Applications of Closed-Cycle Cryocoolers to Small Superconducting Devices April 1978 Proceedings of a Conference Held at the National Biireau 6
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Cryogenic Refrigeration Using an Acoustic Stirling Expander
CRYOGENIC REFRIGERATION USING AN ACOUSTIC STIRLING EXPANDER Masters Thesis by Nick Emery Department of Mechanical Engineering, University of Canterbury Christchurch, New Zealand Abstract A single-stage pulse tube cryocooler was designed and fabricated to provide cooling at 50 K for a high temperature superconducting (HTS) magnet, with a nominal electrical input frequency of 50 Hz and a maximum mean helium working gas pressure of 2.5 MPa. Sage software was used for the thermodynamic design of the pulse tube, with an initially predicted 30 W of cooling power at 50 K, and an input indicated power of 1800 W. Sage was found to be a useful tool for the design, and although not perfect, some correlation was established. The fabricated pulse tube was closely coupled to a metallic diaphragm pressure wave generator (PWG) with a 60 ml swept volume. The pulse tube achieved a lowest no-load temperature of 55 K and provided 46 W of cooling power at 77 K with a p-V input power of 675 W, which corresponded to 19.5% of Carnot COP. Recommendations included achieving the specified displacement from the PWG under the higher gas pressures, design and development of a more practical co-axial pulse tube and a multi-stage configuration to achieve the power at lower temperatures required by HTS. ii Acknowledgements The author acknowledges: His employer, Industrial Research Ltd (IRL), New Zealand, for the continued support of this work, Alan Caughley for all his encouragement, help and guidance, New Zealand’s Foundation for Research, Science and Technology for funding, University of Canterbury – in particular Alan Tucker and Michael Gschwendtner for their excellent supervision and helpful input, David Gedeon for his Sage software and great support, Mace Engineering for their manufacturing assistance, my wife Robyn for her support, and HTS-110 for creating an opportunity and pathway for the commercialisation of the device. -
Chapter 9, Problem 16. an Air-Standard Cycle Is Executed in A
COSMOS: Complete Online Solutions Manual Organization System Chapter 9, Problem 16. An air-standard cycle is executed in a closed system and is composed of the following four processes: 1-2 Isentropic compression from 100 kPa and 27°C to 1 MPa 2-3 P = constant heat addition in amount of 2800 kJ/kg 3-4 v = constant heat rejection to 100 kPa 4-1 P = constant heat rejection to initial state (a) Show the cycle on P-v and T-s diagrams. (b) Calculate the maximum temperature in the cycle. (c) Determine the thermal efficiency. Assume constant specific heats at room temperature. * Problems designated by a “C” are concept questions, and students are encouraged to answer them all. Problems designated by an “E” are in English units, and the SI users can ignore them. Problems with the are solved using EES, and complete solutions together with parametric studies are included on the enclosed DVD. Problems with the are comprehensive in nature and are intended to be solved with a computer, preferably using the EES software that accompanies this text. Thermodynamics: An Engineering Approach, 5/e, Yunus Çengel and Michael Boles, © 2006 The McGraw-Hill Companies. COSMOS: Complete Online Solutions Manual Organization System Chapter 9, Problem 37. The compression ratio of an air-standard Otto cycle is 9.5. Prior to the isentropic compression process, the air is at 100 kPa, 35°C, and 600 cm3. The temperature at the end of the isentropic expansion process is 800 K. Using specific heat values at room temperature, determine (a) the highest temperature and pressure in the cycle; (b) the amount of heat transferred in, in kJ; (c) the thermal efficiency; and (d) the mean effective pressure. -
Thermodynamic Analysis of a Waste Heat Driven Vuilleumier Cycle Heat Pump
