Progress of Pulse Tube Cryocooler

Total Page:16

File Type:pdf, Size:1020Kb

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. The request from the application fields, however, is represented by a piston control volume with heat exchanger. not only the efficiency but also reliability, low cost, Similarly, the work receiver part will be represented by a compactness and applicability (easy to use). reservoir with an orifice as shown in the doted area The key technical aspects that must be taken into respectively. The regenerator, in typically, is made by a consideration are the different specifications required for stack of fine metallic mesh (normally ~300 mesh) within various applications. Generally, for power applications, the the thin tube to have good heat transfer with the gas, when most important application issues are reliability and the gas passing through in the void volume of the mesh. The redundancy problems; for electronics applications, pulse tube is a simple hollow tube with no heat transfer reliability, cost and, possibly, temperature stability are surface in it. Therefore the pulse tube is act as an adiabatic critical issues. Cryocoolers might be used in various tube. In this example of Fig. 1, the mechanical moving temperature regions in the future, depending on their component applications; at present, operation temperatures of 4.2 K, Work receiver 20 K and 77 K (based on the liquid temperature of Helium, Pressure wave generator Hydrogen and Nitrogen) are standard. Cryocoolers are categorized by the thermodynamic operating cycle, such as; Brayton, Joul-Thomson, Stirling and Gifford-McMahon (G-M) cycle. Former two are based on the circulating gas and the latter two are based on the Regenerator Pulse tube oscillating gas. Pulse tube cooler (PTC) as an alternative of Stirling cooler or G-M cooler, which also uses the oscillating gas, is noted as a cooling system to overcome the request from the wide application fields described Vacuum chamber above. Pulse tube coolers might be a promising solution for Heat exchanger some power and electronics applications. The cooling temperatures obtained from each cryogen described above Fig. 1. Fundamental arrangement of the pulse tube cooler are completely covered by pulse tube coolers. Fundamental divided into five critical components. White arrow thermodynamics of PTC is described to find the direction indicates the work flow direction to generate the cooling effect at the heat exchanger between the regenerator and the * Corresponding author: [email protected] pulse tube. 2 Progress of Pulse Tube Cryocooler component is only the piston located at the room thermo-acoustic or Vuillemier type because it is same as temperature. Input the external energy to the piston, then it the gas compression part of Vuillemier (VM) cycle. If the produces the work flow directed to the regenerator as displacer used in the VM cycle replaced to a gas column, shown by the white arrow on the figure. then it becomes thermo-acoustic engine. This work flows through the pulse tube and dissipated at One of the pressure wave generators is connected to the the orifice within the work receiver section. According to regenerator side and one of the work receivers is connected the pressure oscillation, the gas temperature at the heat to the pulse tube side to complete the pulse tube cooler. exchanger is lower when the gas flows from the pulse tube Three additional components shown by arrows below the to the regenerator than that of the reversed flow. This gives vacuum chamber are act as the phase shift mechanism. the cooling effect at the heat exchanger and the minimum The efficiency of the pulse tube cooler keeps improving cooling temperature is given when this cooling effect by changing the work receiver since the first pulse tube balanced with the heat load. cooler was reported by W. E. Gifford and R. C. Longsworth Traditional expression of the cooling effect is due to the in 1964 [1]. They choose the work receiver of simple heat gas expansion occurred near the expansion piston head. In exchanger. This type is now called as Basic pulse tube the case of the pulse tube, there is no solid expansion cooler. Second important improvement has been done by E. piston; however, the part of the gas column, which is I. Mikulin in 1984 [2]. Instead of the simple heat exchanger, oscillating within the pulse tube will act as a gas piston. an orifice and the reservoir is added to receive the work Therefore the heat exchanger temperature decreases and more actively. This type is called as Orifice pulse tube has some cooling capacity at the appropriate cooling cooler. temperature without any moving parts at the low A bypass valve between the regenerator warm end and temperature region inside of the vacuum chamber. This the pulse tube warm end, as shown in middle part of Fig. 2, unique structure leads the design flexibility of the cooling was added to the orifice pulse tube by S. Zhu in 1990 and is system and it expands the further application fields. called as Double inlet pulse tube [3]. Cooling performance Following section introduces the various pressure wave of this type improved further than Orifice type and is generators and the work receivers to