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INFN-MI: Status

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Title: INFN-MI: Status


1
INFN-MI Status
  • Angelo Bosotti, Nicola Panzeri, Paolo Pierini

2
Planning
  • Milestones
  • Report on final tuner design by end 2005
  • Tuner construction and testing by mid 2006
  • Parallel historical tuner activity
  • Started within TTF, now ILC/XFEL
  • In CARE/JRA1/WP8
  • Report in preparation for 1.3 GHz b1 cavities
    (Angelo Bosotti)

3
LFD compensation at high gradients (Dn KL E2)
Evolution of the tuner concept, with integration
of the fast LFD action 1.3 GHz system under
fabrication right now
4
Cavity A characterization
Parameter Value
Design Frequency 704.4 MHz
Geometrical b 0.47
Iris radius 40 mm
Cell to cell coupling 1.34
R/Q 180 Ohm
G 160 Ohm
Epeak/Eacc 3.57
Bpeak/Eacc 5.88 mT/(MV/m)
Stiffening ring radial position 70 mm
Cavity longitudinal stiffness (Kcav) 1.248 kN/mm
Frequency sensitivity (longitudinal) -353.4 kHz/mm
Vacuum freq. coeff. (constrained) 84.7 Hz/mbar
Vacuum reaction force at boundary 3.7 N/mbar
Lorentz coefficient (constrained) 3.7 Hz/(MV/m)2
Lorentz reaction force at boundary 0.177 N/(MV/m)2
Previous estimation 7 Hz/(MV/m)2 only on
half-cell geometry, but also, mechanical load
condition was overestimated by a factor of 2.
Present calculation on the full geometry.
5
Where did we stand in tests with cavity A?
  • Vertical tests 3 at Saclay, 3 at JLAB

Huge spread in static measurements! And off by a
factor 10
6
Influence of boundary conditions
  • Linear superposition of 2 effects
  • Shape deformation (fixed boundary)
  • Cavity shortening (cavityboundary combined
    stiffness)

Analytical derivation of full behavior requires
solution of only 2 load cases
7
Cavity frequency response under arbitrary b.c.
  • Frequency response of the cavity can be then
    understood as a function of the external boundary
    condition
  • Using values from the cavity mechanical
    characterization and Slater perturbation theorem

8
The RF test frames
Saclay tests in 2004
Jlab tests in 2003/2005
Q Are they sufficiently stiff?
9
JLAB frame
  • Cavity is held at He tank disks with a bar
  • Dish stiffness is greatly reduced!

Large tube (FPC) side Large tube (FPC) side
Nominal KDbig 26 kN/mm
JLAB load case 2 kN/mm
Large tube (FPC) side Large tube (FPC) side
Nominal KDsmall 40 kN/mm
JLAB load case 2.1 kN/mm
Component Stiffness
Ti rods (4) 142 kN/mm
Support plates (2) 11 kN/mm
He tank dish, coupler side 2 kN/mm
He tank dish, opposite side 2.1 kN/mm
Overall stiffness 0.93 kN/mm
10
Saclay frame
Displacement load condition Displacement load condition
dz 1 mm
Reaction force 2.536 kN
Force load condition Force load condition
Applied force 1.000 kN
Max dz 0.444 mm
Average frame stiffness Average frame stiffness
kframe 2.39 kN/mm
A NO, both are not stiff enough
11
Correlation with measured KL
  • Mechanical models assume perfect joints and no
    slack contacts between components
  • In reality joints, screws, etc.

12
Alternative check
  • From the Saclay data at low temperatures (2.2 to
    1.7 K, where the bath pressure is more stable),
    an average value of Dn/DP of -462 Hz/mbar can be
    evaluated
  • Kext of 1.15 kN/mm can be estimated, coherent
    with the model discussed before
  • From the JLab data an average of Dn/DP of -1020
    Hz/mbar in the same temperature range can be
    estimated.
  • Comparable to a nearly free cavity behavior
    (nominal -966 Hz/mbar), with a negligible
    external stiffness condition with respect to the
    cavity stiffness, again, coherent with the model
    discussed before

13
Summary on static KL
  • RF test data is understood
  • Weak constraints for the cavity length
  • Low beta geometry very sensible to external
    boundary condition (low cavity stiffness)
  • Behavior of KL agains Kext allows to set tuner
    stiffness requirements under operating conditions
  • Interaction with CEA (GD) has shown a nearly
    perfect agreement of static LFD modeling
  • both calculation modes based on Slater
    perturbation theorem, but different and
    independent implementations, especially
    concerning the mechanical part of the codes
    (ANSYS vs CASTEM)
  • Planning for dynamic LFD calculations
  • harmonic analysis Slater for cavity transfer
    function and piezo tf
  • time dependent analysis overelongation?
  • need time for the development and check the
    procedures

14
Requirements for 704.4 MHz
  • One of the uncertainties of the piezo materials
    is still their stroke capabilities at the low
    operating temperatures
  • Assuming a 3 mm stroke to cavity (long piezos)
  • safe? SRF/WP8 work in progress
  • a 1000 Hz frequency offset can be compensated
    during the fast tuning action
  • With a design accelerating field of 8.5 MV/m,
    this implies that the overall KL in the operating
    condition should be limited to around -10
    Hz/(MV/m)2
  • We took a 50 margin for dynamic LFD? M.Liepe
    factor 2
  • In order to achieve this condition with these
    rather soft cavities the combined stiffness of
    the He Tank and tuner system needs to provide
    10 kN/mm
  • At 20 kN/mm we are hitting limit with He tank
    dish stiffness

15
Tuner requirements
  • Extracting out the Tank and end dish stiffness
    contribution (total of 15 kN/mm), the requirement
    for the tuner becomes about 20 kN/mm

Actual experimental stiffness including leverage
(TTF)
16
On the road to finalize tuner design
Now we are fine-tuning the tuner stiffness by
slight adjustments of the blade number length and
slope for final optimization before emitting
final drawings for Cavity A
Will ask for bids in late 2005 and Order main
tuner mechanical components before end of
year (INFN contribution is available) Then
fabrication time will take 4-6 months
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