Entropy 2015, 17, 1452-1465; doi:10.3390/e17031452 OPEN ACCESS entropy ISSN 1099-4300 www.mdpi.com/journal/entropy Article Thermodynamic Analysis of a Waste Heat Driven Vuilleumier Cycle Heat Pump Yingbai Xie * and Xuejie Sun Department of Power Engineering, North China Electric Power University, Baoding 07100, China; E-Mail: [email protected] * Author to whom correspondence should be addressed; E-Mail: [email protected]; Tel.: +86-312-752-2706; Fax: +86-312-752-2440. Academic Editor: Marc A. Rosen Received: 29 January 2015 / Accepted: 17 March 2015 / Published: 20 March 2015 Abstract: A Vuilleumier (VM) cycle heat pump is a closed gas cycle driven by heat energy. It has the highest performance among all known heat driven technologies. In this paper, two thermodynamic analyses, including energy and exergy analysis, are carried out to evaluate the application of a VM cycle heat pump for waste heat utilization. For a prototype VM cycle heat pump, equations for theoretical and actual cycles are established. Under the given conditions, the exergy efficiency for the theoretical cycle is 0.23 compared to 0.15 for the actual cycle. This is due to losses taking place in the actual cycle. Reheat losses and flow friction losses account for almost 83% of the total losses. Investigation of the effect of heat source temperature, cycle pressure and speed on the exergy efficiency indicate that the low temperature waste heat is a suitable heat source for a VM cycle heat pump. The selected cycle pressure should be higher than 100 MPa, and 200–300 rpm is the optimum speed. -
In-Cylinder Heat Transfer in an Ericsson Engine Prototype
International Conference on Renewable Energies and Power Quality (ICREPQ’13) Bilbao (Spain), 20th to 22th March, 2013 exÇxãtuÄx XÇxÜzç tÇw cÉãxÜ dâtÄ|àç ]ÉâÜÇtÄ (RE&PQJ) ISSN 2172-038 X, No.11, March 2013 In-Cylinder Heat Transfer in an Ericsson Engine Prototype A. FULA 1,2, P. STOUFFS 1 and F.SIERRA2 1 Laboratoire de Thermique, Energétique et Procédés Université de Pau et des Pays de l´Adour 64000, Pau, France. e-mail: [email protected] 2 Facultad de Ingenieria – Laboratorio Máquinas Térmicas y Energias Renovables Universidad Nacional de Colombia - Carrera 30 No 45 a 03 Edificio 401, Bogotá, Colombia. Phone 3165000 xt 11130, e-mail: [email protected] [email protected] Abstract. An Ericsson engine is an external heat supply Qh Qc engine working according to a Joule thermodynamic cycle. It is based on reciprocating piston-cylinder machines. Such engines are especially interesting for low power solar energy conversion and micro-CHP from conventional fossil fuels or from biomass. H RK An Ericsson engine prototype has been designed and realized. Due to the geometrical configuration of the compression space of this prototype, in-cylinder fluid wall heat transfer can be important. The influence of this heat transfer on the engine performance is modelled and the main results are presented. E C The experimental setup designed to study the in-cylinder heat Fig. 1. Principle of the Stirling engine. transfer is presented. Q Key words K c Solar energy conversion, biomass energy conversion, H R Ericsson engine, hot air engines, distributed generation, cylinder wall heat transfer. -
Performance Evaluation of the Thermolift Natural Gas Fired Air Conditioner and Cold-Climate Heat Pump
NOTICE: This document contains information of a preliminary nature and is not intended for release. It is subject to revision or correction and therefore does not represent a final report. ORNL/LTR-2019/1288 Performance Evaluation of the ThermoLift Natural Gas Fired Air Conditioner and Cold-Climate Heat Pump Peter Hofbauer Paul Schwartz Vishaldeep Sharma Approved for public release. Distribution is unlimited September 2019 DOCUMENT AVAILABILITY Reports produced after January 1, 1996, are generally available free via US Department of Energy (DOE) SciTech Connect. Website www.osti.gov Reports produced before January 1, 1996, may be purchased by members of the public from the following source: National Technical Information Service 5285 Port Royal Road Springfield, VA 22161 Telephone 703-605-6000 (1-800-553-6847) TDD 703-487-4639 Fax 703-605-6900 E-mail [email protected] Website http://classic.ntis.gov/ Reports are available to DOE employees, DOE contractors, Energy Technology Data Exchange representatives, and International Nuclear Information System representatives from the following source: Office of Scientific and Technical Information PO Box 62 Oak Ridge, TN 37831 Telephone 865-576-8401 Fax 865-576-5728 E-mail [email protected] Website http://www.osti.gov/contact.html This report was prepared as an account of work sponsored by an agency of the United States Government. Neither the United States Government nor any agency thereof, nor any of their employees, makes any warranty, express or implied, or assumes any legal liability or responsibility for the accuracy, completeness, or usefulness of any information, apparatus, product, or process disclosed, or represents that its use would not infringe privately owned rights. -
