STATUS OF THE MAIN BEAM QUADRUPOLE NANO-POSITIONING + SOME OBJECTIVES WITHIN PACMAN
- K. Artoos , S. Janssens, C. Collette (ULB), M. Esposito,
- C. Eymin, P. Fernandez Carmona
- K. Artoos , CLIC Workshop 2014
STATUS OF THE MAIN BEAM QUADRUPOLE NANO-POSITIONING + SOME - - PowerPoint PPT Presentation
STATUS OF THE MAIN BEAM QUADRUPOLE NANO-POSITIONING + SOME OBJECTIVES WITHIN PACMAN K. Artoos , S. Janssens, C. Collette (ULB), M. Esposito, C. Eymin, P. Fernandez Carmona K. Artoos , CLIC Workshop 2014 Outline 2 Intro + Link to the PACMAN
2
Intro + Link to the PACMAN project Design + Construction of the type 1 stabilisation
First measurements 2014
3
Possible mitigation techniques:
f
Stabilisation Alignment BPM Quad Fidu
4
B P M (m) 10-2 10-3 10-4 10-5 10-6 10-7 10-8 10-9 10-10
Alignment
BPM Nanopos.
Stabilisation
Range Accuracy Precision/resolution
Each system position should be unique above its resolution + known
Interaction ranges and accuracy
Conditions precision and accuracy cascaded systems
Conditions for > 6 d.o.f., Abbé errors + deformations
5
power leads, cabling, interconnects, ventilation, acoustic pressure)
Available space Integration in two beam module 620 mm beam height
Stiff actuating system K> 100 N/μm vertical+lateral Longitudinal transport locking Successfully tested with x-y prototype Ok, type 1 was not easy No manpower Tests in 2014
6
Flexural pins
7
A stiff but light Fixed frame around the mobile part, objective Natural frequencies > 100 Hz
8
Central fixed part Magnet mounted with assembly tool
9
10
11
12
201 Hz 140 Hz 122 Hz 241 Hz
13
14
Sensor Resolution Main + Main - Actuator sensor 0.15 nm No separate assembly Resolution No direct measurement
Capacitive gauge 0.10 nm Gauge radiation hard Mounting tolerances Gain change w. Orthogonal coupling Interferometer 10 pm Accuracy at freq.> 10 Hz Cost Mounting tolerance Sensitive to air flow Orthogonal coupling Optical ruler 0.5*-1 nm Cost 1% orthogonal coupling Mounting tolerance Small temperature drift Possible absolute sensor Rad hardness sensor head not known Limited velocity displacements
Seismometer (after integration) < pm at higher frequencies For cross calibration
K.Artoos, Stabilisation WG , 21th February 2013
15
+ actuator gauges, interferometer + seismometers (calibration)
16
Measured still on the assembly bench, not on the floor….
17
Horizontal motion: (with gain correction for roll)
18
Testing of the range
19
Type 1 Collocated pair X-y proto Seismometer FB max. gain +FF (FBFFV1mod): 7 % luminosity loss (no stabilisation 68 % loss)
EUCARD deliverable
20
Assemble type 4, all parts ready (- assembly tool) T1 + T4 : combine stabilisation and alignment Extensive testing stabilisation, nano positioning + in
Sensor out sourcing + testing Study alternatives for BDS
21
22
Heidenhain : 1nm resolution < 1000 CHF Renishaw: 1 nm resolution < 1000 CHF Smallest LSB can be used as quadrature …. 0.1 nm resolution is already possible Technological innovation: ABSOLUTE optical encoders Faster measurements
23
No stabilization 68% luminosity loss Seismometer FB maximum gain (V1) 13% Seismometer FB medium gain (V1mod) 6% (reduced peaks @ 0.1 and 75 Hz)
Inertial ref. mass 1 Hz (V3mod) 11% Inertial ref. mass 1 Hz + HP filter (V3) 3% Courtesy J. Snuverink, J. Pfingstner et al.
Commercial Seismometer Custom Inertial Reference mass K.Artoos, Stabilisation WG , 21th February 2013
Stef Janssens
24
Stabilisation Limitations:
(*alignment)
(wavelength light)
Expected maximum one
improvement resolution in next decade (Without major technological innovation) Low freq. is where you can win the most
Michelson Stabilised LASER
25
26
1&2 Parasitic roll
luminosity loss (J. Pfingstner)
27
28
0 𝜕 = 𝑙𝑏𝑑𝑢𝑣𝑏𝑢𝑝𝑠 𝑛𝑚𝑝𝑏𝑒
Stress < depolarisation stress A↑ 𝑊𝑝𝑚𝑣𝑛𝑓 ↑ 𝐷𝑞𝑨𝑢 ↑ For same Range: P↑ Resolution ↓ A Bandwidth is limited by Remark about load compensating springs:
Frequency Amplitude Range Force Load compensation reduces range + bandwidth Improves resolution *