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Title: Thermal Shock Measurements for Solid


1
Thermal Shock Measurements for Solid High-Power
Targets at High Temperatures
J. R. J. Bennett1, G. Skoro2, J. Back3, S.
Brooks1, R. Brownsword1, C. J. Densham1, R.
Edgecock1, S. Gray1 and A. J. McFarland1 1
Rutherford Appleton Laboratory, Chilton, Didcot,
Oxon. OX11 0QX, UK 2 Department of Physics and
Astronomy, University of Sheffield, Sheffield. S3
7RH, UK 3 Department of Physics, University of
Warwick, Coventry. CV4 7AL, UK roger.bennett_at_rl.a
c.uk Joint high power target meeting,
EURISOL/BENE, CERN, 22 February 2007
2
  • OUTLINE
  • Introduction
  • Thermal Shock, Fatigue and Creep
  • Wire tests
  • Future work

3
The original RAL Target concept - (after Bruce
King)
4
Schematic diagram of the radiation cooled
rotating toroidal target
5
The alternative concept Individual Bar Targets
6
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7
solenoids
Target Bars
Proton beam
The target bars are connected by links - like a
bicycle chain.
Schematic diagram of the target and collector
solenoid arrangement
8
The Perceived Primary Problem
9
The value of the peak stress is
With typical values for tungsten E 300 GPa a
0.9x10-5 K-1 T 100 K 0.2 Yield Strength
20 MPa at 2000 K UTS 100 MPa smax 270 MPa
Stress exceeds UTS FAILURE EXPECTED!!
10
Real Life is not this simple. - The Pbar target
at FNAL withstands 40,000 J cm-3! - The NF target
has only 300 J cm-3
11
Individual pulses are not the problem. Failure
found after Many Pulses the problem
is- Fatigue Creep
12
Fatigue and Creep Very difficult to predict the
number of cycles to failure. S-N or Wöhler Plot
stress versus number of cycles to failure.
The Fatigue Limit Stress can be expressed by s0
1.6 Hv 0.1Hv Hv - Vickers Hardness in kgf
mm-2 For tungsten at 1800 K Hv 50 so the
fatigue limit stress is s0 80 MPa
Stress, S
s0
N 106
Number of cycles, N (log scale)
13
The primary purpose of these tests is to address
the problem of thermal shock at high temperatures.
To find a refractory material that will withstand
the thermal stresses/fatigue and have a long life
of 1-10 years. 1 year corresponds to 106
pulses on an individual target bar.
14
  • It is not possible to test the full size targets
    in a proton beam and do a life test.
  • The solution
  • Produce shocks by passing high current pulses
    through thin wires.

15
Lorenz Force
Thermal Force
Lorenz Thermal Force
100 ns pulse
Typical radial stress in the wire from thermal
and Lorentz forces
Goran Skoro
16
Goran Skoro
17
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18
Test wire, 0.5 mm F
Pulsed Power Supply. 0-60 kV 0-10000 A 100 ns
rise and fall time 800 ns flat top Repetition
rate 50 Hz or sub-multiples of 2
Coaxial wires
Vacuum chamber, 2x10-7 -1x10-6 mbar
Schematic circuit diagram of the wire test
equipment
19
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20
Vertical Section through the Wire Test Apparatus
21
W26 Tungsten Wire Assembly
22
Picture of the pulse current, 200 ns/division
23
Picture of the pulse current, 1 ?s/division
24
Picture of the wire test equipment
25
Measurement of the Pulse Temperature 1 kHz
measurement rate
26
Tests on Tantalum Wire The wire lasted for a few
hundred thousand pulses before breaking or
bending. Tantalum is not a suitable material
since it too weak at high temperatures (1600-2000
K).
27
Photograph of the tantalum wire showing
characteristic wiggles before failure.
28
A broken tantalum wire
29
Ultimate
Ultimate
Yield
Yield
Ultimate
Yield
Yield and Ultimate Strength of Tantalum and
alloys versus Temperature.
30
Fatigue characteristics of 1 mm thick tantalum
sheet
31
Yield Strength of Tungsten and some Alloys versus
Temperature
32
Ultimate Tensile Strength, MPa
Ultimate Tensile Strength of Tungsten and some
Alloys versus Temperature
33
Tests on Tungsten Wire Tungsten is much stronger
than Tantalum particularly at high
temperatures. So - try Tungsten
34
Some Results 0.5 mm diameter Tungsten Wires
Equivalent Target This shows the equivalent
beam power (MW) and target radius (cm) in a real
target for the same stress in the test wire.
Assumes a parabolic beam distribution and 3
micro-pulses per macro-pulse of 20 micro-s.
35
W26 Broken Tungsten Wire after 13 million pulses.
36
W3 Tungsten Wire, after operating at 4900 A, peak
temperature 1800 K, for 3.3x106 pulses and then a
few pulses at 7200 A at gt2000 K.
37
W5 Tungsten Wire showing wiggles 6200 A, gt2000
K peak temperature, 5625 pulses.
38
  • Radiation Damage
  • Experience on the ISIS targets show that there is
    no serious problem up to 12 dpa.
  • Tungsten pellets irradiated (15-20 dpa) at PSI
    will be examined when cool enough.

39
Conclusions I believe that the viability of solid
tungsten targets at high-temperature for a long
life (10 years) has been demonstrated with
respect to thermal shock and fatigue and will not
suffer undue radiation damage.
40
  • Future Programme
  • Continue wire tests with Tungsten and Graphite.
  • Continue modelling computations.
  • VISAR measurements to asses the properties of
    tungsten, and any changes, during the wire tests.
    (Effect of thermal shock.)
  • Tests with a proton beam to confirm wire tests
    and VISAR measurements but limited number of
    pulses.
  • Radiation damage studies.
  • Test alloys of tungsten.
  • Design build a model of the target bar system.
  • Design the solenoid.
  • Design and cost the complete target station
    including the beam dump.
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