Download - Chapter 5: Introduction of Cryomodule
![Page 1: Chapter 5: Introduction of Cryomodule](https://reader035.vdocuments.site/reader035/viewer/2022071613/6157460434567a5f1d53efd7/html5/thumbnails/1.jpg)
Chapter 5:
Introduction of Cryomodule Typical operating temperature of SRF cavities is 1.8 K~4.5 K
Helium circuit:
SRF cavities are immersed in liquid helium (helium vessel)
Helium supply and return lines are connected to helium vessel
Helium vessel can be pumped down to get lower temperature
Thermal design:
Minimize thermal loss
Typically uses multi-layer insulation and intermediate temperature boundary
in a vacuum chamber
Power coupler: Couples RF power to a cavity
Mechanical tuner
Keeps a cavity on resonance or within a certain range of detuning
HOM coupler: Couples HOMs damp and extract HOM
Magnetic shielding: Reduces ambient magnetic field
![Page 2: Chapter 5: Introduction of Cryomodule](https://reader035.vdocuments.site/reader035/viewer/2022071613/6157460434567a5f1d53efd7/html5/thumbnails/2.jpg)
Keep cold efficiently
One of the major concerns in cryomodules.
Large scale refrigeration plant is also one of major challenges for large scale
machines
Need a very careful consideration in thermal and safety points of view.
thermal: minimize thermal loss or optimize operating condition
safety: cryogenic incident (machine protection, personnel protection)
Insulation: reduce thermal heat transfer
convection: vacuum chamber
conduction: penetrations, supporting structures
thermal radiation: Multilayer insulation (MLI), thermal shield
![Page 4: Chapter 5: Introduction of Cryomodule](https://reader035.vdocuments.site/reader035/viewer/2022071613/6157460434567a5f1d53efd7/html5/thumbnails/4.jpg)
Conduction heat transfer
When a temperature gradient exists in a body or between objects that are in
physical contact, there’s an energy transfer from the high temperature region to
the low temperature region.
The heat transfer rate is proportional to area, temperature gradient
gradient re temperatu:
re temperatua offunction
property), (materialty conductivi thermalcalledconstant alproportion :
conductionfor area:where
][
x
T
k
A
Wx
TkAq
Ex. Each end of rod (2cm dia. And 0.5m long) is connected to thermal
boundaries at 4K and 300 K.
Stainless steel: assume constant k=3 W/mK q=1**1e-4*296/0.5=0.568 W
Copper: assume constant k=300 W/mK q=1**1e-4*296/0.5=56.8 W
![Page 5: Chapter 5: Introduction of Cryomodule](https://reader035.vdocuments.site/reader035/viewer/2022071613/6157460434567a5f1d53efd7/html5/thumbnails/5.jpg)
Thermal conductivity is a
function of material
When one performs a thermal
analysis in large temperature
range,
non-linear analysis is essential
using a FEM code.
From la
![Page 6: Chapter 5: Introduction of Cryomodule](https://reader035.vdocuments.site/reader035/viewer/2022071613/6157460434567a5f1d53efd7/html5/thumbnails/6.jpg)
Convection heat transfer
Heat transfer occurring due to the bulk motion of fluid (gas, liquid).
The transfer of energy between an object and its environment, due to fluid
motion.
Pressure < 10-4 torr: negligible effect
Radiation heat transfer
The transfer of energy to or from a body by means of the emission or
absorption of electromagnetic radiation Thermal
radiation
Electromagnetic Spectrum
![Page 7: Chapter 5: Introduction of Cryomodule](https://reader035.vdocuments.site/reader035/viewer/2022071613/6157460434567a5f1d53efd7/html5/thumbnails/7.jpg)
Energy radiated per unit time and per unit area by the ideal radiator is given
by the Stefan-Boltzmann law:
)KW/(m105.669 constant,Boltzmann -Stefan theis σ whereσTE 42-84
b
Inner cylinder: T1, A1, 1
Outer cylinder: T2, A2, 2
Ex.) Heat exchange between non-blackbodies
1) Two infinitely parallel plates
2) Two long concentric cylinders
3) layers of low emissivity material and insulators.
Ideally (q/A)with shields=(q/A)without shield/(1+n), n=number of layers
11/ε1/ε
)Tσ(Tq/A
21
4
2
4
1
1))(1/ε/A(A1/ε
)T(TσAq
2211
4
2
4
11
![Page 8: Chapter 5: Introduction of Cryomodule](https://reader035.vdocuments.site/reader035/viewer/2022071613/6157460434567a5f1d53efd7/html5/thumbnails/8.jpg)
Phase diagram of 4He
point
0.0497 atm
2.264 atm
Upper point
1.76 K, 29.8 atm
Superfluid:
A phase of matter in which viscosity of a
fluid vanishes.
