The Use of Small Coolers for Hydrogen and Helium Liquefaction

Slides:



Advertisements
Similar presentations
CM-22 Magnet Issues, 6 June MICE Magnet Cool Down and Other Issues Michael A. Green Lawrence Berkeley Laboratory Berkeley CA
Advertisements

Introduction to Closed Cycle Cooling Systems (for MICE) Tom Bradshaw Rutherford Appleton Laboratory MICE Video conference 24 th March 2004.
Basic Refrigeration Cycle
10 June 2006MICE Collaboration Meeting CM-151 Can MICE Solid and Liquid Absorbers be Characterized to better than 0.3 Percent? Michael A. Green 1, and.
1 MICE Hydrogen System Elwyn Baynham, Tom Bradshaw, Iouri Ivaniouchenkov RAL MICE / RAL Safety RAL, 30 October 2003.
1 Cooling the Hydrogen (Helium) Absorbers with Small Coolers Michael A. Green University of Oxford Department of Physics Oxford OX1 3RH, UK MICE Video.
Magnet Cooldown Scheme 17 th February 2012 Roy Preece (STFC RAL)
Spectrometer Solenoid Design and Procurement Review Steve Virostek Mike Green Mike Zisman Lawrence Berkeley National Lab MICE Collaboration Meeting October.
23 October 2005MICE Meeting at RAL1 MICE Tracker Magnets, 4 K Coolers, and Magnet Coupling during a Quench Michael A. Green Lawrence Berkeley Laboratory.
1 Issues concerning the Design of the Tracker Solenoids Michael A. Green Lawrence Berkeley National Laboratory 17 August 2005.
1 Update on Focus Coil Design and Configuration M. A. Green, G. Barr, W. Lau, R. S. Senanayake, and S. Q. Yang University of Oxford Department of Physics.
1 Spectrometer Solenoid Design and Cost Update Michael A. Green Lawrence Berkeley Laboratory 10 February 2005.
Michael A. Green Lawrence Berkeley National Laboratory
Report from meeting Hydrogen system operation from cryocooler and level control Cryocoolers for MICE Tom Bradshaw Elwyn Baynham Yury Ivanyushenkov Rutherford.
Spectrometer Solenoid Update Steve Virostek - LBNL MICE Video Conference #129 February 25, 2010.
9 June 2006MICE CM-15 Fermilab1 Progress on the MICE Cooling Channel and Tracker Magnets since CM-14 Michael A. Green Lawrence Berkeley Laboratory.
1 Superconducting Magnets for the MICE Channel Michael A. Green Oxford University Physics Department Oxford OX1-3RH, UK.
MICE Hydrogen System Implementation Tom Bradshaw Elwyn Baynham Iouri Ivaniouchenkov Jim Rochford.
Spectrometer Solenoid Fabrication & Testing Update Steve Virostek Lawrence Berkeley National Lab MICE CM24 at RAL June 1, 2009.
MICE collaboration meeting RAL 28 October 2004 Absorber R & D Plan by Wing Lau – Oxford University.
1 Infrastructure at RAL Iouri Ivaniouchenkov, RAL MICE Collaboration CERN, 29 March 2003.
MICE Spectrometer Solenoid Design and Fabrication Update Mike Green and Steve Virostek Lawrence Berkeley National Laboratory MICE Video Conference December.
1 Technical Arguments in Favor of using the Cryomech PT-415 Cooler for Cooling the LH 2 Experiment Michael A. Green Lawrence Berkeley Laboratory Berkeley.
Magnet and Absorber Heat Loads and Cooling with Various Small Coolers
12 March 2006NFMCC Meeting, IIT, Chicago1 Progress on the MICE Cooling Channel and Tracker Magnets Michael A. Green Lawrence Berkeley Laboratory.
1 Progress on the MICE Cooling Channel Magnets Michael A. Green Lawrence Berkeley National Laboratory 28 June 2005.
Hydrogen Delivery System – R&D Activities T W Bradshaw M Courthold M Hills J Rochford Daresbury Controls Group etc…
1 Absorber Heat Transfer and Other Issues A Comparison between MICE and the Forced Flow Absorber System Michael A. Green Lawrence Berkeley National Laboratory.
Spectrometer Solenoid and RFCC Update Michael S. Zisman Center for Beam Physics Accelerator & Fusion Research Division Lawrence Berkeley National Laboratory.
Mucool cryo-design Christine Darve Fermilab/Beams Division/ Cryogenic Department 8/12/02.
MICE Hydrogen System Design Tom Bradshaw Iouri Ivaniouchenkov Elwyn Baynham Columbia Meeting June 2003.
Spectrometer Solenoid Fabrication & Testing Update Steve Virostek Lawrence Berkeley National Lab MICE Collaboration Meeting #26 University of California.
MICE Collaboration Meeting CM-151 Is the the pulse tube cooler a must or is it simply better for the MICE AFC module? Michael A. Green Lawrence Berkeley.
