SRF Cavity Preparation and Limitations - CERN · – Process of connecting subcomponents to cavity...
Transcript of SRF Cavity Preparation and Limitations - CERN · – Process of connecting subcomponents to cavity...
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SRF Cavity Preparation and Limitations
J. Mammosser (ORNL)
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Outline:• Cavity Qualifying Test Limitations (Vertical Test)
– Vertical Test Results– Main Limitations (Field emission, Thermal breakdown,
Multipacting)– Not Covered - (Q-disease, Trapped Magnetic Field, High Field Q-
Drop)– Performance History
• Today's Standard Processing Procedures– Standard Processing Sequence (30-40 MV/m)– Surface cleaning, Chemistry, HPR, Heat treatment, Baking, Helium
Processing• Future Process Improvements
– Vertical EP, Plasma Cleaning, Integrated Process Automation
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When Proper Procedure and Attention to Detail Occur –
Rongli Geng 3
• 4 out of 5 reached > 35 MV/m after 1st light EP• A15 quench limited by one defect in one cell
• A15 quench source identified by T-mapping and optical inspection• A12 data after 1st light EP is not shown• A12 data shown are after 2nd light EP
Crawford et al
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However performances are not always ideal
11
10
9
80 25 50 MV/m
Accelerating Field
Residual losses
Multipacting
Field emission
Thermal breakdown
Quench
Ideal
RF Processing
10
10
10
10
Q
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Field Emission
Characterized by an exponential drop of the Q-value
Associated with production of x-rays and emission of dark current
Today good processes and procedures can minimize or eliminate this issue but its always there at some level
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Field Emission
1,E+09
1,E+10
1,E+11
0 2 4 6 8 10 12 14 16 18 20
Qo
E (MV/m)
SNS HB54 Qo versus EaccMultipacting limited at 16MV/m 5/16/08 cg
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Field Emission
0
0
0
0
1
10
100
1000
0 5 10 15 20 25
mR
em/h
r)
E (MV/m)
SNS HTB 54 Radiation at top plate versus Eacc 5/16/08 cg
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Field Emission from Ideal SurfaceFowler-Nordheim model
( )
⎥⎥⎥
⎦
⎤
⎢⎢⎢
⎣
⎡×
−×
=E
EAeEIFN
FN
βφ
φβ 2
3326 1083.6exp1054.1)(
FactortEnhancemenFieldFieldElectricE
AreaSurfaceEmitterEffectiveAfunctionwork
FN
e
==
==
β
φ
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Geometrical Origin of Field Enhancement
Smooth particles show little field emission
Simple protrusions are not sufficient to explain the measured enhancement factors
Possible explanation: tip on tip (compounded enhancement)
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Localized Defects
mμ20≈
mμ20≈
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Field Emission
mμ1015×≈
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Example of Field Emittors
V
Ni Ni
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C, O, Na, In Al, Si
Stainless steel
Melted
Melted
Melted
Example of Field Emitters
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Looking Inside the Cavity During Testing
• Before onset of Radiation outside dewar
• Radiation present on detector and in CCD image
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Enhancement by Absorbates
Adsorbed atoms on the surface can enhance the tunneling of electrons from the metal and increase field emission
Beta Enhancement Factors1 - tip on tip2 - absorbed gas3 – insulator enhancement (field distortion)
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Qo vs. Eacc Radiation vs. Eacc
If this cavity is limited at this condition, what is the limiting factor?Field emission?
MP
FE
Field Emission ?MP! And then later on Field Emission !VTA
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17b in open loop
Radiation Increase(in log scale)
Eacc
CCG5
10
15
20Eacc=16.5
Time (us) Time (us)
[MV/m]Eacc=17.5
Pulsed operationWaveform tells us
what is happening inside
17bRadiation at Eacc=16.5 (Elim=17.5 MV/m due to FE!)
Radiation waveform
Field emissionEx. 17b individual
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Thermal Breakdown
1 4log(ΔT [mK])
Localized heating
Hot area increases with field
At a certain field there is a thermal runaway, the field collapses
sometimes displays a oscillator behavior
sometimes settles at a lower value
sometimes displays a hysteretic behavior
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Thermal Breakdown
Thermal breakdown occurs when the heat generated at the hot spot is larger than that can be evacuated to the helium bath
Both the thermal conductivity and the surface resistance of Nb are highly temperature dependent between 2 and 9K
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Thermal Breakdown
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Pd
T
T
T
Ts-Tb
q
T
Rs
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Surface Resistance vs Temperature
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Power Dissipation vs Temperature
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Niobium Specific Heat vs Temperature
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Heat Transfer Density (Bath-Niobium)
• Tb –Helium Bath• Ts – Niobium
Surface Helium side
• q- heat density
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Niobium Thermal Conductivity vs Temperature
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Thermal Breakdown
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Thermal Conductivity of Nb
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Residual Resistance Ratio
RRR is the ratio of the resistivity at 300K and 4.2K
(300 )(4.2 )
KRRRK
rr
=
RRR is related to the mean free path.
