Adiabatic Processes Introduction
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Advanced Organic Vapor Cycles for Improving Thermal Conversion Efficiency in Renewable Energy Systems by Tony Ho a Dissertation
Advanced Organic Vapor Cycles for Improving Thermal Conversion Efficiency in Renewable Energy Systems By Tony Ho A dissertation submitted in partial satisfaction of the requirements for the degree of Doctor of Philosophy in Engineering – Mechanical Engineering in the Graduate Division of the University of California, Berkeley Committee in charge: Professor Ralph Greif, Co-Chair Professor Samuel S. Mao, Co-Chair Professor Van P. Carey Professor Per F. Peterson Spring 2012 Abstract Advanced Organic Vapor Cycles for Improving Thermal Conversion Efficiency in Renewable Energy Systems by Tony Ho Doctor of Philosophy in Mechanical Engineering University of California, Berkeley Professor Ralph Greif, Co-Chair Professor Samuel S. Mao, Co-Chair The Organic Flash Cycle (OFC) is proposed as a vapor power cycle that could potentially increase power generation and improve the utilization efficiency of renewable energy and waste heat recovery systems. A brief review of current advanced vapor power cycles including the Organic Rankine Cycle (ORC), the zeotropic Rankine cycle, the Kalina cycle, the transcritical cycle, and the trilateral flash cycle is presented. The premise and motivation for the OFC concept is that essentially by improving temperature matching to the energy reservoir stream during heat addition to the power cycle, less irreversibilities are generated and more power can be produced from a given finite thermal energy reservoir. In this study, modern equations of state explicit in Helmholtz energy such as the BACKONE equations, multi-parameter Span- Wagner equations, and the equations compiled in NIST REFPROP 8.0 were used to accurately determine thermodynamic property data for the working fluids considered. Though these equations of state tend to be significantly more complex than cubic equations both in form and computational schemes, modern Helmholtz equations provide much higher accuracy in the high pressure regions, liquid regions, and two-phase regions and also can be extended to accurately describe complex polar fluids. -
Compression of an Ideal Gas with Temperature Dependent Specific
Session 3666 Compression of an Ideal Gas with Temperature-Dependent Specific Heat Capacities Donald W. Mueller, Jr., Hosni I. Abu-Mulaweh Engineering Department Indiana University–Purdue University Fort Wayne Fort Wayne, IN 46805-1499, USA Overview The compression of gas in a steady-state, steady-flow (SSSF) compressor is an important topic that is addressed in virtually all engineering thermodynamics courses. A typical situation encountered is when the gas inlet conditions, temperature and pressure, are known and the compressor dis- charge pressure is specified. The traditional instructional approach is to make certain assumptions about the compression process and about the gas itself. For example, a special case often consid- ered is that the compression process is reversible and adiabatic, i.e. isentropic. The gas is usually ÊÌ considered to be ideal, i.e. ÈÚ applies, with either constant or temperature-dependent spe- cific heat capacities. The constant specific heat capacity assumption allows for direct computation of the discharge temperature, while the temperature-dependent specific heat assumption does not. In this paper, a MATLAB computer model of the compression process is presented. The substance being compressed is air which is considered to be an ideal gas with temperature-dependent specific heat capacities. Two approaches are presented to describe the temperature-dependent properties of air. The first approach is to use the ideal gas table data from Ref. [1] with a look-up interpolation scheme. The second approach is to use a curve fit with the NASA Lewis coefficients [2,3]. The computer model developed makes use of a bracketing–bisection algorithm [4] to determine the temperature of the air after compression. -
Analysis of a CO2 Transcritical Refrigeration Cycle with a Vortex Tube Expansion
sustainability Article Analysis of a CO2 Transcritical Refrigeration Cycle with a Vortex Tube Expansion Yefeng Liu *, Ying Sun and Danping Tang University of Shanghai for Science and Technology, Shanghai 200093, China; [email protected] (Y.S.); [email protected] (D.T.) * Correspondence: [email protected]; Tel.: +86-21-55272320; Fax: +86-21-55272376 Received: 25 January 2019; Accepted: 19 March 2019; Published: 4 April 2019 Abstract: A carbon dioxide (CO2) refrigeration system in a transcritical cycle requires modifications to improve the coefficient of performance (COP) for energy saving. This modification has become more important with the system’s more and more widely used applications in heat pump water heaters, automotive air conditioning, and space heating. In this paper, a single vortex tube is proposed to replace the expansion valve of a traditional CO2 