ENGINES REFRIGERATORS AND HEAT PUMPS This lecture highlights

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ENGINES, REFRIGERATORS, AND HEAT PUMPS This lecture highlights aspects in Chapters 9, 10, 11

ENGINES, REFRIGERATORS, AND HEAT PUMPS This lecture highlights aspects in Chapters 9, 10, 11 of Cengel and Boles. Every thermodynamic device has moving parts. To understand these movements, it is important that you watch some videos on the Internet. I will go through these slides in two 90 -minutes lectures. Zhigang Suo, Harvard University

How humans tell each other something? • • The thing itself Pictures Words Equations

How humans tell each other something? • • The thing itself Pictures Words Equations • • Language Books Movies The Internet 2

Thermodynamics = heat + motion Too many devices to classify neatly • Fuel (input):

Thermodynamics = heat + motion Too many devices to classify neatly • Fuel (input): biomass, fossil, solar thermal, geothermal, nuclear, electricity. • Application (output): mobile power plant (transpiration in air, land, sea), stationary power plant (electricity generation), refrigerator, heat pump. Power cycle, refrigeration cycle. • Working fluid: Gas cycle (air), vapor cycle (steam, phase change). • Fluid-solid coupling: piston engine (reciprocating, crankshaft), turbine engine (jet, compressor). • Site of burning: external combustion, internal combustion. 3

Plan • • • Internal combustion engines Gas turbines Stirling and Ericsson engines Vapor

Plan • • • Internal combustion engines Gas turbines Stirling and Ericsson engines Vapor power cycle Refrigeration cycle 4

Combustion engine burns to move BOILER STEAM WATER Fayette Internal Combustion Engiine I COMBUSTION

Combustion engine burns to move BOILER STEAM WATER Fayette Internal Combustion Engiine I COMBUSTION CHAMBER PISTON External combustion engine • • • Steam engine Stirling engine Ericsson engine Internal combustion engine (ICE) • • Otto (gasoline) engine Diesel engine Gas turbine Jet propulsion US Navy Training Manual, Basic Machines 5

Reciprocating engine also known as piston engine, converts linear motion to rotation CYLINDER PISTON

Reciprocating engine also known as piston engine, converts linear motion to rotation CYLINDER PISTON CONNECTING ROD CRANKSHAFT US Navy Training Manual, Basic Machines 6

fuel-air mixture entering cylinder air entering exhaust valve closed fuel-air mixture being compressed both

fuel-air mixture entering cylinder air entering exhaust valve closed fuel-air mixture being compressed both valves closed Fuel discharging intake from nozzle valve open piston moving down piston moving up valve tappet lifting valve cam lobe lifting valve tappet 1 cycle 4 strokes 2 revolutions INTAKE STROKE spark igniting mixture COMPRESSION STROKE both valves closed exhaust valve open intake valve closed Animated engines http: //www. animatedengines. com/ piston moving up piston moving down valve tappet lifting valve cam lobe lifting valve tappet 7 US Navy Training Manual, Basic Machines POWER STROKE EXHAUST STROKE

Spark-ignition engine (gasoline engine, petrol engine, Otto engine) 8

Spark-ignition engine (gasoline engine, petrol engine, Otto engine) 8

Air-standard assumptions 1. 2. 3. 4. Model the engine as a closed system, and

Air-standard assumptions 1. 2. 3. 4. Model the engine as a closed system, and the working fluid as air (an ideal gas). The cycle is internally reversible. Model combustion by adding heat from an external source Model exhaust by rejecting heat to an external sink 9

Cold air-standard assumption Model air as an ideal gas of constant specific heat at

Cold air-standard assumption Model air as an ideal gas of constant specific heat at room temperature (25°C). 2 independent variables to name all states of thermodynamic equilibrium 6 functions of state: PTvush 4 equations of state Gibbs equation 10

Thermal efficiency of Otto cycle Compression ratio: Conservation of energy: Isentropic processes: Thermal efficiency:

Thermal efficiency of Otto cycle Compression ratio: Conservation of energy: Isentropic processes: Thermal efficiency: wout win 11

Otto cycle represented in planes of different variables s 3 4 qin 2 qout

Otto cycle represented in planes of different variables s 3 4 qin 2 qout 1 v 12

Reciprocating engines of two types Spark-ignition engine (Otto, 1876) Compression-ignition engine (Diesel, 1892) https:

Reciprocating engines of two types Spark-ignition engine (Otto, 1876) Compression-ignition engine (Diesel, 1892) https: //ccrc. kaust. edu. sa/pages/HCCI. aspx 13

Compression-ignition engine (Diesel engine) compression ratio: cut-off ratio: Conservation of energy: Isentropic processes Thermal

Compression-ignition engine (Diesel engine) compression ratio: cut-off ratio: Conservation of energy: Isentropic processes Thermal efficiency: 14

Plan • • • Internal combustion engines Gas turbines Stirling and Ericsson engines Vapor

Plan • • • Internal combustion engines Gas turbines Stirling and Ericsson engines Vapor power cycle Refrigeration 15

Gas turbine (Brayton cycle) 4 steady-flow components: isobaric and isentropic P qin 3 2

Gas turbine (Brayton cycle) 4 steady-flow components: isobaric and isentropic P qin 3 2 1 4 qout 16 s

Thermal efficiency of Brayton cycle Definition of pressure ratio: Conservation of energy: Isentropic processes:

Thermal efficiency of Brayton cycle Definition of pressure ratio: Conservation of energy: Isentropic processes: Thermal efficiency: 17

Brayton cycle has large back work ratio win wout 18

Brayton cycle has large back work ratio win wout 18

Intercooling, reheating, regeneration 19

Intercooling, reheating, regeneration 19

Gas turbine for jet propulsion Thousands of years of history Who invented this? Hero

Gas turbine for jet propulsion Thousands of years of history Who invented this? Hero of Alexandria (first century AD) http: //www. techknow. org. uk/wiki/index. php? title=File: Hero_4. jpg Frank Whittle (UK), Hans von Ohain (Germany) (during World War II) 20

Gas turbine for jet propulsion 6 steady-flow components Propulsive force: Propulsive power: Propulsive efficiency:

Gas turbine for jet propulsion 6 steady-flow components Propulsive force: Propulsive power: Propulsive efficiency: 21

http: //www. ae. utexas. edu/~plv 955/class/propulsion/Cp_air. GIF 22

http: //www. ae. utexas. edu/~plv 955/class/propulsion/Cp_air. GIF 22

Air as an ideal gas of variable specific heat See section 7. 9 for

Air as an ideal gas of variable specific heat See section 7. 9 for the use of this table 23

Plan • • • Internal combustion engines Gas turbines Stirling and Ericsson engines Vapor

Plan • • • Internal combustion engines Gas turbines Stirling and Ericsson engines Vapor power cycle Refrigeration cycle 24

Displacer-type Stirling engine https: //www. stirlingengine. com/faq/ 25

Displacer-type Stirling engine https: //www. stirlingengine. com/faq/ 25

Stirling engine and regenerator (1816) reversible cycle between two fixed temperatures, having the Carnot

Stirling engine and regenerator (1816) reversible cycle between two fixed temperatures, having the Carnot efficiency 26 https: //people. ok. ubc. ca/jbobowsk/Stirling/how. html

Stirling vs. Carnot for given limits of volume, pressure, and temperature • On PV

Stirling vs. Carnot for given limits of volume, pressure, and temperature • On PV plane, the black area represents the Carnot cycle, and shaded areas represent addition work done by the Stirling cycle. • On TS plane, the black area represents the Carnot cycle, and the shaded areas represent additional heat taken in by the Stirling cycle. • The Stirling cycle and the Carnot cycle have the same thermal efficiency. • The Stirling cycle take in more heat and give more work than the Carnot cycle. Walker, Stirling Engine, 1980. 27

Work out by Stirling cycle Specific work Specific gas constant Gas Formula Air R

Work out by Stirling cycle Specific work Specific gas constant Gas Formula Air R (k. J/kg. K) 0. 2870 Steam H 2 O 0. 4615 Ammonia NH 3 0. 4882 Hydrogen H 2 4. 124 Helium He 2. 077 28

Ericsson engine with regenerator (1853) reversible cycle between two fixed temperatures, having the Carnot

Ericsson engine with regenerator (1853) reversible cycle between two fixed temperatures, having the Carnot efficiency 29

Plan • • • Internal combustion engines Gas turbines Stirling and Ericsson engines Vapor

