Modeling and Miniaturization of the Thermoacoustically Driven IPTR to Encourage Sustainable Energy
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Thermoacoustic Analysis of Displacer Gap Loss in a Low Temperature Stirling Cooler
THERMOACOUSTIC ANALYSIS OF DISPLACER GAP LOSS IN A LOW TEMPERATURE STIRLING COOLER Vincent Kotsubo1 and Gregory Swift2 1Ball Aerospace and Technologies Boulder, CO 80027 USA 2Condensed Matter and Thermal Physics Group Los Alamos National Laboratory Los Alamos NM 87545 USA ABSTRACT Thermoacoustic theory is applied to oscillating flow in a parallel-plate gap with finite and unequal heat capacities on the two bounding walls, and with relative movement of one wall with respect to the other. The motivation is to understand the behavior of displacer gap losses at low temperatures in a Stirling cooler. Equations for the oscillating temperature and enthalpy flux down the gap and down the moving solid as a function of pressure amplitude, flow, temperatures, wall velocity, and material properties are derived. General expressions, along with results illustrating the behavior of the solutions, are presented. The primary result is that losses may increase significantly below 25 K, due to vanishing wall heat capacities and reduced thermal penetration depth in the helium gas. KEYWORDS: Thermoacoustics, Stirling, Cryocooler, Displacer PACS: 43.35.Ud INTRODUCTION In a Stirling cryocooler, there are two losses in the gap between the displacer and the displacer cylinder wall. One is shuttle loss, which arises from relative motion between the displacer and the wall, and the other is enthalpy flow loss due to oscillatory flow in the gap. These losses have previously been analyzed in detail, and in fact, for oscillatory flow between two stationary parallel surfaces with identical properties, software codes such as DeltaE [1], Sage [2], and REGEN3 [3] can provide solutions. These codes, however, are deficient when applied to low temperature displacer gaps. -
Thermodynamic Analysis of GM-Type Pulse Tube Coolers Q Y.L
Cryogenics 41 &2001) 513±520 www.elsevier.com/locate/cryogenics Thermodynamic analysis of GM-type pulse tube coolers q Y.L. Ju *,1 Cryogenic Laboratory, Chinese Academy of Sciences, P.O. Box 2711, Beijing 100080, People's Republic of China Received 29 January 2001; accepted 28 June 2001 Abstract The thermodynamic loss of rotary valve and the coecient of performance &COP) of GM-type pulse tube coolers &PTCs) are discussed and explained by using the ®rst and second laws of thermodynamics in this paper. The COP of GM-type PTC, based on two types of pressure pro®les, the sinusoidal wave inside the pulse tube and the step wave at the compressor side, has been derived and compared with that of Stirling-type PTC. Result shows that additional compressor work is needed due to the irreversible entropy productions in the rotary valve thereby decreasing the COP of GM-type PTC. The eect of double-inlet mode on the COP of PTC has distinct improvement at lower temperature region &larger TH=TL). It is also shown that the COP of GM-type PTC is independent of the shape of the pressure pro®les in the ideal case of no ¯ow resistance in the regenerator. Ó 2001 Elsevier Science Ltd. All rights reserved. Keywords: Pulse tube cooler; GM-type; Thermodynamic analysis 1. Introduction achieved [13]. All these machines use a compressor and a valve system to produce pressure oscillation in the In general pulse tube cooler &PTC) requires a phase cooler system. They are called GM-type PTCs. shifter system, located at the hot end of the pulse tube, A GM-type PTC, shown in Fig. -
MODELING and ANALYSIS of PULSE TUBE REFRIGERATOR 1Nishant Solanki, 2Nimesh Parmar
Solanki et al., International Journal of Advanced Engineering Technology E-ISSN 0976-3945 Research Paper MODELING AND ANALYSIS OF PULSE TUBE REFRIGERATOR 1Nishant Solanki, 2Nimesh Parmar Address for Correspondence 1Student, M.E. (Thermal Engineering), Gandhinagar Institute of Technology, Gandhinagar, Gujarat, India 2Asst. Professor, Mechanical Engineering Department, Gandhinagar Institute of Technology, Gandhinagar, Gujarat, India ABSTRACT: Cryogenics comes from the Greek word “kryos”, which means very cold or freezing and “genes” means to produce. Cryogenics is the science and technology associated with the phenomena that occur at very low temperature, close to the