1998 Report of the RTOC
MONTREAL PROTOCOL ON SUBSTANCES THAT DEPLETE THE OZONE LAYER UNEP 1998 REPORT OF THE REFRIGERATION, AIR CONDITIONING AND HEAT PUMPS TECHNICAL OPTIONS COMMITTEE 1998 Assessment UNEP 1998 REPORT OF THE REFRIGERATION, AIR CONDITIONING AND HEAT PUMPS TECHNICAL OPTIONS COMMITTEE 1998 ASSESSMENT 1998 TOC Refrigeration, A/C and Heat Pumps Assessment Report 1 Montreal Protocol On Substances that Deplete the Ozone Layer UNEP 1998 REPORT OF THE REFRIGERATION, AIR CONDITIONING AND HEAT PUMPS TECHNICAL OPTIONS COMMITTEE 1998 ASSESSMENT The text of this report is composed in Times New Roman. Co-ordination: Refrigeration, Air Conditioning and Heat Pumps Technical Options Committee Composition: Lambert Kuijpers (Co-chair) Layout: Dawn Lindon Reproduction: UNEP Nairobi, Ozone Secretariat Date: October 1998 No copyright involved Printed in Kenya; 1998. ISBN 92-807-1731-6 2 1998 TOC Refrigeration, A/C and Heat Pumps Assessment Report UNEP 1998 REPORT OF THE REFRIGERATION, AIR CONDITIONING AND HEAT PUMPS TECHNICAL OPTIONS COMMITTEE 1998 ASSESSMENT 1998 TOC Refrigeration, A/C and Heat Pumps Assessment Report 3 DISCLAIMER The United Nations Environment Programme (UNEP), the Technology and Economic Assessment Panel (TEAP) co-chairs and members, the Technical and Economic Options Committee, chairs, co-chairs and members, the TEAP Task Forces co-chairs and members, and the companies and organisations that employ them do not endorse the performance, worker safety, or environmental acceptability of any of the technical options discussed. Every industrial operation requires consideration of worker safety and proper disposal of contaminants and waste products. Moreover, as work continues - including additional toxicity evaluation - more information on health, environmental and safety effects of alternatives and replacements will become available for use in selecting among the options discussed in this document. -
A Novel Thermomechanical Energy Conversion Cycle ⇑ Ian M
Applied Energy 126 (2014) 78–89 Contents lists available at ScienceDirect Applied Energy journal homepage: www.elsevier.com/locate/apenergy A novel thermomechanical energy conversion cycle ⇑ Ian M. McKinley, Felix Y. Lee, Laurent Pilon Mechanical and Aerospace Engineering Department, Henry Samueli School of Engineering and Applied Science, University of California, Los Angeles, Los Angeles, CA 90095, USA highlights Demonstration of a novel cycle converting thermal and mechanical energy directly into electrical energy. The new cycle is adaptable to changing thermal and mechanical conditions. The new cycle can generate electrical power at temperatures below those of other pyroelectric power cycles. The new cycle can generate larger electrical power than traditional mechanical cycles using piezoelectric materials. article info abstract Article history: This paper presents a new power cycle for direct conversion of thermomechanical energy into electrical Received 21 May 2013 energy performed on pyroelectric materials. It consists sequentially of (i) an isothermal electric poling Received in revised form 18 February 2014 process performed under zero stress followed by (ii) a combined uniaxial compressive stress and heating Accepted 26 March 2014 process, (iii) an isothermal electric de-poling process under uniaxial stress, and finally (iv) the removal of compressive stress during a cooling process. The new cycle was demonstrated experimentally on [001]-poled PMN-28PT single crystals. The maximum power and energy densities obtained were Keywords: 41 W/L and 41 J/L/cycle respectively for cold and hot source temperatures of 22 and 130 °C, electric field Pyroelectric materials between 0.2 and 0.95 MV/m, and with uniaxial load of 35.56 MPa at frequency of 1 Hz. -
Progress of Pulse Tube Cryocooler