understand the classified as 3rd generation corresponding to 2nd mechanism of keeping high efficiency of the pulse tube generation of Orifice type and 1st generation of Basic type. cooler. All other work receivers shown in Fig. 2 are proposed since 1988 to improve the performance of the pulse tube cooler 2.2. Historical background and are corresponding to 3rd generation [4-6]. The warm Three different types of pressure wave generator are displacer can be used instead of warm expander. If this given in Fig. 2. Type (a) is called as valve less compressor solid displacer is replaced to simple gas column then it or Stirling type because it is same as the gas compression becomes thermo-acoustic cooler. Two valves in the Active part used in Stirling cycle. Type (b) consists of circulating buffer type connected to each buffer must be well gas compressor with a heat exchanger (generally called as controlled with main valves of GM type pressure wave after cooler), and a set of switching valve to generate the generator. oscillating flow. This type is called as valved compressor or G-M type because it is same as the gas compression part used in Gifford-McMahon cycle. Type (c) is called as (a) thermo Vacuum chamber Heat exchanger (a) Stirling type After cooler (b) Switching Orifice & reservoir Valve, Ph Regenerator Pulse tube compressor Switching Valve, Pl Bypass valve Warm expander (b) G-M type Warm displacer regenerator (c) Active buffer Ph side displacer Pl side Pulse tube volume Inertance tube (c) Vuillemier type Four valve method Fig. 3. Equivalent PV diagrams within the pulse tube. Fig. 2. Schematic comparison of the pressure wave (a) Basic pulse tube, (b) Orifice pulse tube, (c) Double inlet generators (left side of dashed line) and the work receivers or any other 3rd generation pulse tube. Y-axis is the (right side of dashed line) for a common regenerator and pressure, X-axis is the pulse tube volume, left end is the low the pulse tube. Additional phase sifters are shown by temperature side and the right end is the room temperature arrows below the vacuum chamber. side. Yoichi Matsubara and Deuk-Yong Koh 3 generator. If these two buffers are eliminated and reservoir, so it makes compact but the problem of the connected to the main compressor high and low pressure circulating flow is still remains. Active buffer method and side respectively, then it becomes four-valve method. The the Inertance tube method have no such closed loop as a reason of the necessity of these developments will be source of instability, however, the former requires extra explained by PV diagram as shown in Fig. 3. buffer volume and the latter is not applicable to GM type or In the case of Basic pulse tube, warm end of the tube low frequency pulse tube cooler. Improvement by use of (right side) is closed by a heat exchanger. Therefore the Inertance tube is not significant for the small scale coolers.
Recommended publications
  • 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.
    [Show full text]
  • 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.
    [Show full text]
  • 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.
    [Show full text]
  • 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.
    [Show full text]
  • 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 .....
    [Show full text]
  • Experimental Investigation of Displacer Seal Geometry Effects In
    energies Article Experimental Investigation of Displacer Seal Geometry Effects in Stirling Cycle Machines Jan Sauer and Hans-Detlev Kühl * TU Dortmund University, Lehrstuhl für Thermodynamik (BCI), Emil-Figge-Straße 70, 44227 Dortmund, Germany; [email protected] * Correspondence: [email protected]; Tel.: +49-231-755-2674 Received: 22 August 2019; Accepted: 30 October 2019; Published: 5 November 2019 Abstract: This contribution deals with an experimental investigation of the optimization potential of Stirling engines and similar regenerative machines by an enhanced design of the cylinder liner and the seal. The latter is mounted at the bottom end of the gap surrounding pistons and displacers that separate cylinder volumes at different temperature levels. The thermal loss associated with this gap may amount to more than 10% of the heat input into these machines. Mostly, its design is reduced to an estimation of the optimum width by analytical models, which usually do not account for further relevant optimization parameters, such as a step in the cylinder wall. However, a recently developed, enhanced analytical model predicts that this loss may be significantly reduced by such a step. In this work, this design was realized and investigated experimentally according to this prediction by modification of the cylinder liner and the seal of an extensively tested laboratory-scale machine. The results confirm that such a design actually reduces the thermal loss substantially, presumably by reducing the cyclic mass flows through the open end of the gap. Additionally, it even improves the net power output due to a reduced volumetric displacement by the piston or displacer, resulting in smaller flow losses and thermal regenerator losses, whereas the pressure amplitude remains virtually unchanged, contrary to initial expectations.