transcritical refrigeration system to reduce irreversible loss and improve the COP. The principle of the proposed system is introduced and analyzed: Its mathematical model was developed to simulate and compare the system performance to the traditional system. The results showed that the proposed system could save energy, and the vortex tube inlet temperature and discharge pressure had significant impacts on COP improvement. When the vortex tube inlet temperature was 45 ◦C, and the discharge pressure was 9 MPa, the COP increased 33.7%. When the isentropic efficiency or cold mass fraction of the vortex tube increased, the COP increased about 10%. When the evaporation temperature or the cooling water inlet temperature of the desuperheater decreased, the COP also could increase about 10%. The optimal discharge pressure correlation of the proposed system was established, and its influences on COP improvement are discussed. -
Eindhoven University of Technology MASTER Counterflow Pulse-Tube
Eindhoven University of Technology MASTER Counterflow pulse-tube refrigerator Franssen, R.J.M. Award date: 2001 Link to publication Disclaimer This document contains a student thesis (bachelor's or master's), as authored by a student at Eindhoven University of Technology. Student theses are made available in the TU/e repository upon obtaining the required degree. The grade received is not published on the document as presented in the repository. The required complexity or quality of research of student theses may vary by program, and the required minimum study period may vary in duration. General rights Copyright and moral rights for the publications made accessible in the public portal are retained by the authors and/or other copyright owners and it is a condition of accessing publications that users recognise and abide by the legal requirements associated with these rights. • Users may download and print one copy of any publication from the public portal for the purpose of private study or research. • You may not further distribute the material or use it for any profit-making activity or commercial gain Technische Universiteit Eindhoven Faculteit Technische Natuurkunde Capaciteitsgroep Lage Temperaturen Counterflow pulse-tube refrigerator R.J.M. Franssen Prof. Dr. A.T.A.M. de Waele (supervisor and coach) May 2001 Abstract Abstract In this report we discuss a new type of pulse-tube refrigerator. A pulse-tube refrigerator is a cooler with no moving parts in the cold region. This has the advantage that the cooler is simpler and more reliable, and it also reduces vibrations, which is useful in several applications. -
High Efficiency and Large-Scale Subsurface Energy Storage with CO2
PROCEEDINGS, 43rd Workshop on Geothermal Reservoir Engineering Stanford University, Stanford, California, February 12-14, 2018 SGP-TR-213 High Efficiency and Large-scale Subsurface Energy Storage with CO2 Mark R. Fleming1, Benjamin M. Adams2, Jimmy B. Randolph1,3, Jonathan D. Ogland-Hand4, Thomas H. Kuehn1, Thomas A. Buscheck3, Jeffrey M. Bielicki4, Martin O. Saar*1,2 1University of Minnesota, Minneapolis, MN, USA; 2ETH-Zurich, Zurich, Switzerland; 3TerraCOH Inc., Minneapolis, MN, USA; 4The Ohio State University, Columbus, OH, USA; 5Lawrence Livermore National Laboratory, Livermore, CA, USA. *Corresponding Author: [email protected] Keywords: geothermal energy, multi-level geothermal systems, sedimentary basin, carbon dioxide, electricity generation, energy storage, power plot, CPG ABSTRACT Storing large amounts of intermittently produced solar or wind power for later, when there is a lack of sunlight or wind, is one of society’s biggest challenges when attempting to decarbonize energy systems. Traditional energy storage technologies tend to suffer from relatively low efficiencies, severe environmental concerns, and limited scale both in capacity and time. Subsurface energy storage can solve the drawbacks of many other energy storage approaches, as it can be large scale in capacity and time, environmentally benign, and highly efficient. When CO2 is used as the (pressure) energy storage medium in reservoirs underneath caprocks at depths of at least ~1 km (to ensure the CO2 is in its supercritical state), the energy generated after the energy storage operation can be greater than the energy stored. This is possible if reservoir temperatures and CO2 storage durations combine to result in more geothermal energy input into the CO2 at depth than what the CO2 pumps at the surface (and other machinery) consume. -
Thermodynamics of Ideal Gases
