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Heat engine

From Wikipedia, the free encyclopedia
System that converts heat or thermal energy to mechanical work
See also:Thermodynamic cycle
Figure 1: Heat engine diagram

Thermodynamics
The classicalCarnot heat engine

Aheat engine is a system that transfersthermal energy to domechanical orelectrical work.[1][2] While originally conceived in the context of mechanical energy, the concept of the heatengine has been applied to various other kinds of energy, particularlyelectrical, since at least the late 19th century.[3][4] The heat engine does this by bringing aworking substance from a higher state temperature to a lower state temperature. A heat source generates thermal energy that brings the working substance to the higher temperature state. The working substance generates work in theworking body of the engine whiletransferring heat to the coldersink until it reaches a lower temperature state. During this process some of the thermal energy is converted intowork by exploiting the properties of the working substance. The working substance can be any system with a non-zeroheat capacity, but it usually is a gas or liquid. During this process, some heat is normally lost to the surroundings and is not converted to work. Also, some energy is unusable because offriction anddrag.

In general, an engine is anymachine that convertsenergy to mechanicalwork. Heat engines distinguish themselves from other types of engines by the fact that their efficiency is fundamentally limited byCarnot's theorem ofthermodynamics.[5] Although this efficiency limitation can be a drawback, an advantage of heat engines is that most forms of energy can be easily converted to heat by processes likeexothermic reactions (such as combustion),nuclear fission,absorption of light or energetic particles,friction,dissipation andresistance. Since the heat source that supplies thermal energy to the engine can thus be powered by virtually any kind of energy, heat engines cover a wide range of applications.

Heat engines are often confused with the cycles they attempt to implement. Typically, the term "engine" is used for a physical device and "cycle" for the models.

Overview

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Inthermodynamics, heat engines are often modeled using a standard engineering model such as theOtto cycle. The theoretical model can be refined and augmented with actual data from an operating engine, using tools such as anindicator diagram. Since very few actual implementations of heat engines exactly match their underlying thermodynamic cycles, one could say that a thermodynamic cycle is an ideal case of a mechanical engine. In any case, fully understanding an engine and its efficiency requires a good understanding of the (possibly simplified or idealised) theoretical model, the practical nuances of an actual mechanical engine and the discrepancies between the two.

In general terms, the larger the difference in temperature between the hot source and the cold sink, the larger is the potentialthermal efficiency of the cycle. On Earth, the cold side of any heat engine is limited to being close to the ambient temperature of the environment, or not much lower than 300kelvin, so most efforts to improve the thermodynamic efficiencies of various heat engines focus on increasing the temperature of the source, within material limits. The maximum theoretical efficiency of a heat engine (which no engine ever attains) is equal to the temperature difference between the hot and cold ends divided by the temperature at the hot end, each expressed inabsolute temperature.

The efficiency of various heat engines proposed or used today has a large range:

The efficiency of these processes is roughly proportional to the temperature drop across them. Significant energy may be consumed by auxiliary equipment, such as pumps, which effectively reduces efficiency.

Examples

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Although some cycles have a typical combustion location (internal or external), they can often be implemented with the other. For example,John Ericsson[9] developed an external heated engine running on a cycle very much like the earlierDiesel cycle. In addition, externally heated engines can often be implemented in open or closed cycles. In a closed cycle the working fluid is retained within the engine at the completion of the cycle whereas is an open cycle the working fluid is either exchanged with the environment together with the products of combustion in the case of the internal combustion engine or simply vented to the environment in the case of external combustion engines likesteam engines andturbines.

Everyday examples

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Everyday examples of heat engines include thethermal power station,internal combustion engine,firearms,refrigerators andheat pumps. Power stations are examples of heat engines run in a forward direction in which heat flows from a hot reservoir and flows into a cool reservoir to produce work as the desired product. Refrigerators,air conditioners and heat pumps are examples of heat engines that are run in reverse, i.e. they use work to take heat energy at a low temperature and raise its temperature in a more efficient way than the simple conversion of work into heat (either through friction or electrical resistance). Refrigerators remove heat from within a thermally sealed chamber at low temperature and vent waste heat at a higher temperature to the environment and heat pumps take heat from the low temperature environment and 'vent' it into a thermally sealed chamber (a house) at higher temperature.

In general heat engines exploit the thermal properties associated with the expansion and compression of gases according to thegas laws or the properties associated withphase changes between gas and liquid states.

