Beryllium Windows Lorentz Force Detuning and Field Enhancement
- F. Marhauser,
MuPlus, Inc. 2014-01
Beryllium Windows Lorentz Force Detuning and Field Enhancement F. - - PowerPoint PPT Presentation
Beryllium Windows Lorentz Force Detuning and Field Enhancement F. Marhauser, MuPlus, Inc. 2014-01 Be Windows Beryllium windows (transparent for muons) close cavities such that neighboring cavities (closely packed) can be
MuPlus, Inc. 2014-01
packed) can be independently powered and adjusted in phase
thickness = 157 um, Radius = 8 cm, brazed between annular Be frames
Be foil (99% purity, IF-1) brazed between two annular Be frames (98.5% purity, PS-200)
2001 window still wavy
to measure and simulate
2002
11.5 ppm/K for 99% pure Be and noted deviations for ring with 98.5% Be purity
First successful Beryllium window manufactured for a prototype cavity, Be window is brazed between two annular copper frames
pre-curved, pre-stressed Be windows conceived (designed by Oxford University) designed to remain rigid during thermal cycling
2005
Prototype 201.25 MHz (MICE) cavity
the window
(but no thickness cited). Yet, the latter caused pulse-to-pulse instabilities
to-pulse instabilities, not really explained in this of other papers, very questionable if this can help us
HCC cavities (slides to come)
potential deflections
(frequency shift observed by geometry change was -379 kHz)
1) reference (0 thickness) equilibrium transverse emittance: 0.35 mm 2) 30 µm thick windows equilibrium transverse emittance: 0.60 mm, i.e. almost factor 2 larger
as function of window thickness
several mesh cells per thickness (down to 500 µm window thickness was feasible)
(e.g.: ~4 days CPU time required for 500 µm case)
cavity vacuum and mesh cavity wall and mesh
Units Copper (OFHC) Beryllium I Beryllium II Source NIST Wikipedia Brush Wellman IF1 Alloys, > 99.8% Be Mechanical Calculations Young’s modulus GPa 128.8 287 303 Poisson ratio 0.344 0.032 0.070 CTE 1/K 1.66e-5 1.13e-5 1.15e-5 Thermal calculations (usually non-linear function with temperature used) Thermal Conductivity W/(m·K) 390 200 216 RF Calculations Electrical Conductivity 1/(Ω·m) 5.81e7 2.78e7 2.33e7
Note: TEM3P does not consider β < 1
Be II, note: No detuning due to RF heating considered yet
Window thickness (µm)
Deflection @ 24.1 MV/m (mm) Frequency Detuning at 10/20/30 MV/m (MHz) Comments on Feasibility 30 355 277/1107/2490 impossible 60 46 36/144/324 impossible 120 6 5/19/42 very unlikely to work 380 (like MICE) 0.2 0.2/0.6/1.4 maybe possible at lower field levels (but expect significant emittance increase) 1000 0.012 0.01/0.04/0.09 likely to work (but expect significant emittance increase)
Window thickness (µm)
Deflection @ 24.1 MV/m (mm) Frequency Detuning at 10/20/30 MV/m (MHz) Comments on Feasibility 30 355 277/1107/2490 impossible 60 46 36/144/324 impossible 120 6 5/19/42 very unlikely to work 380 (like MICE) 0.2 0.2/0.6/1.4 maybe possible at lower field levels (but expect significant emittance increase) 1000 0.012 0.01/0.04/0.09 likely to work (but expect significant emittance increase)
would cancel pressure since any power trip in one cavity could disrupt window
equivalent heat transfer coefficient = 72 W/(m2·K) based on Reynolds and Prandtl number, could be larger depending on average velocity of gas (which is an input parameter)
temperature rise within windows seems to be small thanks to gas cooling
0.5 mm windows h = 72 W/(m2·K)
temperature (K)
0.5 mm windows h = 72 W/(m2·K)
temperature (K)
2002
1) Use stepped window to improve thermal capability over uniform foil 2) Use ribbed window to decrease muon scattering, while providing mechanical integrity e.g. ‘waffle’ pattern with reinforced ribs)
e.g. twice the thickness at some radius
3) Gridded windows with various concepts and arrays (touching, non-touching, merged)
4) Gridded windows with various concepts and arrays (touching, merged) 2004 Thesis
Tref = 0 deg. C
baseline diameter = 9.53 mm
(even though models employ rather large tube diameters)
baseline diameter = 9.53 mm
(limit for workstation RAM with Poisson/Superfish)
axis of rotation
1 kV 0 kV free space
adjacent tubes do not perturb field too much (i.e. center between hor./vert. tubes)
then calculate FE factor for each gap/R with hyperbolic fit, i.e. boundary limit in infinity
then calculate FE factor for each gap/R with hyperbolic fit, i.e. boundary limit in infinity
increases with smaller tube radius (R), i.e. thin tubes widely spaced are problematic
given for baseline, but seems to be right
3/8" diameter cases 9/16" diameter cases case 1 2 3 4 5 6 waffle design 4 x4 6 x 6 8 x 8 4 x 4 6 x 6 8 x 8 R (mm) 4.7625 4.7625 4.7625 7.14375 7.14375 7.14375 g (mm) 25.41 13.76 7.94 20.64 9.00 3.18 distance c-c 34.93 23.29 17.47 34.93 23.29 17.47 g/R 5.33 2.89 1.67 2.89 1.26 0.44 3D FEA ANSYS model (2004 thesis, M. Alsharo’a ) 1.90 1.65 1.42 1.75 1.52 1.31 Poisson 2D model (same g/R) 2.26 1.87 1.67 1.87 1.60 1.47
given for baseline, but seems to be right
larger than on axis
given for baseline, but seems to be right
larger than on axis
R = 5mm (fixed)
waffle windows (2D model) DL cavity (2D model)
considers the max. electrical field on the metal surface (beam tube opening)
cavities be employed? Beam dynamics must tell.
electrical field contours
beam dynamics may not allow small fill factor should be further elaborated RF leakage could be kept small with small radius