For Nb: ( 4.2 ) 27 (Å)l T K RRR= »
RRR is related to the thermal conductivity
For Nb: ( 4.2 ) / 4 ( )-1 -1W. m . KT K RRRl = »
At normal conducting and cryogenic state
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Thermal Breakdown
Breakdown field given by(very approximately):
4 ( )T c btb
d d
T THr R
k -=
κT: Thermal conductivity of NbRd: Defect surface resistanceTc: Critical temperature of NbTb: Bath temperature
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Kim ORNL
Quenching pattern examples in the end group
during pulse
during gape-loadings around HOM antenna
e-loading at OC
Low RRR & long path to the thermal sinkThermal margin is relatively small,Intermediate stage at the end-group Results in thermal quench/gas burst
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Thermal Breakdown
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Rongli Geng
33
700 μm dia. defect in AES5
300 μm dia. defect in A15
JLab T-mapping and High-Resolution Optical Inspection
hot spot near equator EBW
Precursor T-jumpat quench location
Ciovati et al
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Multipacting
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Multipacting
1,E+09
1,E+10
1,E+11
0 2 4 6 8 10 12 14 16 18 20
Qo
E (MV/m)
SNS HB54 Qo versus EaccMultipacting limited at 16MV/m 5/16/08 cg
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Multipacting
Multipacting is characterized by an exponential growth in the number of electrons in a cavity
Multipacting requires 2 conditions:
Electron motion is periodic (resonance condition)
Impact energy is such that secondary emission coefficient is >1
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Multipacting
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Secondary Emission in Niobium
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More Then Just Cell Mulitpacting4 MP Locations in the SNS Cavity Observed:
Cell Equator
Input coupler
Beam pipe Transitions
HOM Hooks
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Separating MP and Field Emission Contributions to X-rays Observed
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Performance History DESY cavity experience
L. Lijie’s summary of DESY cavity databank, DESY, 2006
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Performance from my experience• In the early 1990’s gradients were mainly limited around15MV/m
vertical test and 10MV/m in machines– Field emission dominated the performance– Preparation procedure
• Bulk removal BCP, RF tuning, Degreasing, Final light BCP, DI water rinsing, Assembly
• By the mid 1990’s high pressure rinse was established as a new cleaning method to reduce field emission
• Early 2000 – Gradients had reached 20-25 MV/m vertical test which correlated to
machine performance as well– Electropolish chemistry was reintroduced and showed gradients could be
pushed to 30-35MV/m
• Today the focus is on reproducibility with occasional 40MV/m performances
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Standard Process Generalized• Heavy chemical etch (EP or BCP)
– Removal of damaged surface layer (100-150um) caused by fabrication and handling
• Removal of surface contamination– Ultrasonic cleaning of surface with detergent and DI water, heated and or– Alcohol rinse of surface to remove chemical residues
• Heat treatment (600-800C in vacuum furnace)– Removes hydrogen from the bulk niobium to reduce the risk of Q-disease
• RF tuning and mechanical inspection– Last chance to prepare cavity for operational use– Field profile, calibration of test probes, check mechanical structure
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Standard Process Generalized cont.• Removal of surface contamination
– Ultrasonic cleaning of surface with detergent and DI water, heated
• Light chemical etch (EP)– Remove any risk from damage during handling and furnace contamination
• Removal of surface contamination (chemical residues)– Ultrasonic cleaning– Alcohol rinse
• High pressure rinse (UPW) + Class 10 drying of cavity– Reduction of field emission sources, surface particulates– At least two passes over entire surface
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Standard Process Generalized cont.
