Thermodynamics Fundamentals for Energy Conversion Systems Renewable Energy Applications
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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. -
Equilibrium, Energy Conservation, and Temperature Chapter Objectives
Equilibrium, Energy Conservation, and Temperature Chapter Objectives 1. Explain thermal equilibrium and how it relates to energy transport. 2. Understand temperature ranges important for biological systems and temperature sensing in mammals. 3. Understand temperature ranges important for the environment. 1. Thermal equilibrium and the Laws of thermodynamics Laws of Thermodynamics Energy of the system + = Constant Energy of surrounding Energy Conservation 1. Thermal equilibrium and the Laws of thermodynamics Energy conservation Rate of Rate of Rate of Rate of Energy In Energy Out Energy Generation Energy Storage 1. Thermal equilibrium and the Laws of thermodynamics Ex) Solid is put in the liquid. specific mass heat temperature Solid Liquid Energy = m( − ) 1. Thermal equilibrium and the Laws of thermodynamics Energy In = − Energy Out = 0 Energy Generation = 0 Energy Storage = ( +) − −( −) >> Use the numerical values as shown in last page’s picture and equation of energy conservation. Using energy conservation, we can find the final or equilibrium temperature. 2. Temperature in Living System Most biological activity is confined to a rather narrow temperature range of 0~60°C 2. Temperature in Living System Temperature Response to Human body How temperature affects the state of human body? - As shown in this picture, it is obvious that temperature needs to be controlled. 2. Temperature in Living System Temperature Sensation in Humans - The human being can perceive different gradations of cold and heat, as shown in this picture. 2. Temperature in Living System Thermal Comfort of Human and Animals - Body heat losses are affected by air temperature, humidity, velocity and other factors. - Especially, affected by humidity. 3. -
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 . -
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. -
Measuring the Steady State Thermal Efficiency of a Heating System
Measuring the Steady State Thermal Efficiency of a Heating System. Last week you had a tour of “Colby Power and Light” and had a chance to see Gus Libby’s really cool, campus-scale, multi-million dollar calorimeter. This week we will use lab-scale calorimeters to measure the heat and carbon content of different fuels (methane, propane, butane, and gasoline). Our simple calorimeters were designed by Whitney King and Chuck Jones, Science Division Instrument Wizard, to simulate the highly efficient HTP Versa Flame fire-tube boiler. The lab has three parts: 1) Calibrate the calorimeter 2) Measure the heat content of different fuels 3) Compare the measured heat content to the calculated heat content 1) Calibrate the Calorimeter. You lab instructor will demonstrate the assembly of the laboratory- scale fire-tube calorimeter. The heat transferred from the burning fuel to the calorimeter can be determined from the mass of the object being heated, the heat capacity of the object and the change in temperature. � = ���� ∗ �� ∗ ∆� We will begin the experiment by adding a known amount of heat to our calorimeters from a coffee cup heater. The heater is a simple resistor that converts electrical energy into heat. The heater has a resistance of 47.5 ohms and is plugged into a 120 V outlet. Recalling your electricity basics, we know that V=IR where V is the voltage in Figure 1. HTP Versa Flame Fire Tube volts, I is the current in amps, and R is the Boiler. Brown Tubes carry the hot resistance in ohms. The power, P, consumed by combustion gasses inside of the the heater is volts times current, water tank where they condense releasing the maximum available 2 heat. -
Thermal Physics
Slide 1 / 163 Slide 2 / 163 Thermal Physics www.njctl.org Slide 3 / 163 Slide 4 / 163 Thermal Physics · Temperature, Thermal Equilibrium and Thermometers · Thermal Expansion · Heat and Temperature Change · Thermal Equilibrium : Heat Calculations · Phase Transitions · Heat Transfer · Gas Laws Temperature, Thermal Equilibrium · Kinetic Theory Click on the topic to go to that section · Internal Energy and Thermometers · Work in Thermodynamics · First Law of Thermodynamics · Thermodynamic Processes · Second Law of Thermodynamics · Heat Engines · Entropy and Disorder Return to Table of Contents Slide 5 / 163 Slide 6 / 163 Temperature and Heat Temperature Here are some definitions of temperature: In everyday language, many of us use the terms temperature · A measure