Outgassing%20of%20Stainless%20Steel%20Vacuum%20Chambers%20and%20The%20Vacuum%20Pumping%20Speed%20and%20Capacity%20Evaluation%20of%20a%20Titanium%20Sublimation%20Pump - PowerPoint PPT Presentation

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Outgassing%20of%20Stainless%20Steel%20Vacuum%20Chambers%20and%20The%20Vacuum%20Pumping%20Speed%20and%20Capacity%20Evaluation%20of%20a%20Titanium%20Sublimation%20Pump

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Outgassing of Stainless Steel Vacuum Chambers and The Vacuum Pumping Speed and Capacity Evaluation of a Titanium Sublimation Pump Christian Hammill, Wayne State ... – PowerPoint PPT presentation

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Title: Outgassing%20of%20Stainless%20Steel%20Vacuum%20Chambers%20and%20The%20Vacuum%20Pumping%20Speed%20and%20Capacity%20Evaluation%20of%20a%20Titanium%20Sublimation%20Pump


1
Outgassing of Stainless Steel Vacuum Chambers
andThe Vacuum Pumping Speed and Capacity
Evaluation of a Titanium Sublimation Pump
  • Christian Hammill, Wayne State University
  • Dr. Yulin Li Dr. Xianghong Liu, Cornell
    University

2
My Project at a glance
3
Contents
  • Outgassing of stainless steel chambers
  • Introduction and purpose
  • What is the goal of this project?
  • Methodology
  • What methods are used to determine ?
  • What do these methods involve?
  • What is the difference in these methods?
  • Results
  • Conclusions
  • Vacuum characteristics of the TiSP
  • Introduction and purpose
  • What is a TiSP?
  • What do we want to determine from the TiSP?
  • Methodology
  • How do we determine Q(t) and STi(t)?
  • Results
  • Conclusions

4
SST Outgassing Introduction
  • XHV must be achieved in parts of ERL (i.e.
    photo-chamber)
  • Stainless Steel outgassing hinders this
  • When put under vacuum
  • 400C bakeout reduces outgassing
  • Does this last forever?!
  • My mission do stainless steel chambers that have
    been stored properly in N2 for 8 months keep low
    outgassing property?

5
SST Outgassing Methodology I
  • Vacuum system comprised of two parts
  • Testing Chamber
  • Enclosed by oven
  • Heating gun/ air blower
  • Water cooling coils/ heating tape
  • SRG/ sample chamber
  • Sensor Chamber
  • Valve to Testing Chamber
  • RGA
  • CCG
  • Ion Pump Turbo Pump

6
SST Outgassing Methodology II
  • Two methods of determining
  • Rate of Rise method
  • Where V is the volume of the chamber (28L) and As
    is inner surface area of the sample chamber (7500
    cm2)
  • Throughput method
  • Where is Sip the pumping speed of the ion pump
    and As is inner surface area of the sample
    chamber
  • ?P (pressure increase due to outgassing) is
    explained later

7
SST Outgassing Methodology III
  • Both methods follow a similar procedure
  • Set up and leak check
  • All vacuum flanges are connected and properly
    tightened
  • Then, entire vacuum system is pumped down and
    checked for gas leaks
  • Bakeout
  • The adsorbed water molecules (from air exposure)
    are eliminated via temperatures gt120C
  • Measurement
  • is determined using either ROR method or
    throughput
  • Repeat
  • Baking temperature is increased each time (150C
    to 200C to 250C)

8
The Rate of Rise Method
  • In RoR measurements, the sample chamber is closed
    off from any pumping
  • This allows gas to accumulate in the closed
    system
  • With a constant outgassing rate, , a linear
    pressure rise is expected
  • The rate of rise in the pressure, , is
    measured to calculate such that

9
The Spinning Rotor Gauge
  • SRG consists of a magnetized rotor ball in a
    gimble tube, and a removable head that contains
    sets of coils
  • The Rotor is magnetically levitated and spinning
  • Molecules in the chamber collide with the rotor,
    ever slightly slowing down the rotor, the
    molecular drag
  • The SRG measures the pressure by measuring the
    slowing down rate ofthe rotor due to the
    molecular drag

10
Throughput method
  • Used as crosscheck for RoR method
  • The pressure at the CCG is recorded while the
    sample chamber is still closed off from the
    sensor chamber gt baseline pressure
  • The chamber is then opened and the pressure is
    left to settle then recorded
  • The difference between the settled pressure and
    the baseline pressure is known as the change in
    pressure, ?P
  • Then, using the pumping speed of the ion pump,
    Sip (9L/s), we calculate

11
A Typical RoR Result
Pressure measured by SRG clearly show a linear
rise in time. The fitted slope dP/dt
2x10-12 Torr/s.
Very stable temperature control ?T 0.17 C
12
A Typical Throughput Result
Sip is determined via a pump down of sample
chamber
Fitting (blue) curve, P(t)
Gas composition at point A
In this case, ?P1.5x10-11 Torr, Sip 9 L/s
therefore, 1.9x10-14 TorrLs-1cm-2
13
Outgassing Results Summary
Current project data
Tbake(C) (10-15 TorrLs-1cm-2) (10-15 TorrLs-1cm-2)
Tbake(C) Rate of rise Throughput
120 2.6 30
120 6.0 19
120 7.5 n/a
150 25 n/a
150 18 n/a
150 15 n/a
200 6.7 15
200 6.7 28
250 9.3 35
250 7.5 38
Data from 8 months ago
TBake (C) (10-15 TorrLs1cm-2)
150 19.0
200 16.0
250 14.0
14
SST Outgassing Conclusions
  • The outgassing rates measured in this study are
    comparable with the results from 8 months ago.
  • This indicates that the extremely low outgassing
    property can be maintained.
  • The comparison between the rate of rise method
    and the throughput results is very good, when one
    considers at least two factors
  • The measurements were done at very different
    pressure ranges (10-6 torr for rate of rise, and
    10-10 torr for the throughput).
  • They both use very different gauges (SRG vs.
    CCG).
  • Therefore, in certain places in the ERL (i.e. the
    photo-cathode) one can vent out the vacuum,
    properly store the stainless steel components in
    N2, and not damage the outgassing properties of
    these components