• Assembly of subcomponents (most hardware at this step)– Process of connecting subcomponents to cavity openings– Slow and careful steps, high level of attention to detail– Ionized nitrogen gas blow off (cleaning) of subcomponents and hardware – Assembly optimized to reduce particulate contamination into cavity
surface
• High pressure rinse (UPW) + Class 10 drying of cavity– Last chance to clean surface and remove particulates from first assembly– Most critical cleaning step against field emission– At least two passes over entire surface
• Assembly of subcomponents (final evacuation flange)– Most critical assembly step no follow-up cleaning
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Heat treatment (600-800C)Details
Temperatureof hot zone
Low end 600C Typical 800C
Vacuum Start 1e-7 Torr End 1e-5 Torr
Cavity cleaning
Typically -degreasing
Sometimes-Chemistry and HPR
Support structure
Moly rails or rods
Automated controls
RGA, PLC
Process time 6-12 hrs or more
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Small Part Ultrasonic Cleaning Stations• Rinse tank out• Fill with DI water• Add Liquid Detergent
– Liquinox– Micro-90– Few percent by
volume• Ultrasonic agitation
– 15-60 minutes• Remove and rinse
parts with DI water• Blow dry
– ionized nitrogen gas– Laminar flow hepa air
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49 Managed by UT-Battellefor the U.S. Department of Energy Presentation_name
Ultrasonic cleaning
• Immersion of components in DI water and detergent medium
• Wave energy forms microscopic bubbles on component surfaces. Bubbles collapse (cavitation) on surface loosening particulate matter.
• Transducer provides high intensity ultrasonic fields that set up standing waves. Higher frequencies lowers the distance between nodes which produce less dead zones with no cavitation.
• Ultrasonic transducers are available in many different wave frequencies from 18 KHz to 120 KHz, the higher the frequency the lower the wave intensity.
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50 Managed by UT-Battellefor the U.S. Department of Energy Presentation_name
The Need For Material Removal
•
•
• • • • •
• 0
10
20
30
40
0 50 100 150 200 250
Rre
s [nΩ
]
Material Removal [µm]
• •
• • •
• •
•
010203040506070
0 50 100 150 200 250
Epe
ak [M
V/m
]
Material Removal [µm]
K. SaitoP. Kneisel
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51 Managed by UT-Battellefor the U.S. Department of Energy Presentation_name
Niobium Material Removal by Chemistry
Niobium surface after BCP Niobium surface after EP
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52 Managed by UT-Battellefor the U.S. Department of Energy Presentation_name
Hydrofluoric Acid Safety• Hydrofluoric acid is an anomaly
– It does not react like all other acids once absorbed into the skin
– It absorbs deeply into skin, destroys everything in the path, then slowly releases into blood stream bonding all calcium
– Calcium is needed to control the hart cardiac arrest can result in 8 hours after the exposure
– Time to proper first aid (removal of and bonding of fluorine) is the most important detail and will determine the outcome
– Large exposures always lead to death even with first aid and medical treatment
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53 Managed by UT-Battellefor the U.S. Department of Energy Presentation_name
HF Safety cont.
• Before using HF– Ensure the lab has a functioning safety shower– Calcium gluconate cream or equivalent– Proper PPE to cover all exposed skin– Additional personnel trained in providing first aid and available
• Before using a System– Review and understand the hazards– Know what to do when an accident happens
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54 Managed by UT-Battellefor the U.S. Department of Energy Presentation_name
Buffered Chemical Polish (BCP)Acid = HF (49%), HNO3 (65%), H3PO4 (85%)Mixture 1:1:1 , or 1:1:2 by volume typical
Reaction:
Oxidation 2Nb + 5HNO3 Nb205 + 5NO2
Reduction Nb2O5 + 6HF H2NbOF5 + NbO2F 0.5H2O + 1.5H2O
NbO2F 0.5H2O + 4HF H2NbOF5 + 1.5H2OReaction exothermic!
Brown gas
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55 Managed by UT-Battellefor the U.S. Department of Energy Presentation_name
Use of BCP:
• 1:1:1 still used for etching of subcomponents (etch rates of 8um/min)
• 1:1:2 used for most cavity treatments– Mixing necessary reaction products at surface– Acid is usually cooled to 10-15C (1-3um/min) to control
the reaction rate and Nb surface temperatures (reduce hydrogen absorption)
Dissolved Niobium in Acid (g/L)
Etch rate (um/min)
Acid Wasted After 15g/L Nb
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56 Managed by UT-Battellefor the U.S. Department of Energy Presentation_name
Effects of BCP on The Niobium Surface
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57 Managed by UT-Battellefor the U.S. Department of Energy Presentation_name
(BCP) Systems for Cavity Etching:
• Bulk & Final chemistry– Bulk removal of (100-200um)– Final removal of (5-20um) to
remove any additional damage from QA steps and produce a fresh surface
Implementation:
• Cavity held vertically
• Closed loop flow through style process, some gravity fed system designs
• Etch rate 2X on iris then equator
• Temperature gradient causes increased etching from one end to the other
• Manually connected to the cavity but process usually automated
BCP Cabinet JLab
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58 Managed by UT-Battellefor the U.S. Department of Energy Presentation_name
Electropolish (EP)
Electrolyte = 1 part HF(49%), 9 parts H2SO4 (96%)
Reaction:Oxidation
2Nb +5SO42- + 5H2O Nb2O5 +10H+ +5SO4
2- +10e-
ReductionNb2O5 + 6HF H2NbOF5 + NbO2F 0.5H2O + 1.5H2O
NbO2F 0.5H2O + 4HF H2NbOF5 + 1.5H2O
Hydrogen Gas
These are not the only reactions that take place!