lowest theoretically attainable temperature. In this research paper, three dimensional model of pulse tube refrigerator is developed in ANSYS CFX and compared it with experimental results. It shows good agreement with experimental results with ANSYS CFD results. KEYWORDS : Pulse tube refrigerator, ANSYS CFD INTRODUCTION: volume on the thermodynamic performance of The pulse tube refrigerators (PTR) are capable of various components in a simple orifice and a double cooling to temperature below 123K. Unlike the inlet pulse tube cooler by combining a linearized ordinary refrigeration cycles which utilize the vapour model with a thermodynamic analysis. The results compression cycle as described in classical reveal that the performance of the pulse tube cooler is thermodynamics, a PTR implements the theory of significantly affected when the reservoir to pulse tube oscillatory compression and expansion of the gas volume ratio is less than 5, which helps the design of within a closed volume to achieve desired a practical pulse tube cooler. refrigeration. Being oscillatory, a PTR is a non steady Y.L. He, C.F. -
Recording and Evaluating the Pv Diagram with CASSY
LD Heat Physics Thermodynamic cycle Leaflets P2.6.2.4 Hot-air engine: quantitative experiments The hot-air engine as a heat engine: Recording and evaluating the pV diagram with CASSY Objects of the experiment Recording the pV diagram for different heating voltages. Determining the mechanical work per revolution from the enclosed area. Principles The cycle of a heat engine is frequently represented as a closed curve in a pV diagram (p: pressure, V: volume). Here the mechanical work taken from the system is given by the en- closed area: W = − ͛ p ⋅ dV (I) The cycle of the hot-air engine is often described in an idealised form as a Stirling cycle (see Fig. 1), i.e., a succession of isochoric heating (a), isothermal expansion (b), isochoric cooling (c) and isothermal compression (d). This description, however, is a rough approximation because the working piston moves sinusoidally and therefore an isochoric change of state cannot be expected. In this experiment, the pV diagram is recorded with the computer-assisted data acquisition system CASSY for comparison with the real behaviour of the hot-air engine. A pressure sensor measures the pressure p in the cylinder and a displacement sensor measures the position s of the working piston, from which the volume V is calculated. The measured values are immediately displayed on the monitor in a pV diagram. Fig. 1 pV diagram of the Stirling cycle 0210-Wei 1 P2.6.2.4 LD Physics Leaflets Setup Apparatus The experimental setup is illustrated in Fig. 2. 1 hot-air engine . 388 182 1 U-core with yoke . -
Novel Hot Air Engine and Its Mathematical Model – Experimental Measurements and Numerical Analysis
POLLACK PERIODICA An International Journal for Engineering and Information Sciences DOI: 10.1556/606.2019.14.1.5 Vol. 14, No. 1, pp. 47–58 (2019) www.akademiai.com NOVEL HOT AIR ENGINE AND ITS MATHEMATICAL MODEL – EXPERIMENTAL MEASUREMENTS AND NUMERICAL ANALYSIS 1 Gyula KRAMER, 2 Gabor SZEPESI *, 3 Zoltán SIMÉNFALVI 1,2,3 Department of Chemical Machinery, Institute of Energy and Chemical Machinery University of Miskolc, Miskolc-Egyetemváros 3515, Hungary e-mail: [email protected], [email protected], [email protected] Received 11 December 2017; accepted 25 June 2018 Abstract: In the relevant literature there are many types of heat engines. One of those is the group of the so called hot air engines. This paper introduces their world, also introduces the new kind of machine that was developed and built at Department of Chemical Machinery, Institute of Energy and Chemical Machinery, University of Miskolc. Emphasizing the novelty of construction and the working principle are explained. Also the mathematical model of this new engine was prepared and compared to the real model of engine. Keywords: Hot, Air, Engine, Mathematical model 1. Introduction There are three types of volumetric heat engines: the internal combustion engines; steam engines; and hot air engines. The first one is well known, because it is on zenith nowadays. The steam machines are also well known, because their time has just passed, even the elder ones could see those in use. But the hot air engines are forgotten. Our aim is to consider that one. The history of hot air engines is 200 years old. -