Superconductivity and Cryogenics Vol.12, No.4, (2010), pp.1~7 Progress of Pulse Tube Cryocooler Yoichi Matsubara1,* and Deuk-Yong Koh2 1Former Professor of Nihon University, 763 Kotto Chikura minamiboso Chiba 295-0022, Japan 2KIMM, 171 Jang-dong Yuseong-ku Daejeon 305-343, Korea Received 7 September 2010; accepted 15 October 2010 ``` Abstract-- The pulse tube cooler as an alternative of of future development of the cooling system for each Stirling, G-M or VM cooler to overcome the requirement application fields. from the various application fields is described. The necessity of the object oriented cooler development is explained to realize the cryocooler of more energy-efficient, more reliable, 2. CLASSIFICATION OF PTC more compact and less expensive than what is currently available commercially. 2.1. Critical components of PTC Most characteristic merit of the pulse tube cooler is that it 1. INTRODUCTION has no mechanical moving components at the cold part of the cooling device without the sacrifice of thermodynamic Cryogenic technology, including cryocoolers, is a efficiency. From the view point of thermodynamic aspect, crucial supporting technology for superconductor pulse tube cooler will be divided into five critical applications, without exception. In general, if the existing components. room temperature technology is replaced with the Fig. 1 shows the basic arrangement of each component; superconducting technology, the extra work required for pressure wave generator, regenerator, pulse tube, heat the cooling system becomes a sort of penalty. Therefore the exchanger and the work receiver section. The simplest development of efficient cryocooler becomes essential configuration of the pressure wave generator will be issue. -
Review of Research, Development, and Deployment of Gas Heat Pumps in North America
Authors: Paul Glanville, R&D Manager, Gas Technology Institute; Patricia Rowley, Senior Engineer, Gas Technology Institute Session Title: Utilization: Innovations In Residential and Commercial Gas Technologies Title: Review of Research, Development, and Deployment of Gas Heat Pumps in North America Abstract In North America, natural gas is the predominant fuel for providing heat and hot water to residential and commercial buildings. In the U.S., the majority of homes and businesses use natural gas for heating and collectively consume 65 billion therms overall for space heating and hot water, equal to 23% of national natural gas consumption. In Canada, half of homes heat and 65% generate hot water with natural gas and a greater fraction of business, 80%, use natural gas for the same. Additionally, where available, consumer surveys indicate that natural gas is a preferred fuel for thermal comfort over alternatives. Despite its status as the predominant domestic and commercial fuel for heating and service hot water, direct use of natural gas for thermal comfort in North America is declining and may be undergoing a nascent transformation towards the expanded use of gas heat pumps (GHP). GHPs are at a cost premium over conventional, and even high-efficiency gas-fired heating equipment (e.g. furnaces, boilers.) While in many cases GHP products remain at the pre-commercial stage, they are receiving renewed attention due to potentially significant increases in delivered efficiency and the ability to provide seasonal comfort through some combination of heating, cooling, and hot water outputs. Market trends and pressures driving this interest include: (a) GHP technologies that may offer improved reliability, efficiency, financial payback, and end user comfort, (b) regulatory pressures concerning energy efficiency and both criteria and greenhouse gas (GHG) emissions, and (c) other environmental drivers concerning the primary energy budget of residential/commercial buildings, including pursuit of “Zero Net Energy” buildings. -
Lecture 3 Thermodynamic Principles of Energy Conversion
Thermodynamic principles of energy conversion Md. Mizanur Rahman School of Mechanical Engineering Universiti Teknologi Malaysia 1 Introduction • Mechanical and electrical power developed from the combustion of fossil fuels or the fission of nuclear fuel or renewable sources • This released energy is never lost but is transformed into other forms • This conservation of energy is explicitly expressed by the first law of thermodynamics • The work of an engine cannot be the same as the energy available in the fuel sources • Second law of thermodynamics is to meet to happen the process 2 Forms of energy • Energy can exist in numerous forms such as thermal, mechanical, kinetic, potential, electric, magnetic, chemical, and nuclear, and their sum constitutes the total