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59 Managed by UT-Battellefor the U.S. Department of Energy Presentation_name
Nb Surface Effects After EP
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60 Managed by UT-Battellefor the U.S. Department of Energy Presentation_name
50 μm 50 μm
BCP EP
Surface Roughness of Niobium
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61 Managed by UT-Battellefor the U.S. Department of Energy Presentation_name
Basic Concepts of EP
+--
PotentialV1 V2 V3
Curr
ent
Den
sity
• 0-V1- Concentration Polarization occurs, active dilution of niobium, electrolyte resistance
• V2-V3 – Limiting Current Density, viscous layer on niobium surface
• >V3 Additional Cathodic Processes Occur, oxygen gas generated
Al
Nb
I-V Curve
DC Power Supply
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62 Managed by UT-Battellefor the U.S. Department of Energy Presentation_name
Cavity IV Curve not easy to interpret
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63 Managed by UT-Battellefor the U.S. Department of Energy Presentation_name3/27/06 OPS-
T lk
Hydrogen Gas Shielding Experiment
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64 Managed by UT-Battellefor the U.S. Department of Energy Presentation_name
Electropolishing of 9-cell Resonators (Nomura Plating & KEK)
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65 Managed by UT-Battellefor the U.S. Department of Energy Presentation_name
Electropolishing Systems JLAB
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66 Managed by UT-Battellefor the U.S. Department of Energy Presentation_name
Electropolishing Systems DESY
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67 Managed by UT-Battellefor the U.S. Department of Energy Presentation_name3/27/06 OPS-
T lk
High Pressure Rinsing:
• The need for HPR surface cleaning:– Entire surface contaminated after
chemistry, early field emission will result if not performed
– Effective at removing particulates on the surface after assembly steps
ISSUES:
• HPR systems are still not optimized for the best surface cleaning performance • Surface left in a vulnerable state, wet
• This is still the best cleaning method against field emission!
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68 Managed by UT-Battellefor the U.S. Department of Energy Presentation_name
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69 Managed by UT-Battellefor the U.S. Department of Energy Presentation_name3/27/06 OPS-
T lk
HPR spray heads needs to be optimized for a particular geometry!
Very effective on irises Equator fill with water too high flow rate
For a given pump displacement the nozzle opening diameter and number of nozzles sets the system pressure and flow rate
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70 Managed by UT-Battellefor the U.S. Department of Energy Presentation_name
Helium Processing
• Variation of RF processing• Keep pressure below discharge condition• Run cavity in the field emission regime• Push the gradient as high as the system allows• The process in details is unknown
– Electron spraying from FE bombard surface ionization of helium at around surface destroy field emitter???
– Controlled processing is difficult• Relying on field emitter locations and responses
– Uniformity??
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71 Managed by UT-Battellefor the U.S. Department of Energy Presentation_nameRongli Geng
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72 Managed by UT-Battellefor the U.S. Department of Energy Presentation_name
Preliminary experimental setup in RFTF
805 MHz500W CW amplifier
HB cavity
Gas feedingmanifold
Pump
First plasma in the SNSHB cavity
300W forward200W reflected1e-4 torr
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73 Managed by UT-Battellefor the U.S. Department of Energy Presentation_name
Plasma cleaning
• Ablation– Soft– Etching
• Activation• Crosslinking• Deposition
Base material
contaminants
Ion, molecule (radical), electron
before
afterwettability
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74 Managed by UT-Battellefor the U.S. Department of Energy Presentation_name
AP Talk Feb 19 2009
Radiation (before and after processing)Radiation reduced by factor of 5 to 100Showed promising results for in-situ processing
before after
Eacc=10 Eacc=10
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75 Managed by UT-Battellefor the U.S. Department of Energy Presentation_name
Integrated Process Automation
The Need!• Cryomodules are expensive ($M)
– Amount of hands-on labor– Failure rates (sensitivity of performance to errors)– Material costs (increasing with time, complexity of design)
• Machine energies are increasing– Cryomodule numbers are increasing (100,s 1000’s)
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76 Managed by UT-Battellefor the U.S. Department of Energy Presentation_name
Integrated Process Automation
• There is hope however for reduction of failure rates and labor– In my opinion “Vertical EP” may be the breakthrough we
needed
– Now one can imagine combining many of the processes into a single process station or two• Example
• Degreasing Assembly• Electropolish Evacuation• HPR Leak test• Drying Baking