Section 15-6: Thermodynamic Cycles
Answer to Essential Question 15.5: The ideal gas law tells us that temperature is proportional to PV. for state 2 in both processes we are considering, so the temperature in state 2 is the same in both cases. , and all three factors on the right-hand side are the same for the two processes, so the change in internal energy is the same (+360 J, in fact). Because the gas does no work in the isochoric process, and a positive amount of work in the isobaric process, the First Law tells us that more heat is required for the isobaric process (+600 J versus +360 J). 15-6 Thermodynamic Cycles Many devices, such as car engines and refrigerators, involve taking a thermodynamic system through a series of processes before returning the system to its initial state. Such a cycle allows the system to do work (e.g., to move a car) or to have work done on it so the system can do something useful (e.g., removing heat from a fridge). Let’s investigate this idea. EXPLORATION 15.6 – Investigate a thermodynamic cycle One cycle of a monatomic ideal gas system is represented by the series of four processes in Figure 15.15. The process taking the system from state 4 to state 1 is an isothermal compression at a temperature of 400 K. Complete Table 15.1 to find Q, W, and for each process, and for the entire cycle. Process Special process? Q (J) W (J) (J) 1 ! 2 No +1360 2 ! 3 Isobaric 3 ! 4 Isochoric 0 4 ! 1 Isothermal 0 Entire Cycle No 0 Table 15.1: Table to be filled in to analyze the cycle. -
Thermodynamic Cycles of Direct and Pulsed-Propulsion Engines - V
THERMAL TO MECHANICAL ENERGY CONVERSION: ENGINES AND REQUIREMENTS – Vol. I - Thermodynamic Cycles of Direct and Pulsed-Propulsion Engines - V. B. Rutovsky THERMODYNAMIC CYCLES OF DIRECT AND PULSED- PROPULSION ENGINES V. B. Rutovsky Moscow State Aviation Institute, Russia. Keywords: Thermodynamics, air-breathing engine, turbojet. Contents 1. Cycles of Piston Engines of Internal Combustion. 2. Jet Engines Using Liquid Oxidants 3. Compressor-less Air-Breathing Jet Engines 3.1. Ramjet engine (with fuel combustion at p = const) 4. Pulsejet Engine. 5. Cycles of Gas-Turbine Propulsion Systems with Fuel Combustion at a Constant Volume Glossary Bibliography Summary This chapter considers engines with intermittent cycles and cycles of pulsejet engines. These include, piston engines of various designs, pulsejet engines, and gas-turbine propulsion systems with fuel combustion at a constant volume. This chapter presents thermodynamic cycles of thermal engines in which the propulsive mass is a mixture of air and either a gaseous fuel or vapor of a liquid fuel (on the initial portion of the cycle), and gaseous combustion products (over the rest of the cycle). 1. Cycles of Piston Engines of Internal Combustion. Piston engines of internal combustion are utilized in motor vehicles, aircraft, ships and boats, and locomotives. They are also used in stationary low-power electric generators. Given the variety of conditions that engines of internal combustion should meet, depending on their functions, engines of various types have been designed. From the standpointUNESCO of thermodynamics, however, – i.e. EOLSS in terms of operating cycles of these engines, all of them can be classified into three groups: (a) engines using cycles with heat addition at a constant volume (V = const); (b) engines using cycles with heat addition at a constantSAMPLE pressure (p = const); andCHAPTERS (c) engines using the so-called mixed cycles, in which heat is added at either a constant volume or a constant pressure. -
Thermodynamic Analysis of Solar Absorption Cooling System Open Access Jasim Abdulateef1,, Sameer Dawood Ali1, Mustafa Sabah Mahdi2