D Thermodynamics of ideal gases An ideal gas is a nice “laboratory” for understanding the thermodynamics of a fluid with a non-trivial equation of state. In this section we shall recapitulate the conventional thermodynamics of an ideal gas with constant heat capacity. For more extensive treatments, see for example [67, 66]. D.1 Internal energy In section 4.1 we analyzed Bernoulli’s model of a gas consisting of essentially 1 2 non-interacting point-like molecules, and found the pressure p = 3 ½ v where v is the root-mean-square average molecular speed. Using the ideal gas law (4-26) the total molecular kinetic energy contained in an amount M = ½V of the gas becomes, 1 3 3 Mv2 = pV = nRT ; (D-1) 2 2 2 where n = M=Mmol is the number of moles in the gas. The derivation in section 4.1 shows that the factor 3 stems from the three independent translational degrees of freedom available to point-like molecules. The above formula thus expresses 1 that in a mole of a gas there is an internal kinetic energy 2 RT associated with each translational degree of freedom of the point-like molecules. Whereas monatomic gases like argon have spherical molecules and thus only the three translational degrees of freedom, diatomic gases like nitrogen and oxy- Copyright °c 1998{2004, Benny Lautrup Revision 7.7, January 22, 2004 662 D. THERMODYNAMICS OF IDEAL GASES gen have stick-like molecules with two extra rotational degrees of freedom or- thogonally to the bridge connecting the atoms, and multiatomic gases like carbon dioxide and methane have the three extra rotational degrees of freedom. -
Thermodynamics for Cryogenics
Thermodynamics for Cryogenics Ram C. Dhuley USPAS – Cryogenic Engineering June 21 – July 2, 2021 Goals of this lecture • Revise important definitions in thermodynamics – system and surrounding, state properties, derived properties, processes • Revise laws of thermodynamics and learn how to apply them to cryogenic systems • Learn about ‘ideal’ thermodynamic processes and their application to cryogenic systems • Prepare background for analyzing real-world helium liquefaction and refrigeration cycles. 2 Ram C. Dhuley | USPAS Cryogenic Engineering (Jun 21 - Jul 2, 2021) Introduction • Thermodynamics deals with the relations between heat and other forms of energy such as mechanical, electrical, or chemical energy. • Thermodynamics has its basis in attempts to understand combustion and steam power but is still “state of the art” in terms of practical engineering issues for cryogenics, especially in process efficiency. James Dewar (invented vacuum flask in 1892) https://physicstoday.scitation.org/doi/10.1063/1.881490 3 Ram C. Dhuley | USPAS Cryogenic Engineering (Jun 21 - Jul 2, 2021) Definitions • Thermodynamic system is the specified region in which heat, work, and mass transfer are being studied. • Surrounding is everything else other than the system. • Thermodynamic boundary is a surface separating the system from the surrounding. Boundary System Surrounding 4 Ram C. Dhuley | USPAS Cryogenic Engineering (Jun 21 - Jul 2, 2021) Definitions (continued) Types of thermodynamic systems • Isolated system has no exchange of mass or energy with its surrounding • Closed system exchanges heat but not mass • Open system exchanges both heat and mass with its surrounding Thermodynamic State • Thermodynamic state is the condition of the system at a given time, defined by ‘state’ properties • More details on next slides • Two state properties define a state of a “homogenous” system • Usually, three state properties are needed to define a state of a non-homogenous system (example: two phase, mixture) 5 Ram C. -
Thermodynamic Modeling of an Atkinson Cycle with Respect to Relative AirFuel Ratio, Fuel Mass Flow Rate and Residual Gases R
Vol. 124 (2013) ACTA PHYSICA POLONICA A No. 1 Thermodynamic Modeling of an Atkinson Cycle with respect to Relative AirFuel Ratio, Fuel Mass Flow Rate and Residual Gases R. Ebrahimi∗ Department of Agriculture Machine Mechanics, Shahrekord University, P.O. Box 115, Shahrekord, Iran (Received March 26, 2013; in nal form April 17, 2013) The performance of an air standard Atkinson cycle is analyzed using nite-time thermodynamics. The results show that if the compression ratio is less than a certain value, the power output increases with increasing relative airfuel ratio, while if the compression ratio exceeds a certain value, the power output rst increases and then starts to decrease with increase of relative airfuel ratio. With a further increase in compression ratio, the increase in relative airfuel ratio results in decrease of the power output. Throughout the compression ratio range, the power output increases with increase of fuel mass ow rate. The results also show that if the compression ratio is less than a certain value, the power output increases with increase of residual gases, on the contrast, if the compression ratio exceeds a certain value, the power output decreases with increase of residual gases. The results obtained herein can provide guidance for the design of practical Atkinson engines. DOI: 10.12693/APhysPolA.124.29 PACS: 05.70.Ln, 82.60.Fa, 88.05.−b 1. Introduction formance of an air standard Atkinson cycle under the re- striction of the maximum cycle temperature. The results The Atkinson cycle is a type of internal combustion show that the power output as well as the eciency, for engine, which was designed and built by a British engi- which the maximum power-output occurs, will rise with neer James Atkinson in 1882. -