    [Show full text]
  • Cryogenic Refrigeration Methods for Low and Ultra-Low Temperatures - a Review
    Sddhand, Vol. 9, Part 3, November 1986, pp. 191-232. ~ Printed in India. Cryogenic refrigeration methods for low and ultra-low temperatures - a review M THIRUMALESHWAR* and S V SUBRAMANYAM** * Cryogenics Section, Technical Physics and Prototype Engineering Division, BARC, Bombay 400 085, India ** Department of Physics, Indian Institute of Science, Bangalore 560 012, India MS received 2 September 1985; revised 4 April 1986 Abstract. In this review, various cryogenic refrigeration methods to obtain temperatures extending down to the milliKelvin/microKelvin range are described after first explaining the concepts of a "thermo- dynamically ideal cycle" and the "figure of merit". The various cycles are compared with each other. Data about some of the commercially available refrigerators/cryogenerators have also been included in this review. Keywords. Cryogenics; ultra-low temperatures; refrigeration methods. I. Introduction Cryogenics literally means "icy cold". However, generally this word connotes temperatures below 120 K (Barron 1966). A review of the history of the development of cryogenics is given by Mendelssohn (1966). Cryogenic technology implies the science and techniques of liquefaction, transportation and usage of cryogenic fluids such as liquid nitrogen (LN2), liquid hydrogen (LH2), liquid helium (LHe) etc. Developments of this technology from both the commercial and laboratory points of view are described in standard references (e.g., Mendelssohn 1966; Hoare et al 1961; Scott 1959; Croft 1976; Kurti 1971). Cryogenic refrigeration methods cover a wide spectrum from large industrial plants for production of cryogenic liquids to closed cycle helium refrigerators handling only a few watts at very low temperatures. Daniels and du Pre (1971) give specifically the require- ments of such small refrigerators for cooling some electronic devices.
    [Show full text]
  • Applications of Closed-Cycle Cryocoolers to Small Superconducting Devices April 1978 Proceedings of a Conference Held at the National Biireau 6
    A111D3 DLbSbfi '^*™illiinLi™.?I'!},!:'.9i!'SP.S&.^ R.I.C. «KW3t??..„ SPECIAL PUBLICATION 508 U.S. DEPARTMENT OF COMMERCE / National Bureau of Standards 1 osea- 0 Small l7Q tioMl Bureau of Staruiards MAY 1 i 1978 ^ Applications of Closed-Cycle Cryocoolers to ^0 Small Superconducting Devices Proceedings of a Conference Held at the National Bureau of Standards, Boulder, Colorado October 3-4, 1977 Edited by James E. Zimmerman and Thomas M. Flynn Cryogenics Division Institute for Basic Standards National Bureau of Standards Boulder, Colorado 80303 Sponsored by National Bureau of Standards and Office of Naval Research Arlington, Virginia 22217 U.S. DEPARTMENT OF COMMERCE, Juanita M. Kreps, Secretary Dr. Sidney Harman, Under Secretary Jordan J. Baruch, Assistant Secretary for Science and Technology NATIONAL BUREAU OF STANDARDS, Ernest Ambler, Director Issued April 1978 Library of Congress Catalog Card Number: 78-606017 National Bureau of Standards Special Publication 508 Nat. Bur. Stand. (U.S.) Spec. Publ. 508, 238 pages (Apr. 1978) CODEN. XNBSAV U.S. GOVERNMENT PRINTING OFFICE WASHINGTON: 1978 For sale by the Superintendent of Documents, U.S. Government Printing Office, Washington, D.C. 20434 Stock No 003-003-01910-1 Price $4.25 (Add 25 percent additional for other than U.S. mailing). ABSTRACT This document contains the proceedings of a meeting of specialists in small superconducting devices and in small cryogenic refrigerators. Industry, Government, and academia were represented at the meeting held at the National Bureau of Standards (NBS) on October 3 and 4, 1977« The purpose of the meeting was to define the refrigerator requirements for small superconducting devices and to determine if small cryogenic refrigerators that are produced in relatively large quantities can be adapted or developed to replace liquid helium as the cooling medium for the superconducting devices.
