ATF2: final doublet support

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Presentation transcript:

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

Outline FD support specifications Initial active support study Rigid support on intermediate feet Final rigid support Measurements with water flow Installation photos Conclusion A.Jeremie CLIC'08

Shintake Monitor: information on the beam size ATF2 Layout Shintake Monitor: information on the beam size Final doublets A.Jeremie CLIC'08

FD layout IP 1225 SBPM QC3 FFTB 2.13 S3.00 SF1 QF1 76.2 450.1 575 200 180 311.9 785 380 45 65 53.1 SD0 QD0 1940 mm What is needed to support all these components? A.Jeremie CLIC'08

ATF2 specifications For QD0 at ATF2: 6-7nm tolerance ATF ground motion 6-7nm 0.1Hz ~50Hz For QD0 at ATF2: 6-7nm tolerance Repetition rate 1Hz=> need a “mechanical” stabilisation from 0.1Hz (below, the beam based alignment works) Two solutions possible: Isolate/cut vibrations in the desired frequency range Push the first resonance peaks at higher frequencies where ground motion is lower A.Jeremie CLIC'08

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 Initial suggestion: CERN wanted to contribute by sending the commercial TMC table Honeycomb table Isolator: Passive => turned OFF Active => turned ON A.Jeremie CLIC'08

Vertical direction: Integrated RMS Vibrations of the passive TMC table Vertical direction: Integrated RMS ~Same response Damping Amplification Amplification 27 0.5 30 Below 0.5Hz: No amplification or damping on the table Above 0.5Hz: Amplification Above 30Hz: damping begins A.Jeremie CLIC'08

Vertical direction: integrated RMS Vibrations of the active TMC table Vertical direction: integrated RMS Below 0.8Hz: Amplification on the table Above 0.8Hz: Damping on the table  Factor 7 of damping above 1.5Hz A.Jeremie CLIC'08

Good ground motion coherence: measured on KEK site Specifications 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 Shintake monitor Interference fringes Final doublets If Shintake Monitor and FD on separate active supports, coherence is lost Beam Ground 4m Good ground motion coherence: measured on KEK site  Separate stiff supports rigidly fixed to the floor Study the honeycomb block but without feet A.Jeremie CLIC'08

Table without any masses Table with masses simulating the weight of FD “simple” Simulation: just a block with the right boundary conditions=> to see the evolution First resonance peak in free-free configuration: 230Hz Boundary conditions: table put on / fixed to 4 rigid supports at its corners Too low! With masses: 26.2Hz  Fall of the eigenfrequency Without any masses: 56.2Hz  Lower than in free configuration! Table without any masses Table with masses simulating the weight of FD velocity sensors accelerometers Microphones A.Jeremie CLIC'08

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 Bien montrer au depart les 2 gros pics (avec et sans masses) sur la frequence de resonance et dire qu’on est sur que ce sont deux freq de resonance grace a la phase zomme. Dire ensuite qu’il ya des pics en plus qui ne sont pas des freq de resonance: le pic a 27Hz n’en est pas un a cause de la phase qui est a 4 degre et le pic a 52Hz n’en est pas un car trop proche du pic de resonance avec masses; Impact of the different vibration peaks on relative motion A.Jeremie CLIC'08

Relative motion between table and floor Integrated RMS of relative motion between table and floor to predict on the ATF site Calculation to perform by integrating the vibratory behaviour of the table measured at LAPP and the data of ATF ground motion Calculation performed for these specific needs: A.Jeremie CLIC'08

Relative motion between table and floor Integrated RMS of relative motion at ATF 6.7nm Total relative motion ([0.17; 100]Hz): 6.7nm  Above tolerances (6nm)! Contribution of the peak alone: [30; 100]Hz: 4.6nm 4.6nm  Need to push resonances to higher frequencies where ground motion is lower A.Jeremie CLIC'08

Is the honeycomb table rigid enough? Table fixed on 4 rigid supports at the 4 corners 2 tri-axis accelerometers Michael GUINCHARD (CERN) Z X Y Impact hammer on table Modal deformations for each resonance (up to 150Hz) In the three axis 6 first modes: rigid body modes in 6 degrees of freedom Modes 1) T-X 2) T-Y 3) R-Z 4) T-Z 5) R-Y 6) R-X Frequency (Hz) 34.8 41.8 60.6 80.6 103.9 136.0 Damping (%) 2.8 2.6 2.4 2.3 2.1 4.0 T: Translation R: Rotation The table is a rigid body, but the feet are not  Fix table on whole surface to remove these modes A.Jeremie CLIC'08

3 steel plates bolted to the floor Table fixed directly to the floor on 1 entire side simulation With masses: 135.2Hz  Fall of the eigenfrequency but still high Without any masses: 526.1Hz  Even higher than in free configuration! Honeycomb table 3 steel plates bolted to the floor Bees wax Set-up can be moved in the future 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 A.Jeremie CLIC'08

FD configuration Quads, sextupoles and movers :SLAC (from FFTB) IP From floor to mover: LAPP (new) BPM+support: KNU, LAPP QD0 IP QF1 SD0 SF1 Adjustment possible in x, y, z with shims (0.05mm) and adjustment pushers for 1.2m beam height 2.4m beeswax Room for slings for table lifting A.Jeremie CLIC'08

Table fixed on one entire face to the floor Experimental set-up Honeycomb table Bees wax 3 steel plates bolted to the floor No masses: no peak With masses: 92Hz  Good boundary conditions chosen for the table: Relative motion should be very low compared to tolerances A.Jeremie CLIC'08

Impact of the resonance peak on the RMS Object Peak position Integrated RMS 4-feet table with weight 46Hz 4.6nm Glued table with weight 92Hz 0.3nm Sextupole on mover/support 100Hz 0.26nm Quad on mover/support 76Hz 1.1nm 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 A.Jeremie CLIC'08

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 A.Jeremie CLIC'08

Quadrupole (QD0) with water flow Measurement in time GURALP sensors (0.2Hz – 50Hz) ENDEVCO sensors (10Hz – 100Hz) Start flowing water No significant increase of vibrations with cooling water flowing=>impact of peak on integrated rms : 1.1nm 3D frequency analysis A.Jeremie CLIC'08

Sextupole (SD0) with water flow Measurement in time GURALP sensors (0.2Hz – 50Hz) ENDEVCO sensors (10Hz – 100Hz) 80Hz Start flowing water 3D frequency analysis Some increase at higher frequency=> impact of peak on integrated rms: 0.7nm=>not significant Water flow in magnets has no significant effect on vibrations A.Jeremie CLIC'08

Installation at KEK from September 16 to September 25 2008 A.Jeremie CLIC'08

Installing beeswax on plates bolted to the ground Unpacking Beam dump Table comes down Installing “feet” and movers Bending magnet Shintake monitor A.Jeremie CLIC'08

QD0 installed QD0 comes down Everything installed, centered and aligned in x, y and z, Thursday September 25 2008; Next step: BPM installation A.Jeremie CLIC'08

S-BPM installation October 15, 2008 A.Jeremie CLIC'08

Conclusion Impatiently waiting for the beam to start! 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 Impatiently waiting for the beam to start! A.Jeremie CLIC'08

A.Jeremie CLIC'08

11 novembre 2008 A.Jeremie CLIC'08