MICE hydrogen review Summary of system hardware. System function To provide 22 litres of liquid hydrogen for use as a muon absorber within a superconducting.
CASIPP Design of Cryogenic Distribution System for CFETR CS model coil Division of Cryogenic Engineering and Technical Institute of Plasma Physics Chinese.
Progress on the MuCool and MICE Coupling Coils * L. Wang a, X. K Liu a, F. Y. Xu a, A. B. Chen a, H. Pan a, H. Wu a, X. L. Guo a, S. X Zheng a, D. Summers.
Spectrometer Solenoid Update Steve Virostek Lawrence Berkeley National Lab Roy Preece Rutherford Appleton Lab October 28, 2011 MICE Collaboration Meeting.
Status and Integration of the Spectrometer Solenoid Magnets Steve Virostek Lawrence Berkeley National Lab MICE RAL June 15, 2007.
Magnet quench during a training run Successfully trained to peak currents and operationally tested Thermal performance requirements met 3D magnetic bore.
Spectrometer Solenoid Test Plan Workshop: Spectrometer Solenoid Overview Steve Virostek - LBNL February 17, 2012.
Hydrogen system R&D. R&D programme – general points Hydrogen absorber system incorporates 2 novel aspects Hydrogen storage using a hydride bed Hydrogen.
Spectrometer Solenoids MICO 214 Steve Virostek LBNL February 6, 2013.
Hall D Target Design Status Jim Fochtman- February 22, 2012.
Spectrometer Solenoid: Plans to Fix Magnet 2 Steve Virostek Lawrence Berkeley National Lab Spectrometer Solenoid Review November 18, 2009.
Spectrometer Solenoid Fabrication & Testing Update Steve Virostek Lawrence Berkeley National Lab MICE CM25 at RAL November 6, 2009.
Spectrometer Solenoid Fabrication Status and Schedule Steve Virostek Lawrence Berkeley National Lab MICE RAL October 20, 2008.
Hall D Target System Review J. FochtmanSeptember 28,2011 Preliminary Design Work.
MICE Cooling Channel Magnets: Spectrometer Solenoid Procurement RF Module Coupling Coil Proposal Steve Virostek Lawrence Berkeley National Lab NFMCC 07.
Magnet vacuum vessel w/radiation shield and cold mass in place Magnet leads (left) and the three cryocoolers on the top of the spectrometer solenoid service.
Spectrometer Solenoid Update Steve Virostek Lawrence Berkeley National Lab MICE Collaboration Meeting #28 Sofia, Bulgaria.
CM-26 Cooler and Lead Test1 Tests of a PT415 Cooler with HTS Leads in the Drop-in Mode Michael A. Green Lawrence Berkeley Laboratory, Berkeley CA 94720,
„Cryogen-free“ Dilution Refrigerators
Chapter 11 Refrigeration Cycles Study Guide in PowerPoint to accompany Thermodynamics: An Engineering Approach, 8th edition by Yunus A. Çengel.
Removal of 3 He from 4 He (R&D) David Haase, Franklin Dubose, Travis McCaw and Paul Huffman North Carolina State University.
Spectrometer Solenoid Fabrication Update Steve Virostek Lawrence Berkeley National Lab NFMCC at LBNL January 25, 2009.
22 October 2005MICE Meeting at RAL1 Tracker Solenoid Overview Michael A. Green Lawrence Berkeley Laboratory MICE Collaboration Meeting 22 October 2005.
What is a Cryocar? It is a liquid nitrogen powered vehicle. Propulsion systems are cryogenic heat engines in which a cryogenic substance is used as a.
1 Small Coolers for MICE Michael A. Green University of Oxford Department of Physics Oxford OX1 3RH, UK MICE Collaboration Meeting RAL.
Spectrometer Solenoid Design and Test Results Steve Virostek Lawrence Berkeley National Lab Spectrometer Solenoid Review November 18, 2009.
Spectrometer Solenoid Background Info Steve Virostek Lawrence Berkeley National Lab MICE Spectrometer Solenoid Review: Phone Meeting October 5, 2009.
MICE Spectrometer Solenoid Recovery Review - December 3-4, Steve Virostek MICE Spectrometer Solenoid Design and Assembly.
Cooling Circuit Design Steve Virostek Lawrence Berkeley National Lab February 29, 2012 MICE Coupling Coil Cryostat Design Review Lawrence Berkeley National.
MICE Coupling Coil Fabrication Steps to Complete Allan DeMello Lawrence Berkeley National Laboratory Coupling Coil Working Group January 28, 2014 January.
S A Griffiths CM42 June 2015 Electrical & Control.
Michael A. Green and Heng Pan
Spectrometer Solenoid Fabrication Status and Schedule
Small Coolers for MICE MICE Collaboration Meeting RAL Michael A. Green
SNS PPU Cryomodule Instrumentation
Inter University Accelerator Centre, New Delhi
SNS PPU Cryomodule Instrumentation
Presentation transcript:

The Use of Small Coolers for Hydrogen and Helium Liquefaction Michael A. Green Lawrence Berkeley Laboratory CM-17 Talk Feb. 2007

Why is liquefaction with a cooler a problem? The heat of vaporization for hydrogen and helium is much lower than the heat that must be removed to cool the gas to the liquefaction temperature. For helium the heat of vaporization is 20.7 J g-1. The sensible heat from 300 K to 4 K is 1540 J g-1. A perfect helium liquefier has refrigeration to liquefaction coefficient of 20.7 J g-1. For hydrogen the heat of vaporization is 445 J g-1. The sensible heat from 300 K to 20 K is ~4000 J g-1. A perfect hydrogen liquefier has refrigeration to liquefaction coefficient of 445 J g-1. Hydrogen is easier to liquefy with a cooler than helium. CM-17 Talk Feb. 2007

2-Stage GM Cooler with an Added J-T Loop CM-17 Talk Feb. 2007

Liquefaction with a separate J-T loop. Refrigeration at 4 K is relatively easy even when the cooler can only produce 8 K at the 2nd-stage. Liquefaction of helium is nearly impossible. Re-condensation is not the same as liquefaction. The refrigeration to liquefaction coefficients for helium are greater 500 J g-1. The advent of 4 K coolers improved liquefaction with a separate J-T circuit, but to refrigeration to liquefaction coefficients are still high (~350 J g-1). Liquefaction of hydrogen is easier. CM-17 Talk Feb. 2007

2-Stage 4 K GM Cooler used as Liquefier CM-17 Talk Feb. 2007

Liquefaction with a 4 K GM Cooler Liquefaction with a 4 K cooler is possible if there is a larger heat exchanger on the 2nd-stage. Adding a heat exchanger to to the 1st-stage greatly improves liquefaction of helium. The refrigeration to liquefaction coefficient is ~ 160 J g-1. Adding liquid nitrogen cooling improve liquefaction even more. In theory, a refrigeration to liquefaction coefficient of 600 J g-1 can be achieved for hydrogen. CM-17 Talk Feb. 2007

Additional Cooling can come off of the Regenerator and Pulse tubes of a Cryomech Pulse Tube Cooler CM-17 Talk Feb. 2007

One can get additional cooling from the tubes of Cryomech pulse tube coolers The experiment at Cryomech using a PT-405 cooler showed that additional cooling is available between stages from the regenerator tube and the pulse tube. Cooling between stages is not available for a typical GM cooler. Not all pulse tube coolers have cooling available between stages. The cooling between stages can greatly improve the liquefaction efficiency (a lower refrigeration to liquefaction coefficient). CM-17 Talk Feb. 2007

Circuit Diagram for the PT-410 Liquefier with Tube Heat Exchanger CM-17 Talk Feb. 2007

PT-410 Liquefier with Tube Heat Exchanger Condensing Pot Cooler 2nd-Stage Tube Heat Exchanger Cooler 1st-Stage 1st Stage Heat Exchanger Rotary Valve Rotary Valve Motor Ballast Tank CM-17 Talk Feb. 2007

Liquefaction with the PT-410 Cooler The heat exchanger on the 1st-stage and the heat exchanger on the regenerator tube between the 1st and 2nd stages of a PT-410 cooler reduces the refrigeration to liquefaction coefficient of 45 J g-1 for helium. This is better than any other helium liquefier. Cooling from the tubes between stage permits one to operate the PT-415 cooler in the drop in mode because there is free-convection between the mounting tube and the cooler. CM-17 Talk Feb. 2007

Drop In PT-415 Cooler with Condenser for the MICE Tracker Solenoids CM-17 Talk Feb. 2007