of the warmth or coldness of an object or substance with and heat interchangeably reference to some standard value. But in physics, these terms have very different meanings. · Any of various standardized numerical measures of this ability, such Think about this… as the Kelvin, Fahrenheit, and Celsius scale. · When you touch a piece of metal and a piece of wood both · A measure of the ability of a substance, or more generally of any resting in front of you, which feels warmer? · When do you feel warmer when the air around you is 90°F physical system, to transfer heat energy to another physical system. and dry or when it is 90°F and very humid? · A measure of the average kinetic energy of the particles in a sample · In both cases the temperatures of what you are feeling is of matter, expressed in terms of units or degrees designated on a the same. -
Thermal Equilibrium State of the World Oceans
Thermal equilibrium state of the ocean Rui Xin Huang Department of Physical Oceanography Woods Hole Oceanographic Institution Woods Hole, MA 02543, USA April 24, 2010 Abstract The ocean is in a non-equilibrium state under the external forcing, such as the mechanical energy from wind stress and tidal dissipation, plus the huge amount of thermal energy from the air-sea interface and the freshwater flux associated with evaporation and precipitation. In the study of energetics of the oceanic circulation it is desirable to examine how much energy in the ocean is available. In order to calculate the so-called available energy, a reference state should be defined. One of such reference state is the thermal equilibrium state defined in this study. 1. Introduction Chemical potential is a part of the internal energy. Thermodynamics of a multiple component system can be established from the definition of specific entropy η . Two other crucial variables of a system, including temperature and specific chemical potential, can be defined as follows 1 ⎛⎞∂η ⎛⎞∂η = ⎜⎟, μi =−Tin⎜⎟, = 1,2,..., , (1) Te m ⎝⎠∂ vm, i ⎝⎠∂ i ev, where e is the specific internal energy, v is the specific volume, mi and μi are the mass fraction and chemical potential for the i-th component. For a multiple component system, the change in total chemical potential is the sum of each component, dc , where c is the mass fraction of each component. The ∑i μii i mass fractions satisfy the constraint c 1 . Thus, the mass fraction of water in sea ∑i i = water satisfies dc=− c , and the total chemical potential for sea water is wi∑iw≠ N −1 ∑()μμiwi− dc . -
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 - -
25 Kw Low-Temperature Stirling Engine for Heat Recovery, Solar, and Biomass Applications
25 kW Low-Temperature Stirling Engine for Heat Recovery, Solar, and Biomass Applications Lee SMITHa, Brian NUELa, Samuel P WEAVERa,*, Stefan BERKOWERa, Samuel C WEAVERb, Bill GROSSc aCool Energy, Inc, 5541 Central Avenue, Boulder CO 80301 bProton Power, Inc, 487 Sam Rayburn Parkway, Lenoir City TN 37771 cIdealab, 130 W. Union St, Pasadena CA 91103 *Corresponding author: [email protected] Keywords: Stirling engine, waste heat recovery, concentrating solar power, biomass power generation, low-temperature power generation, distributed generation ABSTRACT This paper covers the design, performance optimization, build, and test of a 25 kW Stirling engine that has demonstrated > 60% of the Carnot limit for thermal to electrical conversion efficiency at test conditions of 329 °C hot side temperature and 19 °C rejection temperature. These results were enabled by an engine design and construction that has minimal pressure drop in the gas flow path, thermal conduction losses that are limited by design, and which employs a novel rotary drive mechanism. Features of this engine design include high-surface- area heat exchangers, nitrogen as the working fluid, a single-acting alpha configuration, and a design target for operation between 150 °C and 400 °C. 1 1. INTRODUCTION Since 2006, Cool Energy, Inc. (CEI) has designed, fabricated, and tested five generations of low-temperature (150 °C to 400 °C) Stirling engines that drive internally integrated electric alternators. The fifth generation of engine built by Cool Energy is rated at 25 kW of electrical power output, and is trade-named the ThermoHeart® Engine. Sources of low-to-medium temperature thermal energy, such as internal combustion engine exhaust, industrial waste heat, flared gas, and small-scale solar heat, have relatively few methods available for conversion into more valuable electrical energy, and the thermal energy is usually wasted. -
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).