Journal of Advanced Research in Fluid Mechanics and Thermal Sciences 60, Issue 2 (2019) 233-246 Journal of Advanced Research in Fluid Mechanics and Thermal Sciences Journal homepage: www.akademiabaru.com/arfmts.html ISSN: 2289-7879 Thermodynamic Analysis of Solar Absorption Cooling System Open Access Jasim Abdulateef1,, Sameer Dawood Ali1, Mustafa Sabah Mahdi2 1 Mechanical Engineering Department, University of Diyala, 32001 Diyala, Iraq 2 Chemical Engineering Department, University of Diyala, 32001 Diyala, Iraq ARTICLE INFO ABSTRACT Article history: This study deals with thermodynamic analysis of solar assisted absorption refrigeration Received 16 April 2019 system. A computational routine based on entropy generation was written in MATLAB Received in revised form 14 May 2019 to investigate the irreversible losses of individual component and the total entropy Accepted 18 July 2018 generation (푆̇ ) of the system. The trend in coefficient of performance COP and 푆̇ Available online 28 August 2019 푡표푡 푡표푡 with the variation of generator, evaporator, condenser and absorber temperatures and heat exchanger effectivenesses have been presented. The results show that, both COP and Ṡ tot proportional with the generator and evaporator temperatures. The COP and irreversibility are inversely proportional to the condenser and absorber temperatures. Further, the solar collector is the largest fraction of total destruction losses of the system followed by the generator and absorber. The maximum destruction losses of solar collector reach up to 70% and within the range 6-14% in case of generator and absorber. Therefore, these components require more improvements as per the design aspects. Keywords: Refrigeration; absorption; solar collector; entropy generation; irreversible losses Copyright © 2019 PENERBIT AKADEMIA BARU - All rights reserved 1. -
Tabletop Thermoacoustic Refrigerator for Demonstrations Daniel A
Tabletop thermoacoustic refrigerator for demonstrations Daniel A. Russell and Pontus Weibulla) Science and Mathematics Department, Kettering University,b͒ Flint, Michigan 48504 ͑Received 29 May 2001; accepted 22 April 2002͒ An inexpensive ͑less than $25͒ tabletop thermoacoustic refrigerator for demonstration purposes was built from a boxed loudspeaker, acrylic tubing and sheet, a roll of 35 mm film, fishing line, an aluminum plug, and two homemade thermocouples. Temperature differences of more than 15 °C were achieved after running the cooler for several minutes. While nowhere near the efficiency of devices described in the literature, this demonstration model effectively illustrates the behavior of a thermoacoustic refrigerator. © 2002 American Association of Physics Teachers. ͓DOI: 10.1119/1.1485720͔ I. INTRODUCTION around a central spindle so that adjacent layers of the spirally wound film provide the stack surfaces. Lengths of 15-lb ny- The basic workings of heat engines and refrigerators are lon fishing line separated adjacent layers of the spirally commonly described in the undergraduate physics curricu- wound film stack so that air could move between the layers lum. Thermoacoustic heat engines and refrigerators, how- along the length of the stack parallel to the length of the ever, are topics usually reserved for graduate level courses resonator tube. Figure 1͑b͒ shows a cross section of the and research. Recent articles in popular scientific journals rolled-film stack, with layers separated by fishing line. have made the concepts behind such devices understandable 1,2 The primary constraint in designing the stack is the fact to a much wider audience. A demonstration apparatus, as that stack layers need to be a few thermal penetration depths described in this note, can effectively introduce students to apart, with four thermal penetration depths being the opti- the physics behind thermoacoustic refrigerators. -
Design of Thermoacoustic Refrigerators M.E.H
Cryogenics 42 (2002) 49–57 www.elsevier.com/locate/cryogenics Design of thermoacoustic refrigerators M.E.H. Tijani, J.C.H. Zeegers, A.T.A.M. de Waele * Department of Applied Physics, Eindhoven University of Technology, P.O. Box 513, 5600 MB Eindhoven, Netherlands Received 12 November 2001; accepted 5 December 2001 Abstract In this paper the design of thermoacoustic refrigerators, using the linear thermoacoustic theory, is described. Due to the large number of parameters, a choice of some parameters along with dimensionless independent variables will be introduced. The design strategy described in this paper is a guide for the design and development of thermoacoustic coolers. The optimization of the different parts of the refrigerator will be discussed, and criteria will be given to obtain an optimal system. Ó 2002 Elsevier Science Ltd. All rights reserved. Keywords: Thermoacoustic; Refrigeration 1. Introduction temperature of À65 °C. The measurement results can be found elsewhere [3,4]. The theory of thermoacoustics is well established, but quantitative engineering approach to design thermoa- coustic refrigerators is still lacking in the literature. 2. Design strategy Thermoacoustic refrigerators are systems which use sound to generate cooling power. They consist mainly of We start by considering the design and optimization of a loudspeaker attached to an acoustic resonator (tube) the stack which forms the heart of the cooler. The coef- filled with a gas. In the resonator, a stack consisting of a ficient of performance of the stack, defined as the ratio of number of parallel plates and two heat exchangers, are the heat pumped by the stack to the acoustic power used installed, as shown in Fig. -
