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March 10, 2016 | International Cryogenic Engineering Conference-26, New Delhi, India Nitrogen gas propagation following a sudden vacuum loss in a tube.

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Presentation on theme: "March 10, 2016 | International Cryogenic Engineering Conference-26, New Delhi, India Nitrogen gas propagation following a sudden vacuum loss in a tube."— Presentation transcript:

1 March 10, 2016 | International Cryogenic Engineering Conference-26, New Delhi, India
Nitrogen gas propagation following a sudden vacuum loss in a tube cooled by liquid helium Ram C. Dhuley Steven W. Van Sciver National High Magnetic Field Laboratory, Tallahassee, FL 32310, USA Mechanical Engineering Department, FAMU-FSU College of Engineering, Tallahassee, FL 32310, USA Research supported by US Department of Energy grant DE-FG02-96ER40952

2 Loss of vacuum in a SRF beam-line
Cryomodule environment atmosphere more cryomodules LHe vacuum beam-line How does air propagate in a LHe cooled vacuum channel?

3 Conceptual picture of the propagation
vacuum Air LHe front channel wall (cold) Atmosphere (~ 295 K) channel wall, warm due to air condensation LHe Vacuum Air Channel wall Gas front in the vacuum space Heat wave in the tube wall

4 Experimental setup Mass flow generation and measurement
Ram C. Dhuley and Steven W. Van Sciver, IEEE Trans. Appl. Supercond. 25(3), , (2015) R. C. Dhuley and S. W. Van Sciver, Cryogenics (under review) Mass flow generation and measurement Propagation speed measurement

5 The gas front decelerates along
the vacuum tube! Direction of propagation T1 T11 T12 pstart = 50 kPa Deceleration observed during experiments with pstart = 50, 100, and 150 kPa in the gas tank

6 Empirical analysis of the front arrival data
R. C. Dhuley and S. W. Van Sciver, Int. J. Heat Mass Transfer 96, , (2016) Three experiments: pstart = 50 kPa, 100 kPa, 150 kPa Front speed decreases nearly exponentially along the tube b = speed decay length-scale

7 Analytical model of the gas front speed
R. C. Dhuley and S. W. Van Sciver, Int. J. Heat Mass Transfer 96, , (2016) constant if choked Conservation of mass in the gas phase: the propagation speed should decrease along the tube : constant : will grow with x

8 Reducing the empirical and analytical models
Empirical fit Analytical model constant with x

9 vs. location How do b’ and b compare? b’ = mdep decay length-scale
R. C. Dhuley and S. W. Van Sciver, Int. J. Heat Mass Transfer (under review) Local for the three experiments b’ = mdep decay length-scale How do b’ and b compare?

10 Comparison of the decay length-scales
The two independent analyses agree reasonably

11 Our contribution A simple analytical model to explain the front
deceleration Experimental evidence of the exponential decrease in the front speed

12 Thank you

13 Extra slide: Estimation of
R. C. Dhuley and S. W. Van Sciver, IOP Conf. Proc.: Mater. Sci. Eng. 101, , (2015) Locally, Temperature vs. time data at the twelve locations Local condensation heat transfer rate, qdep (energy balance at the tube wall)

14 Extra slide: Estimation of
: exists ‘exactly’ at the front, extremely difficult to measure/quantify Approximation: , mass deposition rate behind the front

15 Extra slide: Effect of He II coolant
Preliminary result (same N2 mass in-flow rate) The front travels slower when the tube is cooled by He II He II bath size (heat capacity) will influence the front speed

16 Extra slide: Effect of the decreasing mass in-flow
pstart (kPa) min start* (g/s) min end** % change 50 9.2 7.4 20 100 19.1 17.6 8 150 28.4 27 5 pstart (kPa) b (m) % (v0-v)/v0 50 0.46 96 100 0.63 91 150 0.95 80 Over the travel length,


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