The drop in cooler concept will be used for the PT-415 cooler for the MICE tracker solenoid. It is hoped that free-convection cooling between the cooler tubes and the mounting tube will reduce the heat leak down the mounting tube. The mounting tube wall thickness will be machined down from 0.87 mm to 0.37 mm. The 1st-stage tapered joint allows heat from the leads, the thermal radiation shield, and the cold mass supports to the cooler 1st stage. CM-17 Talk Feb. 2007

Cryomech found that the liquefaction improved without the tube heat exchanger. Eliminating the heat exchanger from the cooler liquefier reduces the cost of the liquefier. Eliminating the heat exchanger from the cooler liquefier increases the efficiency of liquefaction about 30 percent. The new Cryomech liquefier has a refrigeration to liquefaction coefficient of 36 J g-1. Cryomech would like to build the hydrogen (helium) liquefier for the MICE absorbers. CM-17 Talk Feb. 2007

A More Efficient Liquefier without the Tube Heat Exchanger The areas shown are based on the PT-415 cooler. CM-17 Talk Feb. 2007

The Proposed Cryomech Absorber Hydrogen Liquefaction System Using the PT-415 Cooler CM-17 Talk Feb. 2007

A Proposed Absorber Cooler Module Cryomech has a commercial interest in building a hydrogen liquefier. Cryomech proposes to use the pulse tubes and regenerator tubes and holes in the first stage to pre-cool the hydrogen being liquefied. Standard tube parts would be used for the liquefier. Hydrogen from the hydride bed (or bottles) must be fed into the upper part of the cooler space between the top plate and the first stage heat exchanger The absorber probably can be filled in 24 hours. CM-17 Talk Feb. 2007

An End View of a Proposed MICE Absorber Cooler Module with Hydrogen Liquefier CM-17 Talk Feb. 2007

A Proposed Cooler Experiment Using the PT-415 Cooler CM-17 Talk Feb. 2007

Purpose of the Cooler Experiment Measure the performance of the PT-415 cooler in the magnet configuration over a range of 2nd-stage temperatures from 2.5 K to about 22 K and 1st-stage temperatures from 30 K to 65 K. Confirm the that the PT-415 cooler will will work well in the drop in configuration. Measure the extra heat leak (if any) that comes from this method of mounting the cooler in this way. Demonstrate that the PT-415 cooler will liquefy both helium and hydrogen. CM-17 Talk Feb. 2007

Known Operating Points of the PT-415 Cooler 6 5 4 3 2 SECOND STAGE TEMPERATURE K The measured test data is from Tom Painter of Florida State University. CM-17 Talk Feb. 2007

Plans for the Cooler Experiment This experiment will measure the temperature of both stages of a PT-415 pulse tube cooler as a function of the heat load on both stages. On the first stage power with Q = 0, 20, 40, 60 and 80 W will be applied. At that same time, the second stage power will be changed in steps of Q = 0, 0.5, 1.0, 1.5, 2.0, 5, 10, 15, 20, 25, and 30 W. The measurements will be done both in vacuum and in a helium gas atmosphere. The experiment will compare the thermal resistance of the first stage taper boundary in vacuum and in helium gas CM-17 Talk Feb. 2007

Cooler Experiment Purpose Continued The degree to which convection currents play a role in intercepting heat will be measured by recording the temperature on the tube between stages both in vacuum and in helium. With liquid helium in the tank, the DT between the tank and the second stage cold head will be measured. Operate the cryogenic system with the cooler with helium at 3.8 K, 4.2 K and 4.6 K. Measure the liquefaction of helium at 4.3 K. Measure the liquefaction of hydrogen at 20.8 K. CM-17 Talk Feb. 2007

Diagram of a Proposed Cooler Experiment CM-17 Talk Feb. 2007

What is needed for the experiment? One MICE PT-415 cooler for a magnet The actual magnet cooler mounting tube A liquefaction vessel (~1.5 liters) for He and H2 A 1st stage thermal shield with MLI inside and outside the shield to minimize heat leak The experiment vacuum vessel Seven (or eight) diode temperature sensors T Two 1st Stage heaters Q (0 to 80 watts) Two 2nd Stage heaters Q (0 to 30 watts) Commercial LHe and LH2 liquid level gauges CM-17 Talk Feb. 2007

Concluding Comments Hydrogen liquefaction is possible with both GM and pulse tube coolers. Liquefaction must be done correctly. Cryomech has proposed that the could fabricate the absorber hydrogen liquefaction module. This may be cost effective. A test of the PT-415 cooler is needed, even for the tracker magnet. If LBL doesn’t do the test, who will do the test? CM-17 Talk Feb. 2007