Earth's heat engine

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Earth'satmosphere andhydrosphere—Earth's heat engine—are coupled processes that constantly even out solar heating imbalances through evaporation of surface water, convection, rainfall, winds and ocean circulation, when distributing heat around the globe.[10]

AHadley cell is an example of a heat engine. It involves the rising of warm and moist air in the earth's equatorial region and the descent of colder air in the subtropics creating a thermally driven direct circulation, with consequent net production of kinetic energy.[11]

Phase-change cycles

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Inphase change cycles and engines, theworking fluids are gases and liquids. The engine converts the working fluid from a gas to a liquid, from liquid to gas, or both, generating work from the fluid expansion or compression.

Gas-only cycles

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In these cycles and engines the working fluid is always a gas (i.e., there is no phase change):

Liquid-only cycles

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In these cycles and engines the working fluid are always like liquid:

Electron cycles

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Magnetic cycles

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Cycles used for refrigeration

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Main article:Refrigeration

A domesticrefrigerator is an example of aheat pump: a heat engine in reverse. Work is used to create a heat differential. Many cycles can run in reverse to move heat from the cold side to the hot side, making the cold side cooler and the hot side hotter. Internal combustion engine versions of these cycles are, by their nature, not reversible.

Refrigeration cycles include:

Evaporative heat engines

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The Barton evaporation engine is a heat engine based on a cycle producing power and cooled moist air from the evaporation of water into hot dry air.

Mesoscopic heat engines

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Mesoscopic heat engines are nanoscale devices that may serve the goal of processing heat fluxes and perform useful work at small scales. Potential applications include e.g. electric cooling devices. In such mesoscopic heat engines, work per cycle of operation fluctuates due to thermal noise. There is exact equality that relates average of exponents of work performed by any heat engine and the heat transfer from the hotter heat bath.[13] This relation transforms the Carnot's inequality into exact equality. This relation is also a Carnot cycle equality

Efficiency

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The efficiency of a heat engine relates how much useful work is output for a given amount of heat energy input.

From the laws ofthermodynamics, after a completed cycle:[14]

W+Q=ΔcycleU=0{\displaystyle W+Q=\Delta _{cycle}U=0}
and therefore
W=Q=(Qc+Qh){\displaystyle W=-Q=-(Q_{c}+Q_{h})}
where
W=PdV{\displaystyle W=-\oint PdV} is the net work extracted from the engine in one cycle. (It is negative, in theIUPAC convention, since work isdone by the engine.)
Qh>0{\displaystyle Q_{h}>0} is the heat energy taken from the high temperature heat source in the surroundings in one cycle. (It is positive since heat energy isadded to the engine.)
Qc=|Qc|<0{\displaystyle Q_{c}=-|Q_{c}|<0} is the waste heat given off by the engine to the cold temperature heat sink. (It is negative[14] since heat islost by the engine to the sink.)

In other words, a heat engine absorbs heat energy from the high temperature heat source, converting part of it to useful work and giving off the rest as waste heat to the cold temperature heat sink.

In general, the efficiency of a given heat transfer process is defined by the ratio of "what is taken out" to "what is put in". (For a refrigerator or heat pump, which can be considered as a heat engine run in reverse, this is thecoefficient of performance and it is ≥ 1.) In the case of an engine, one desires to extract work and has to put in heatQh{\displaystyle Q_{h}}, for instance fromcombustion of a fuel, so the engine efficiency is reasonably defined as

η=|W|Qh=Qh+QcQh=1+QcQh=1|Qc|Qh{\displaystyle \eta ={\frac {|W|}{Q_{h}}}={\frac {Q_{h}+Q_{c}}{Q_{h}}}=1+{\frac {Q_{c}}{Q_{h}}}=1-{\frac {|Q_{c}|}{Q_{h}}}}

The efficiency is less than 100% because of the waste heatQc<0{\displaystyle Q_{c}<0} unavoidably lost to the cold sink (and corresponding compression work put in) during the required recompression at the cold temperature before thepower stroke of the engine can occur again.

Thetheoretical maximum efficiency of any heat engine depends only on the temperatures it operates between. This efficiency is usually derived using an ideal imaginary heat engine such as theCarnot heat engine, although other engines using different cycles can also attain maximum efficiency. Mathematically, after a full cycle, the overall change of entropy is zero:

   ΔSh+ΔSc=ΔcycleS=0{\displaystyle \ \ \ \Delta S_{h}+\Delta S_{c}=\Delta _{cycle}S=0}

Note thatΔSh{\displaystyle \Delta S_{h}} is positive because isothermal expansion in the power stroke increases themultiplicity of the working fluid whileΔSc{\displaystyle \Delta S_{c}} is negative since recompression decreases the multiplicity. If the engine is ideal and runsreversibly,Qh=ThΔSh{\displaystyle Q_{h}=T_{h}\Delta S_{h}} andQc=TcΔSc{\displaystyle Q_{c}=T_{c}\Delta S_{c}}, and thus[15][14]

Qh/Th+Qc/Tc=0{\displaystyle Q_{h}/T_{h}+Q_{c}/T_{c}=0},

which givesQc/Qh=Tc/Th{\displaystyle Q_{c}/Q_{h}=-T_{c}/T_{h}} and thus the Carnot limit for heat-engine efficiency,

ηmax=1TcTh{\displaystyle \eta _{\text{max}}=1-{\frac {T_{c}}{T_{h}}}}

whereTh{\displaystyle T_{h}} is theabsolute temperature of the hot source andTc{\displaystyle T_{c}} that of the cold sink, usually measured inkelvins.

