Thermodynamics (2) (Lectures)
Total Page:16
File Type:pdf, Size:1020Kb
Load more
Recommended publications
-
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. -
Fuel Cells Versus Heat Engines: a Perspective of Thermodynamic and Production
Fuel Cells Versus Heat Engines: A Perspective of Thermodynamic and Production Efficiencies Introduction: Fuel Cells are being developed as a powering method which may be able to provide clean and efficient energy conversion from chemicals to work. An analysis of their real efficiencies and productivity vis. a vis. combustion engines is made in this report. The most common mode of transportation currently used is gasoline or diesel engine powered automobiles. These engines are broadly described as internal combustion engines, in that they develop mechanical work by the burning of fossil fuel derivatives and harnessing the resultant energy by allowing the hot combustion product gases to expand against a cylinder. This arrangement allows for the fuel heat release and the expansion work to be performed in the same location. This is in contrast to external combustion engines, in which the fuel heat release is performed separately from the gas expansion that allows for mechanical work generation (an example of such an engine is steam power, where fuel is used to heat a boiler, and the steam then drives a piston). The internal combustion engine has proven to be an affordable and effective means of generating mechanical work from a fuel. However, because the majority of these engines are powered by a hydrocarbon fossil fuel, there has been recent concern both about the continued availability of fossil fuels and the environmental effects caused by the combustion of these fuels. There has been much recent publicity regarding an alternate means of generating work; the hydrogen fuel cell. These fuel cells produce electric potential work through the electrochemical reaction of hydrogen and oxygen, with the reaction product being water. -
The Aircraft Propulsion the Aircraft Propulsion
THE AIRCRAFT PROPULSION Aircraft propulsion Contact: Ing. Miroslav Šplíchal, Ph.D. [email protected] Office: A1/0427 Aircraft propulsion Organization of the course Topics of the lectures: 1. History of AE, basic of thermodynamic of heat engines, 2-stroke and 4-stroke cycle 2. Basic parameters of piston engines, types of piston engines 3. Design of piston engines, crank mechanism, 4. Design of piston engines - auxiliary systems of piston engines, 5. Performance characteristics increase performance, propeller. 6. Turbine engines, introduction, input system, centrifugal compressor. 7. Turbine engines - axial compressor, combustion chamber. 8. Turbine engines – turbine, nozzles. 9. Turbine engines - increasing performance, construction of gas turbine engines, 10. Turbine engines - auxiliary systems, fuel-control system. 11. Turboprop engines, gearboxes, performance. 12. Maintenance of turbine engines 13. Ramjet engines and Rocket engines Aircraft propulsion Organization of the course Topics of the seminars: 1. Basic parameters of piston engine + presentation (1-7)- 3.10.2017 2. Parameters of centrifugal flow compressor + presentation(8-14) - 17.10.2017 3. Loading of turbine blade + presentation (15-21)- 31.10.2017 4. Jet engine cycle + presentation (22-28) - 14.11.2017 5. Presentation alternative date Seminar work: Aircraft engines presentation A short PowerPoint presentation, aprox. 10 minutes long. Content of presentation: - a brief history of the engine - the main innovation introduced by engine - engine drawing / cross-section - -
Carnot Cycles
CARNOT CYCLES Sadi Carnot was a French physicist who proposed an “ideal” cycle for a heat engine in 1824. Historical note – the idea of an ideal cycle came about because engineers were trying to develop a steam engine (a type of heat engine) where they could reject (waste) a minimal amount of heat. This would produce the best efficiency since η = 1 – (QL/QH). Carnot proposed that a cycle comprised of completely (internally and externally) reversible processes would give the maximum amount of net work for a given heat input, since the work done by a system in a reversible (ideal) process is always greater than that in an irreversible (real) process. THE CARNOT HEAT ENGINE CYCLE CONSISTS OF FOUR REVERSIBLE PROCESSES IN A SEQUENCE: 1 Æ 2: Reversible isothermal expansion. Heat transfer from HTR (+) and boundary work (+) occur in closed system 2 Æ 3: Reversible adiabatic expansion Work output (+), but no heat transfer 3 Æ 4: Reversible isothermal compression Heat transfer (-) and boundary work (-) occur in closed system 4 Æ 1: Reversible adiabatic compression Work input (-), but no heat transfer AND Wout >>> Win 1 P-V DIAGRAM FOR CARNOT HEAT ENGINE CYCLE P 1 2 4 3 Showing net work is POSITIVE. V A useful example of an isothermal expansion is boiling (vaporization) at a constant pressure in a device such as a piston-cylinder. Similarly, an example of an isothermal compression is condensation at a constant pressure in a piston-cylinder. Also, heat transfer can only occur in processes 1 Æ 2 and 3 Æ4. 1 Æ 2: since work is positive (expansion) and Δu is positive (e.g., boiling) then heat transfer is positive (input from HTR). -
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. -
Lecture 10. Heat Engines (Ch. 4)
Lecture 11. Heat Engines (Ch. 4) A heat engine – any device that is capable of converting thermal energy (heating) into mechanical energy (work). We will consider an important class of such devices whose operation is cyclic. Heating – the transfer of energy to a system by thermal contact with a reservoir. Work – the transfer of energy to a system by a change in the external parameters (V, el.-mag. and grav. fields, etc.). The main question we want to address: what are the limitations imposed by thermodynamic on the performance of heat engines? Perpetual Motion Machines are Impossible Perpetual Motion Machines of the first type – these designs seek to violation of the First Law create the energy required for their (energy conservation) operation out of nothing. Perpetual Motion Machines of the second type - these designs extract the energy required for their operation violation of the Second in a manner that decreases the entropy Law of an isolated system. hot reservoir Word of caution: for non-cyclic processes, T H 100% of heat can be transformed into work without violating the Second Law. heat Example: an ideal gas expands isothermally work being in thermal contact with a hot reservoir. Since U = const at T = const, all heat has been transformed into work. impossible cyclic heat engine Fundamental Difference between Heating and Work - is the difference in the entropy transfer! Transferring purely mechanical energy to or from a system does not (necessarily) change its entropy: ΔS = 0 for reversible processes. For this reason, all forms of work are thermodynamically equivalent to each other - they are freely convertible into each other and, in particular, into mechanical work. -