energy, E of a system. • Mechanical Energy • Kinetic energy, KE: The energy that a system possesses as a result of its motion relative to some reference frame, KE=1/2mV2. • Potential energy, PE: The energy that a system possesses as a result of its elevation in a gravitational field, PE=mgh • For a moving body, E=PE+KE remains constant 3 Internal energy, U: The sum of all the microscopic forms of energy. • For gases, molecules are so widely separated in space that they may be considered to be moving independently of each other, each possessing a distinct total energy. • In the case of liquids or solids, each molecule is under the influence of forces exerted by nearby molecules • Changes in internal energy are measurable by changes in temperature, pressure, and density. 4 • Chemical energy: The internal energy associated with the atomic bonds in a molecule. -
Intro-Propulsion-Lect-18
18 1 Lect-18 In this lecture ... • Stirling and Ericsson cycles • Brayton cycle: The ideal cycle for gas- turbine engines • The Brayton cycle with regeneration • The Brayton cycle with intercooling, reheating and regeneration • Rankine cycle: The ideal cycle for vapour power cycles 2 Prof. Bhaskar Roy, Prof. A M Pradeep, Department of Aerospace, IIT Bombay Lect-18 Stirling and Ericsson cycles • The ideal Otto and Diesel cycles are internally reversible, but not totally reversible. • Hence their efficiencies will always be less than that of Carnot efficiency. • For a cycle to approach a Carnot cycle, heat addition and heat rejection must take place isothermally. • Stirling and Ericsson cycles comprise of isothermal heat addition and heat rejection. 3 Prof. Bhaskar Roy, Prof. A M Pradeep, Department of Aerospace, IIT Bombay Lect-18 Regeneration Working fluid • Both these cycles also have a regeneration process. • Regeneration, a process during which heat is Energy transferred to a thermal energy storage device Energy (called a regenerator) during one part of the cycle and is transferred back to the working fluid during Concept of a regenerator another part of the cycle. 4 Prof. Bhaskar Roy, Prof. A M Pradeep, Department of Aerospace, IIT Bombay Lect-18 Stirling cycle • Consists of four totally reversible processes: – 1-2 T = constant, expansion (heat addition from the external source) – 2-3 v = constant, regeneration (internal heat transfer from the working fluid to the regenerator) – 3-4 T= constant, compression (heat rejection to the external sink) – 4-1 v = constant, regeneration (internal heat transfer from the regenerator back to the working fluid) 5 Prof. -
Nasa Cr-145078 Study of a Vuilleumier Cycle
NASA CR-145078 STUDY OF A VUILLEUMIER CYCLE CRYOGENIC REFRIGERATOR FOR DETECTOR COOLING ON THE LIMB SCANNING INFRARED RADIOMETER by Samuel C. Russo JULY 1976 Prepared under Contract NAS 1-14337 by HUGHES AIRCRAFT CpMPANY x Culver City, California ^^ for National Aeronautics and Space Administration NASA CR-145078 STUDY OF A VUILLEU.MIER CYCLE CRYOGENIC REFRIGERATOR FOR DETECTOR COOLING ON THE LIMB SCANNING. INFRARED RADIOMETER July 1976 Samuel C. Russo Prepared under Contract NAS 1-14337 by ;.! . HUGHES AIRCRAFT COMPANY • ' Culver City, California !„,.'•..•, '• for NASA National Aeronautics and Space Administration IY CONTENTS I INTRODUCTION AND SUMMARY 1 II VM CYCLE THEORY OF OPERATION. 5 in DETERMINATION OF CRYOGENIC COOLING REQUIREMENTS ... 9 IV THERMODYNAMIC DESIGN AND PARAMETRIC PERFORMANCE ANALYSIS 16 Thermodynamic Design Analysis 16 Parametric Performance Analysis 20 Calculations of Transient Performance 29 V CONCEPTUAL MECHANICAL DESIGN 32 Dynamic Balance 32 Description of Refrigerator 35 Interfaces 43 Electronic Interface Unit . 47 VI IMPLEMENTATION PLAN . 53 General Tasks 54 Test Plans 55 Schedule 57 VII RELIABILITY AND LIFE STUDIES 58 VIII CONCLUSIONS 61 APPENDIX A DESIGN SPECIFICATION 63 APPENDIX B INHERENT THERMODYNAMIC AND HEAT TRANSFER LOSSES OF VM REFRIGERATOR 82 APPENDIX C DESCRIPTION OF INPUT COMMANDS 87 EFERENCES.......................................... "M 111 LIST OF ILLUSTRATIONS Figure Page 1 Schematic of basic two-stage VM cryogenic refrigerator 6 2 Indicator diagrams of first- and second-stage expansion volumes 7 3 Indicator diagrams of expansion hot volume and crankcase volume 8 4 Typical small VM cooler (71-7244) .~77TT. 10 5 Thermal loads from detector support 13 6 Effect of ground operation on wear rate of hot rider ring .....