The reasoning behind this being themaximal efficiency goes as follows. It is first assumed that if a more efficient heat engine than a Carnot engine is possible, then it could be driven in reverse as a heat pump. Mathematical analysis can be used to show that this assumed combination would result in a net decrease inentropy. Since, by thesecond law of thermodynamics, this is statistically improbable to the point of exclusion, the Carnot efficiency is a theoretical upper bound on the reliable efficiency ofany thermodynamic cycle.

Empirically, no heat engine has ever been shown to run at a greater efficiency than a Carnot cycle heat engine.

Figure 2 and Figure 3 show variations on Carnot cycle efficiency with temperature. Figure 2 indicates how efficiency changes with an increase in the heat addition temperature for a constant compressor inlet temperature. Figure 3 indicates how the efficiency changes with an increase in the heat rejection temperature for a constant turbine inlet temperature.

Figure 2: Carnot cycle efficiency with changing heat addition temperature.
Figure 3: Carnot cycle efficiency with changing heat rejection temperature.

Endo-reversible heat-engines

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By its nature, any maximally efficient Carnot cycle must operate at aninfinitesimal temperature gradient; this is because any transfer of heat between two bodies of differing temperatures is irreversible, therefore the Carnot efficiency expression applies only to the infinitesimal limit. The major problem is that the objective of most heat-engines is to output power, and infinitesimal power is seldom desired.

A different measure of ideal heat-engine efficiency is given by considerations ofendoreversible thermodynamics, where the system is broken into reversible subsystems, but with non reversible interactions between them. A classical example is the Curzon–Ahlborn engine,[16] very similar to a Carnot engine, but where the thermal reservoirs at temperatureTh{\displaystyle T_{h}} andTc{\displaystyle T_{c}} are allowed to be different from the temperatures of the substance going through the reversible Carnot cycle:Th{\displaystyle T'_{h}} andTc{\displaystyle T'_{c}}. The heat transfers between the reservoirs and the substance are considered as conductive (and irreversible) in the formdQh,c/dt=α(Th,cTh,c){\displaystyle dQ_{h,c}/dt=\alpha (T_{h,c}-T'_{h,c})}. In this case, a tradeoff has to be made between power output and efficiency. If the engine is operated very slowly, the heat flux is low,TT{\displaystyle T\approx T'} and the classical Carnot result is found

η=1TcTh{\displaystyle \eta =1-{\frac {T_{c}}{T_{h}}}},

but at the price of a vanishing power output. If instead one chooses to operate the engine at its maximum output power, the efficiency becomes

η=1TcTh{\displaystyle \eta =1-{\sqrt {\frac {T_{c}}{T_{h}}}}} (Note:T in units ofK or°R)

This model does a better job of predicting how well real-world heat-engines can do (Callen 1985, see alsoendoreversible thermodynamics):

Efficiencies of power stations[16]
Power stationTc{\displaystyle T_{c}} (°C)Th{\displaystyle T_{h}} (°C)η{\displaystyle \eta } (Carnot)η{\displaystyle \eta } (Endoreversible)η{\displaystyle \eta } (Observed)
West Thurrock (UK)coal-fired power station255650.640.400.36
CANDU (Canada)nuclear power station253000.480.280.30
Larderello (Italy)geothermal power station802500.330.1780.16

As shown, the Curzon–Ahlborn efficiency much more closely models that observed.

History

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Main article:Timeline of heat engine technology
See also:History of the internal combustion engine andHistory of thermodynamics

Heat engines have been known since antiquity but were only made into useful devices at the time of the industrial revolution in the 18th century. They continue to be developed today.