Power Plant Steam Cycle Theory - R.A
THERMAL POWER PLANTS – Vol. I - Power Plant Steam Cycle Theory - R.A. Chaplin POWER PLANT STEAM CYCLE THEORY R.A. Chaplin Department of Chemical Engineering, University of New Brunswick, Canada Keywords: Steam Turbines, Carnot Cycle, Rankine Cycle, Superheating, Reheating, Feedwater Heating. Contents 1. Cycle Efficiencies 1.1. Introduction 1.2. Carnot Cycle 1.3. Simple Rankine Cycles 1.4. Complex Rankine Cycles 2. Turbine Expansion Lines 2.1. T-s and h-s Diagrams 2.2. Turbine Efficiency 2.3. Turbine Configuration 2.4. Part Load Operation Glossary Bibliography Biographical Sketch Summary The Carnot cycle is an ideal thermodynamic cycle based on the laws of thermodynamics. It indicates the maximum efficiency of a heat engine when operating between given temperatures of heat acceptance and heat rejection. The Rankine cycle is also an ideal cycle operating between two temperature limits but it is based on the principle of receiving heat by evaporation and rejecting heat by condensation. The working fluid is water-steam. In steam driven thermal power plants this basic cycle is modified by incorporating superheating and reheating to improve the performance of the turbine. UNESCO – EOLSS The Rankine cycle with its modifications suggests the best efficiency that can be obtained from this two phaseSAMPLE thermodynamic cycle wh enCHAPTERS operating under given temperature limits but its efficiency is less than that of the Carnot cycle since some heat is added at a lower temperature. The efficiency of the Rankine cycle can be improved by regenerative feedwater heating where some steam is taken from the turbine during the expansion process and used to preheat the feedwater before it is evaporated in the boiler. -
Comparison of ORC Turbine and Stirling Engine to Produce Electricity from Gasified Poultry Waste
Sustainability 2014, 6, 5714-5729; doi:10.3390/su6095714 OPEN ACCESS sustainability ISSN 2071-1050 www.mdpi.com/journal/sustainability Article Comparison of ORC Turbine and Stirling Engine to Produce Electricity from Gasified Poultry Waste Franco Cotana 1,†, Antonio Messineo 2,†, Alessandro Petrozzi 1,†,*, Valentina Coccia 1, Gianluca Cavalaglio 1 and Andrea Aquino 1 1 CRB, Centro di Ricerca sulle Biomasse, Via Duranti sn, 06125 Perugia, Italy; E-Mails: [email protected] (F.C.); [email protected] (V.C.); [email protected] (G.C.); [email protected] (A.A.) 2 Università degli Studi di Enna “Kore” Cittadella Universitaria, 94100 Enna, Italy; E-Mail: [email protected] † These authors contributed equally to this work. * Author to whom correspondence should be addressed; E-Mail: [email protected]; Tel.: +39-075-585-3806; Fax: +39-075-515-3321. Received: 25 June 2014; in revised form: 5 August 2014 / Accepted: 12 August 2014 / Published: 28 August 2014 Abstract: The Biomass Research Centre, section of CIRIAF, has recently developed a biomass boiler (300 kW thermal powered), fed by the poultry manure collected in a nearby livestock. All the thermal requirements of the livestock will be covered by the heat produced by gas combustion in the gasifier boiler. Within the activities carried out by the research project ENERPOLL (Energy Valorization of Poultry Manure in a Thermal Power Plant), funded by the Italian Ministry of Agriculture and Forestry, this paper aims at studying an upgrade version of the existing thermal plant, investigating and analyzing the possible applications for electricity production recovering the exceeding thermal energy. A comparison of Organic Rankine Cycle turbines and Stirling engines, to produce electricity from gasified poultry waste, is proposed, evaluating technical and economic parameters, considering actual incentives on renewable produced electricity.