15
TiSP Performance Introduction
  • After measuring the properties of the electron
    beam, it must be safely terminated at the beam
    dump in the Cornell Proto-type Photo-cathode
    Injector
  • Very large gas loads of H2 gas are generated at
    the beam dump when this happens
  • A large TiSP will be used together with two large
    ion pumps to control the H2 gas load
  • Will this do the trick?
  • My mission evaluate the pumping performance
    (particularly the pumping speed and the pumping
    capacity) of the TiSP to determine if it is
    suitable for this application

16
TiSP Performance methodology I
  • Experimental Setup
  • The test system was leak checked and baked at
    170C
  • Ultra-high purity hydrogen is used to measure the
    TiSP pumping performance
  • The flow-rate of H2 was experimentally determined
    before any Ti-sublimation,
  • After Ti-sublimation, H2 flows through the TiSP
    chamber, and the pressures are monitored by two
    cold cathode gauges

17
TiSP performance methodology II
  • Ti Sublimation
  • There are 3 Ti cartidges on the end of the
    chamber
  • Each filament is heated via voltage power source
  • This heating causes the Ti to sublimate in the
    chamber
  • This process is known as flashing
  • The Ti is flashed in the chamber for a certain
    period of time at a certain power

Ti cartrige with 3 filaments
18
Determining STi(t)
  • After flashing, we open the H2 valve again and
    let the gas flow
  • Because the Ti layer inside the chamber is so
    reactive, it will capture much of the gas as it
    enters the chamber
  • This causes the pressure to decrease at the CCG
  • At the CCG there are now 2 pumping speeds
  • The effective speed of the turbo, , and
    the pumping speed of the chamber, STi(t).
  • Knowing this, we derive the formula for the
    pumping speed of the chamber over time
  • ? this
    follows the Equation, SP

19
Determination of Q(t)
  • We want to determine the total amount of H2 gas
    pumped away by the TiSP chamber, Q(t).
  • As the Ti film pumps more and more H2 is pumped
    away it becomes saturated with H2
  • As it becomes more saturated, its pumping speed
    decreases
  • The accumulated Q(t) is directly related to
    STi(t) such that

20
TiSP Performance Results I
  • STi(t) was measured at 2 flashing settings
  • (A) 3 minutes at 170W
  • (B) 5 minutes at 195W
  • Higher Ti-flashing power longer duration gt
    much thicker Ti layer
  • The STi(t)s are plotted against the Q(t)s
  • Limited Ti flashing and H2 saturation cycles were
    done
  • Thick, H2 rich, Ti films are known to be flaky

21
TiSP Performance Results II
  • Q(t) is arbitrary and depends on its application.
  • Here, we chose Q(t) to be the point where STi(t)
    drops to 100L/s
  • (i.e. 10 of its initial pumping speed).
  • With this definition, one sees from that
  • QA 4 TorrL
  • QB 25 TorrL
  • With maximum pumping speeds of
  • STi, A(t) 900L/s STi, B(t) 1200L/s
  • As a side note, it took 80 hours for B to
    saturate from the beginning to 100L/s

Hydrogen Pumping by Ti
Step 1 Dissociative adsorption
H2 ? 2Hads
Step 2 Bulk diffusion
Hads ? HBulk
Step 1 depends on surface reactivity of Ti
film Step 2 depends on Ti film thickness and
solubility
22
TiSP Performance Conclusions
  • It can be seen that the max STi 1200 L/s
    that it is capable of pumping out 25 TorrL of
    H2 gas.
  • The estimated gas load at the beam dump (A5
    section of the Cornell Proto-type Photo-cathode
    Injector) can be as high as 1.8x10-3 TorrL/s.
  • Considering that two other ion pumps will be
    sharing half of the load, the TiSP will have to
    handle a gas load of 9.0x10-4 TorrL/s.
  • With a little math, we can see that the TiSP can
    go 8 hours before needing to go through a
    flashing cycle again.
  • This is considered to be sufficient for the
    injector operations
  • Therefore the TiSP is suitable for the ERL
    prototype project

23
Acknowledgements
  • Thanks are due to
  • My mentors Dr. Yulin Li and Dr. Xianghong Liu
    who have assisted me in the writing of this
    paper, the assembling of the experiments, and the
    overall guidance though this project.
  • The lab technical staff Tim Giles, Tobey Moore,
    and Brent Johnson.
  • Dr. Rich Galik and Dr. Claude Pruneau who are the
    assemblers of this REU project and made it able
    for me to attend the summer here.
  • The National Science Foundation who every year
    make it possible for students much like myself to
    have experiences like this one.
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