Plan • • • Internal combustion engines Gas turbines Stirling and Ericsson engines Vapor power cycle Refrigeration cycle 30

Coal power station coverts coal to electricity 31

Coal power station coverts coal to electricity 31

Brayton Point Power Station Sommerset, Massachusetts Mount Hope Bay http: //www. clf. org/blog/clean-energy-climate-change/brayton-point-retirement-means-game-coal-new-england/ 32

Brayton Point Power Station Sommerset, Massachusetts Mount Hope Bay http: //www. clf. org/blog/clean-energy-climate-change/brayton-point-retirement-means-game-coal-new-england/ 32

Nuclear power station converts uranium to electricity Animation https: //www. awesomestories. com/images/user/be 4285 df

Nuclear power station converts uranium to electricity Animation https: //www. awesomestories. com/images/user/be 4285 df 4 b. gif 33 http: //www. nuclear-power. net/nuclear-power-plant/

Nine Mile Point Nuclear Power Plant, New York Lake Ontario Cooling tower 34

Nine Mile Point Nuclear Power Plant, New York Lake Ontario Cooling tower 34

Why water? Why steam? • • Water is cheap. Water flows! Water is a

Why water? Why steam? • • Water is cheap. Water flows! Water is a liquid at the temperature of heat sink (rivers, lakes, . . . ). Vaporization changes specific volume greatly: a lot of work at relatively low pressure. https: //www. ohio. edu/mechanical/thermo 35

Rankine cycle 4 steady-flow components: isobaric and isentropic wpump, in = h 2 -

Rankine cycle 4 steady-flow components: isobaric and isentropic wpump, in = h 2 - h 1 qboiler, in = h 3 - h 2 wturbine, out = h 3 – h 4 qcondenser, out = h 4 – h 1 P 2 qboiler, in 3 wturbine, out wpumo, in 1 qcondenser, out 4 s 36

Rankin cycle has small back work ratio 37

Rankin cycle has small back work ratio 37

Carnot cycle is unsuitable as vapor power cycle Issues with the in-dome Carnot cycle

Carnot cycle is unsuitable as vapor power cycle Issues with the in-dome Carnot cycle Process 1 -2 limits the maximum temperature below the critical point (374°C for water) Process 2 -3. The turbine cannot handle steam with a high moisture content because of the impingement of liquid droplets on the turbine blades causing erosion and wear. Process 4 -1. It is not practical to design a compressor that handles two phases. Issues with supercritical Carnot cycle Process 1 -2 requires isothermal heat transfer at variable pressures. Process 4 -1 requires isentropic compression to extremely high pressures. 38

Cogeneration 39

Cogeneration 39

Plan • • • Internal combustion engines Gas turbines Stirling and Ericsson engines Vapor

Plan • • • Internal combustion engines Gas turbines Stirling and Ericsson engines Vapor power cycle Refrigeration cycle 40

Refrigerator and heat pump 4 steady-flow components 41

Refrigerator and heat pump 4 steady-flow components 41

Selecting Refrigerant 1. 2. 3. 4. 5. 6. • • • Large enthalpy of

Selecting Refrigerant 1. 2. 3. 4. 5. 6. • • • Large enthalpy of vaporization Sufficiently low freezing temperature Sufficiently high critical temperature Low condensing pressure Do no harm: non-toxic, non-corrosive, non-flammable, environmentally-friendly Low cost R-717 (Ammonia, NH 3) used in industrial and heavycommercial sectors. Toxic. R-12 (Freon 12, CCl 2 F 2). Damage ozone layer. Banned. R-134 a (HFC 134 a, CH 2 FCF 3) used in domestic refrigerators, as well as automotive air conditioners. 42

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Summary • Engine converts fuel to motion. • Refrigerator and heat pump use work

Summary • Engine converts fuel to motion. • Refrigerator and heat pump use work to pump heat from a place of low temperature to a place of high temperature. • Many ideal cycles are internally reversible, but externally irreversible. • Stirling and Ericsson cycles are internally and externally reversible, so they have the same thermal efficiency as the Carnot cycle. • Use ideal-gas model to analyze gas as working fluid. • Use property table to analyze vapor as working fluid. • Model piston engine as a closed system (Otto, Diesel, Stirling, Ericsson). • Model turbine (or compressor) device as steady-flow components in series (Brayton cycle, Rankine cycle, refrigeration cycle). 45