigid body modes in 6 degrees of freedom 2 tri-axis accelerometers Michael GUINCHARD (CERN) Z X Y T: Translation R: Rotation  Fix table on whole surface to remove these modes Table fixed on 4 rigid supports at the 4 corners The table is a rigid body, but the feet are not

15 A.Jeremie CLIC'0815  Without any masses: 526.1Hz  Even higher than in free configuration!  With masses: 135.2Hz  Fall of the eigenfrequency but still high Table fixed directly to the floor on 1 entire side Choice of the ATF2 collaboration: Get the same table to send it to Japan and fix it to the floor Bees wax: good vibration transmission, can be unglued, stable in time, rad hard Honeycomb table 3 steel plates bolted to the floor Bees wax Set-up can be moved in the future simulation

16 A.Jeremie CLIC'0816 IP QD0 SF1 QF1 SD0 beeswax Room for slings for table lifting FD configuration Quads, sextupoles and movers :SLAC (from FFTB) From floor to mover: LAPP (new) BPM+support: KNU, LAPP 2.4m Adjustment possible in x, y, z with shims (0.05mm) and adjustment pushers for 1.2m beam height

17 A.Jeremie CLIC'0817 Table fixed on one entire face to the floor Experimental set-up 3 steel plates bolted to the floor Honeycomb table Bees wax  Good boundary conditions chosen for the table: Relative motion should be very low compared to tolerances No masses: no peak With masses: 92Hz

18 A.Jeremie CLIC'0818 Impact of the resonance peak on the RMS ObjectPeak positionIntegrated RMS 4-feet table with weight 46Hz4.6nm Glued table with weight 92Hz0.3nm Sextupole on mover/support 100Hz0.26nm Quad on mover/support 76Hz1.1nm Adding up the integrated rms values keeps us under the 6- 7nm tolerances The honeycomb table fixed to the floor on whole surface, with adjusted movers validated for ATF2 Final Doublet support

19 A.Jeremie CLIC'0819 Effect of flowing water in FD magnets Study done at LAPP at the end of July 08 Effect of cooling water on the vibrations of final doublets

20 A.Jeremie CLIC'0820  No significant increase of vibrations with cooling water flowing=>impact of peak on integrated rms : 1.1nm 3D frequency analysis Quadrupole (QD0) with water flow GURALP sensors (0.2Hz – 50Hz)ENDEVCO sensors (10Hz – 100Hz) Measurement in time Start flowing water

21 A.Jeremie CLIC'0821 Sextupole (SD0) with water flow GURALP sensors (0.2Hz – 50Hz)ENDEVCO sensors (10Hz – 100Hz)  Some increase at higher frequency=> impact of peak on integrated rms: 0.7nm=>not significant Measurement in time 3D frequency analysis Start flowing water 80Hz Water flow in magnets has no significant effect on vibrations

22 A.Jeremie CLIC'0822 Installation at KEK from September 16 to September 25 2008

23 A.Jeremie CLIC'0823 Unpacking Installing beeswax on plates bolted to the ground Table comes down Installing “feet” and movers Shintake monitor Bending magnet Beam dump

24 A.Jeremie CLIC'0824 QD0 installed QD0 comes down Everything installed, centered and aligned in x, y and z, Thursday September 25 2008; Next step: BPM installation

25 A.Jeremie CLIC'0825 S-BPM installation October 15, 2008

26 A.Jeremie CLIC'0826 ATF2 rigid Final Doublet support chosen (vs. active support) SLAC FFTB movers adjusted to meet beam height Vibration measurements validate the rigid support choice Water flow in magnets has no significant effect on vibrations ATF2 Final Doublet support installed at KEK Conclusion Impatiently waiting for the beam to start!


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