Discovered in 1937 by Kapitza, Allen, and
Misener.
L. Landau won the Novel Prize in Physics
‘phenomenological and semi-microscopic
theory of superfluidity of 4He’.
Film creeping Thermo-caloric effect
saturated
![Page 9: Chapter 5: Introduction of Cryomodule](https://reader035.vdocuments.site/reader035/viewer/2022071613/6157460434567a5f1d53efd7/html5/thumbnails/9.jpg)
Cryogenic efficiency
Ideal Carnot efficiency
opambient
op
idealTT
Tη
Ex. Ideal case: ideal=0.345 for 300K77K,
ideal=0.014 for 300K4.2K
In practice, actual efficiency is much lower than this ideal case.
/ideal= ratio typically ranges 0.1~0.35 (<0.1 in small systems)
Smaller machine has lower efficiency.
As technologies improve, efficiencies are getting higher.
Some reference numbers for scaling
Room temperature power/power at 4.5 K: 250~350
Room temperature power/power at 2 K: 1100~1300
Rough scaling:
If we have 100 W load at 2 K we need ~120 kW cryogenic system at least.
(we will re-visit this concern for machine efficiency estimation in Chapter 7)
![Page 10: Chapter 5: Introduction of Cryomodule](https://reader035.vdocuments.site/reader035/viewer/2022071613/6157460434567a5f1d53efd7/html5/thumbnails/10.jpg)
0
5
10
15
20
25
30
35
40
2 2.5 3 3.5 4 4.5 5 5.5
Temperature (K)
heat of vaporization at saturation(J/10cc)
heat of vaporization (J/g)
density at saturation (g/100cc)
Helium properties at saturation
Low efficiency + small heat capacity + expensive: need very careful design
![Page 11: Chapter 5: Introduction of Cryomodule](https://reader035.vdocuments.site/reader035/viewer/2022071613/6157460434567a5f1d53efd7/html5/thumbnails/11.jpg)
Ex. SNS Refrigerator System
Helium Refrigerator System
2400 Watt Capacity@ 2.1Kelvin and
8300 Watt Shield Load @ 38/50Kelvin
15g/s Liquefaction at 4.5Kelvin
80g/s Liquefaction Mode
Cryogenic Transfer Line System
4.5K & 38K Helium Supply and
4.0K & 50K Helium Return
Whole system consumes >3 MW electricity CRYO MODULES
PURIFIERS GAS STORAGE
WARM
COMPRESSORS
SYSTEM
OIL
REMOVAL
CHL MAIN COLD BOX
(4.5K) NITROGEN
DEWAR
HELIUM
DEWAR
2.1K
COLD BOX
COLD
COMPRS
SUPPLY
CAN
RETURN
CAN TRANSFER
LINES
P.S. P.R. S.S. S.R.
![Page 12: Chapter 5: Introduction of Cryomodule](https://reader035.vdocuments.site/reader035/viewer/2022071613/6157460434567a5f1d53efd7/html5/thumbnails/12.jpg)
SNS CHL layout
![Page 13: Chapter 5: Introduction of Cryomodule](https://reader035.vdocuments.site/reader035/viewer/2022071613/6157460434567a5f1d53efd7/html5/thumbnails/13.jpg)
Warm Compressor
4 K Cold Box
2 K Cold Box
![Page 14: Chapter 5: Introduction of Cryomodule](https://reader035.vdocuments.site/reader035/viewer/2022071613/6157460434567a5f1d53efd7/html5/thumbnails/14.jpg)
Schematics of cryomodule
Helium return/pumping port Helium supply line
Vacuum chamber
RF power coupler
Multi-layer
insulator
Helium vessel
Thermal
shield
Magnetic
Field shield
Beam
pipe
Mechanical
tuner
![Page 15: Chapter 5: Introduction of Cryomodule](https://reader035.vdocuments.site/reader035/viewer/2022071613/6157460434567a5f1d53efd7/html5/thumbnails/15.jpg)
Cavity with
Helium vessel
Cavity string
Space frame and thermal shield
![Page 16: Chapter 5: Introduction of Cryomodule](https://reader035.vdocuments.site/reader035/viewer/2022071613/6157460434567a5f1d53efd7/html5/thumbnails/16.jpg)
Ex: SNS Cryomodule
End can for
Helium supply
End can for
Helium return
Power couplers and
waveguide transitions
Helium
vessel
Thermal shield and
Space frame
Vacuum
Chamber
Magnetic field
Shield
![Page 17: Chapter 5: Introduction of Cryomodule](https://reader035.vdocuments.site/reader035/viewer/2022071613/6157460434567a5f1d53efd7/html5/thumbnails/17.jpg)
Medium Beta Cavity
Fundamental
Power Coupler
HOM
Coupler
HOM
Coupler
Field
Probe
NbTi Dished