    [Show full text]
  • Table of Contents
    Table of Contents Preface A Review of Mathematical Models for Performance Analysis of Hybrid Solar Photovoltaic - Thermal (PV/T) Air Heating Systems P. Baskar and G. Edison 3 Design, Analysis and Experimental Evaluation of Photovoltaic Forced Convection Solar Dryer for the Tropics A.O. Adelaja and S.J. Ojolo 14 Studies on Solar Drying of Oily Sludge L.L. Mi, N.R. Liu and M. Meng 27 Effects of Exterior Sun Shades on Heat Transfer by Solar Radiation C.H. Huang and S.Y. Tsai 33 Operating Modes of the Solar Assisted Drainwater System for Ground Source Heat Pump Y.L. Yin, Q. Gao, B.F. Zhu and M. Li 38 Experimental Performance of a Mix Mode Solar Dryer for Drying Centella Asiatica N. Srisittipokakun and K. Kirdsiri 44 Performance Studies on Solar Photovoltaic Thermal System for Crop Drying M.B. Gorawar, P.P. Revankar, V. Tambarallimath and K. Shekar 48 Theoretical Investigation and Analysis of Solar Thermoelectric Air Conditioning Z.H. Qi, L.Y. Xu and B.H. Sun 56 The Application of Solar District Heating and Water Heating Integrated System in Residential Quarter Z.Z. Guan, C.J. Wang and Y.B. Xue 60 Solar Air-Conditioning System Using Single-Double Effect Combined Absorption Chiller H. Yabase and A. Hirai 65 Performance of a Solar Drying System Driven by a Hybrid Power System H. Zhong, Z.M. Li, T. Wu, M.J. Yu and R.S. Tang 71 Solar Driven Absorption Chiller for Medium Temperature Food Refrigeration, a Study for Application in Indonesia I.N. Suamir 79 Joint Application of Solar Water Heating System and Air-Conditioning System in a Dormitory Building H.Y.
    [Show full text]
  • Use Style: Paper Title
    International Journal on Recent Technologies in Mechanical and Electrical Engineering (IJRMEE) ISSN: 2349-7947 Volume: 2 Issue: 1 021– 023 _______________________________________________________________________________________________ Various parameters affecting the performance of a regenerator Ku. D P Bhadarka S P Dayal Mechanical Engineering Department Mechanical Engineering Department R C Technical Institute, Ahmedabad Government Polytechnic Vadnagar Gujarat, India Gujarat, India e-mail: [email protected] e-mail: [email protected] Abstract—main objective of this review paper is to show how various parameters affect the performance of regenerator. Performance of regenerator is very important parameter to design it.varius parameter which affects the performance of regenerator has been discussed. Keywords-regenerator,parameter __________________________________________________*****_________________________________________________ I. INTRODUCTION A regenerator is a very efficient compact heat exchanger which is used in cryogenic systems such as the Stirling cycle, Gifford-McMahon cycle, Solvay cycle, Vuilleumier cycle, and pulse tube refrigerator types. It is constructed of a matrix material that has the capability of quickly transferring and Fig 1 Cry cooler system Diagram storing heat from a gas, which passes through it. It is also highly resistant to heat flowing along its longitudinal direction. During the steady state operation of the regenerator, for As compared to the counter-flow heat exchanger, the one cycle, the warm gas from a compressor at temperature Th, regenerator does not require simultaneous continuous flow of passes through the regenerator, from point 1 to point 2, and two physically separated fluids. The regenerator transfers heat progressively transfers to the matrix material until the gas to and from the same gas by the intermediate heat transfer with temperature approaches the refrigeration temperature Tc.