Carnot Heat Engine Efficiency with a Paramagnetic Gas
Carnot heat engine efficiency with a paramagnetic gas Manuel Malaver1,2,3 1 Bijective Physics Institute, Bijective Physics Group, Idrija, Slovenia 2 Entro-π Fluid Research Group. 3 Maritime University of the Caribbean, Catia la Mar, Venezuela. *Corresponding author (Email: [email protected]) Abstract – Considering ideal paramagnetic medium, in this paper we deduced an expression for the thermal efficiency of Carnot heat engine with a paramagnetic gas as working substance. We found that the efficiency depends on the limits of maximum and minimal temperature imposed on the Carnot cycle, as in the ideal gas, photon gas and variable Chaplygin gas. Keywords – Carnot heat engine, ideal paramagnetic medium, thermal efficiency, paramagnetic gas. 1. Introduction The magnetism is a type of associated physical phenomena with the orbital and spin motions of electrons and the interaction of electrons with each other (Ahmed et al., 2019). The electric currents and the atomic magnetic moment of elementary particles generate magnetic fields that can act on other currents and magnetic materials. The most common effect occurs in ferromagnetic solids which is possible when atoms are rearrange in such a way that magnetic atomic moments can interact to align parallel to each other (Eisberg and Resnick, 1991; Chikazumi, 2009). In quantum mechanics, the ferromagnetism can be described as a parallel alignment of magnetic moments what depends of the interaction between neighbouring moments (Feynman et al., 1963). Although ferromagnetism is the cause of many frequently observed magnetism effects, not all materials respond equally to magnetic fields because the interaction between magnetic atomic moments is very weak while in other materials this interaction is stronger (Ahmed et al., 2019). -
Performance of a Combined ORC and VCC for Heat Activated
Performance of a Combined Organic Rankine Cycle and Vapor Compression Cycle for Heat Activated Cooling Hailei Wang*, Richard Peterson, Kevin Harada, Erik Miller, Robbie Ingram-Goble, Luke Fisher, James Yih, Chris Ward School of Mechanical, Industrial, & Manufacturing Engineering 204 Rogers Hall, Oregon State University Corvallis, OR 97331, USA * Corresponding Author Phone: 541-713-1354, Fax: 541-758-9320, Email: [email protected] Abstract Heat activated cooling has the potential of utilizing thermal sources that currently go unused such as engine exhaust heat or industrial waste heat. Using these heat sources can provide enhanced energy utilization and reduced fuel usage in applications where cooling is needed. The concept developed here uses waste heat from stationary and mobile engine cycles to generate cooling for structures and vehicles. It combines an organic Rankine cycle (ORC) with a conventional vapor compression cycle. A nominal 5 kW cooling capacity prototype system was developed based on this concept and tested under laboratory conditions. In order to maintain high system performance while reducing size and weight for portable applications, microchannel based heat transfer components and scroll based expansion and compression were used. Although the system was tested off of its design point, it performed well achieving 4.4 kW of cooling at a measured heat activated COP of 0.48. Both the conversion and 2 nd law efficiencies were close to the model results, proving it to be an attractive technology. The measured isentropic efficiency of the scroll expander reached 84%, when the pressure ratio was close to the scroll intrinsic expansion ratio. The reduced cooling capacity was attributed to off design operation. -
Lecture 11 Second Law of Thermodynamics
LECTURE 11 SECOND LAW OF THERMODYNAMICS Lecture instructor: Kazumi Tolich Lecture 11 2 ¨ Reading chapter 18.5 to 18.10 ¤ The second law of thermodynamics ¤ Heat engines ¤ Refrigerators ¤ Air conditions ¤ Heat pumps ¤ Entropy Second law of thermodynamics 3 ¨ The second law of thermodynamics states: Thermal energy flows spontaneously from higher to lower temperature. Heat engines are always less than 100% efficient at using thermal energy to do work. The total entropy of all the participants in any physical process cannot decrease during that process. Heat engines 4 ¨ Heat engines depend on the spontaneous heat flow from hot to cold to do work. ¨ In each cycle, the hot reservoir supplies heat �" to the engine which does work �and exhausts heat �$ to the cold reservoir. � = �" − �$ ¨ The energy efficiency of a heat engine is given by � � = �" Carnot’s theorem and maximum efficiency 5 ¨ The maximum-efficiency heat engine is described in Carnot’s theorem: If an engine operating between two constant-temperature reservoirs is to have maximum efficiency, it must be an engine in which all processes are reversible. In addition, all reversible engines operating between the same two temperatures, �$ and �", have the same efficiency. ¨ This is an idealization; no real engine can be perfectly reversible. ¨ The maximum efficiency of a heat engine (Carnot engine) can be written as: �$ �*+, = 1 − �" Quiz: 1 6 ¨ Consider the heat engine at right. �. denotes the heat extracted from the hot reservoir, and �/ denotes the heat exhausted to the cold reservoir in one cycle. What is the work done by this engine in one cycle in Joules? Quiz: 11-1 answer 7 ¨ 4000 J ¨ � = �.