Head
Titanium Bellows
NbTi Dished
Head
Stiffening Rings
2 - Phase Return Header
Ex. SNS Cavity Assembly
![Page 18: Chapter 5: Introduction of Cryomodule](https://reader035.vdocuments.site/reader035/viewer/2022071613/6157460434567a5f1d53efd7/html5/thumbnails/18.jpg)
Comparisons of
various modes of
helium heat
transfer
Downward:
Upward:
metal
helium
metal
helium
![Page 19: Chapter 5: Introduction of Cryomodule](https://reader035.vdocuments.site/reader035/viewer/2022071613/6157460434567a5f1d53efd7/html5/thumbnails/19.jpg)
Resonance frequency control
Slow tuner (mechanical tuner):
Compensate static or quasi-static detuning
(initial offset or slow drift of resonance frequency)
Compress/expand cavity length typically using stepper motor
Coarse tuning: usually put the resonance frequency in the allowable band
Typical tuning range: about +/- few mm
Types:
CEA/Scalay tuners
blade tuner (DESY, INFN)
side jack tuner (KEK)
![Page 20: Chapter 5: Introduction of Cryomodule](https://reader035.vdocuments.site/reader035/viewer/2022071613/6157460434567a5f1d53efd7/html5/thumbnails/20.jpg)
Slow
Tuner
Helium
Vessel
Fast
Tuner
Piezo
Actuator
Flexure Connection
to Helium Vessel (2X)
Motor & Harmonic
Drive
INFN, Blade tuner for ILC
SNS tuner (saclay-TTF generation I type)
Side Jack tuner (KEK)
![Page 21: Chapter 5: Introduction of Cryomodule](https://reader035.vdocuments.site/reader035/viewer/2022071613/6157460434567a5f1d53efd7/html5/thumbnails/21.jpg)
Fast tuner:
Fine & fast tuning
Pulsed operation: Compensate Lorentz force detuning within RF pulses
High Qext: Compensate microphonics
Piezoelectric actuators: electromechanical actuator. Linear
electromechanical interaction between the mechanical and the
electrical state in piezoelectric materials.
typical tuning range: few to several mm
magnetostrictive actuator: solid state magnetic actuator. A current
driven coil surrounding the magnetostrictive rod generates the
expansion of the rod.
![Page 22: Chapter 5: Introduction of Cryomodule](https://reader035.vdocuments.site/reader035/viewer/2022071613/6157460434567a5f1d53efd7/html5/thumbnails/22.jpg)
Voltage is applied to the piezoelectric actuator device which make the piezo
stack shrink/expand
Piezo
stack Piezo-stack
voltage input
Shrink/expand
Piezoelectric actuator
Typically
Stroke: 70~80 mm for 100 mm stack at room temperature
stroke at cryogenic temperature 5~10 % of that at room temperature
Resolution: ~Hz
![Page 23: Chapter 5: Introduction of Cryomodule](https://reader035.vdocuments.site/reader035/viewer/2022071613/6157460434567a5f1d53efd7/html5/thumbnails/23.jpg)
23/39 September 21, 2006, Accelerator
Performance
Model vs. Reality
1. On the CAD Model
2. Mounted On the Bare Cavity
3. Reality – Pretty Complicated
3
![Page 24: Chapter 5: Introduction of Cryomodule](https://reader035.vdocuments.site/reader035/viewer/2022071613/6157460434567a5f1d53efd7/html5/thumbnails/24.jpg)
Power Coupler
Function: Deliver RF power
Coupling Qex
Concerns: Transmission loss
Thermal stability
Mechanical stability
Simplicity
Reliability
Cost
Multipacting
Frequency
Power needed
Coupling
Types
Cooling
Window
![Page 25: Chapter 5: Introduction of Cryomodule](https://reader035.vdocuments.site/reader035/viewer/2022071613/6157460434567a5f1d53efd7/html5/thumbnails/25.jpg)
TTF3 coupler (ILC) SNS power coupler
Coaxial
Waveguide
![Page 26: Chapter 5: Introduction of Cryomodule](https://reader035.vdocuments.site/reader035/viewer/2022071613/6157460434567a5f1d53efd7/html5/thumbnails/26.jpg)
Multipacting simulations around ceramic window
![Page 27: Chapter 5: Introduction of Cryomodule](https://reader035.vdocuments.site/reader035/viewer/2022071613/6157460434567a5f1d53efd7/html5/thumbnails/27.jpg)
Coupler conditioning