    [Show full text]
  • Stirling Engine Design Manual
    https://ntrs.nasa.gov/search.jsp?R=19830022057 2020-03-21T03:20:43+00:00Z r .,_ DOE/NASA/3194---I NASA C,q-168088 Stirling Engine Design Manual Second Edition {NASA-CR-1580 88) ST_LiNG ,,'-NGINEDESI_ N83-30328 _ABU&L, 2ND _DIT.ION (_artini E[tgineeraag) 412 p HC Ai8/MF AO] CS_ laF Unclas G3/85 28223 Wi'liam R. Martini Martini Engineering January 1983 Prepared for NATIONAL AERONAUTICS AND SPACE ADMINISTRATION Lewis Research Center Under Grant NSG-3194 for U.S. DEPARTMENT OF ENERGY Conservation and Renewable Energy Office of Vehicle and Engine R&D DOE/NASA/3194-1 NASA CR-168088 Stirling Engine Design Manual Second Edition William R. Maltini Martir)i Engineering Ricllland Washif_gtotl Janualy 1983 P_epared Io_ National Aeronautics and Space Administlation Lewis Research Center Cleveland, Ollio 44135 Ulldel Giant NSG 319,1 IOI LIS DEF_ARIMENT OF: ENERGY Collsefvation aim Renewable E,lelgy Office of Vehicle arid Engir_e R&D Wasl_if_gton, D.C,. 20545 Ul_del IntefagencyAgleenlenl Dt: AI01 7/CS51040 TABLE OF CONTENTS I. Summary .............................. I 2. Introduction ......................... 3 2.22.1 WhatWhy Stirling?:Is a Stirl "in"g "En"i"g ne"? ". ". ". ............... 43 2.3 Major Types of Stirling Engines ................ 7 2,4 Overview of Report ...................... 10 3. Fully Described Stirling Engines .................. 12 3 • 1 The GPU-3 Engine m m • . • • • • • • • • . • • • . • • • • • • 12 3,2 The 4L23 Ergine ....................... 27 4. Partially Described Stirling Engines ................ 42 4.1 The Philips 1-98 Engine .................... 42 4.2 Miscellaneous Engines ..................... 46 4.3 Early Philips Air Engines ................... 46 4.4 The P75 Engine ........................ 58 4,5 The P40 Engine .......................
    [Show full text]
  • Knowledge-Based Query Formulation in Information Retrieval
    Knowledge-based Query Formulation in Information Retrieval Knowledge-based Query Formulation in Information Retrieval PROEFSCHRIFT ter verkrijging van de graad van doctor aan de Universiteit Maastricht, op gezag van de Rector Magnificus, Prof. dr. A.C. Nieuwenhuijzen Kruseman, volgens het besluit van het College van Decanen, in het openbaar te verdedigen op donderdag 14 september 2000 om 14:00 uur door Rudolf Wolfgang van der Pol Promotores: Prof. dr. H.J. van den Herik Prof. dr. ir. J.L.G. Dietz (Technische Universiteit Delft) Prof. dr. ir. A. Hasman Leden van de beoordelingscommissie: Prof. dr. H. Visser (voorzitter) Prof. dr. ir. K.L. Boon Prof. dr. K. Järvelin (Universiteit Tampere, Finland) Prof. dr. H. Koppelaar (Technische Universiteit Delft) Prof. dr. A.J. van Zanten Dissertation Series No. 2000-5 ISBN 90-801577-4-0 Uitgeverij Phidippides, Cadier en Keer © 2000 Ruud van der Pol Cover design and lay-out: Rob Molthoff Contents Chapter 1. Searching documents . 1 1.1 The central theme: document-search processes . 1 1.1.1 Concepts of query-based document-search processes. 2 1.1.2 Performance measures. 5 1.2 Motivation of the research . 5 1.2.1 Query-based document search processes have become crucial. 6 1.2.2 Query-based document-search processes are far from perfect . 7 1.2.3 A research opportunity: the project. 8 1.3 Outline of the thesis . 9 Chapter 2. Basic notions for document-search processes . 11 2.1 Basic assumptions. 11 2.1.1 The world . 11 2.1.2 Human beings . 12 2.2 Communication .
    [Show full text]