Enhancements

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Engineers have studied the various heat-engine cycles to improve the amount of usable work they could extract from a given power source. The Carnot cycle limit cannot be reached with any gas-based cycle, but engineers have found at least two ways to bypass that limit and one way to get better efficiency without bending any rules:

  1. Increase the temperature difference in the heat engine. The simplest way to do this is to increase the hot side temperature, which is the approach used in modern combined-cyclegas turbines. Unfortunately, physical limits (such as the melting point of the materials used to build the engine) and environmental concerns regardingNOx production (if the heat source is combustion with ambient air) restrict the maximum temperature on workable heat-engines. Modern gas turbines run at temperatures as high as possible within the range of temperatures necessary to maintain acceptable NOx output[citation needed]. Another way of increasing efficiency is to lower the output temperature. One new method of doing so is to use mixed chemical working fluids, then exploit the changing behavior of the mixtures. One of the most famous is the so-calledKalina cycle, which uses a 70/30 mix ofammonia and water as its working fluid. This mixture allows the cycle to generate useful power at considerably lower temperatures than most other processes.
  2. Exploit thephysical properties of the working fluid. The most common such exploitation is the use of water above the critical point (supercritical water). The behavior of fluids above theircritical point changes radically, and with materials such as water andcarbon dioxide it is possible to exploit those changes in behavior to extract greater thermodynamic efficiency from the heat engine, even if it is using a fairly conventional Brayton or Rankine cycle. A newer and very promising material for such applications issupercritical CO2.SO2 andxenon have also been considered for such applications. Downsides include issues of corrosion and erosion, the different chemical behavior above and below the critical point, the needed high pressures and – in the case of sulfur dioxide and to a lesser extent carbon dioxide – toxicity. Among the mentioned compounds xenon is least suitable for use in a nuclear reactor due to the highneutron absorption cross section of almost allisotopes of xenon, whereas carbon dioxide and water can also double as aneutron moderator for a thermal spectrum reactor.
  3. Exploit thechemical properties of the working fluid. A fairly new and novel exploit is to use exotic working fluids with advantageous chemical properties. One such isnitrogen dioxide (NO2), a toxic component of smog, which has a naturaldimer as di-nitrogen tetraoxide (N2O4). At low temperature, the N2O4 is compressed and then heated. The increasing temperature causes each N2O4 to break apart into two NO2 molecules. This lowers the molecular weight of the working fluid, which drastically increases the efficiency of the cycle. Once the NO2 has expanded through the turbine, it is cooled by theheat sink, which makes it recombine into N2O4. This is then fed back by the compressor for another cycle. Such species asaluminium bromide (Al2Br6), NOCl, and Ga2I6 have all been investigated for such uses. To date, their drawbacks have not warranted their use, despite the efficiency gains that can be realized.[17]

Heat engine processes

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CycleCompression, 1→2Heat addition, 2→3Expansion, 3→4Heat rejection, 4→1Notes
Power cycles normally withexternal combustion - or heat pump cycles:
Bell ColemanadiabaticisobaricadiabaticisobaricA reversed Brayton cycle
CarnotisentropicisothermalisentropicisothermalCarnot heat engine
EricssonisothermalisobaricisothermalisobaricThe second Ericsson cycle from 1853
RankineadiabaticisobaricadiabaticisobaricSteam engines
Hygroscopicadiabaticisobaricadiabaticisobaric
Scuderiadiabaticvariable pressure
and volume
adiabaticisochoric
StirlingisothermalisochoricisothermalisochoricStirling engines
Mansonisothermalisochoricisothermalisochoric then adiabaticManson andManson-Guise engines
Stoddardadiabaticisobaricadiabaticisobaric
Power cycles normally withinternal combustion:
AtkinsonisentropicisochoricisentropicisochoricDiffers from Otto cycle in that V1 < V4.
BraytonadiabaticisobaricadiabaticisobaricRamjets,turbojets,-props, and-shafts. Originally developed for use in reciprocating engines. The external combustion version of this cycle is known as thefirst Ericsson cycle from 1833.
DieseladiabaticisobaricadiabaticisochoricDiesel engine
HumphreyisentropicisochoricisentropicisobaricShcramjets,pulse- andcontinuous detonation engines
LenoirisochoricadiabaticisobaricPulse jets. 1→2 accomplishes both the heat rejection and the compression. Originally developed for use in reciprocating engines.
OttoisentropicisochoricisentropicisochoricGasoline / petrol engines

Each process is one of the following:

  • isothermal (at constant temperature, maintained with heat added or removed from a heat source or sink)
  • isobaric (at constant pressure)
  • isometric/isochoric (at constant volume), also referred to as iso-volumetric
  • adiabatic (no heat is added or removed from the system during adiabatic process)
  • isentropic (reversible adiabatic process, no heat is added or removed during isentropic process)

See also

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References

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Wikimedia Commons has media related toHeat engines.
  1. ^Fundamentals of Classical Thermodynamics, 3rd ed. p. 159, (1985) by G. J. Van Wylen and R. E. Sonntag: "A heat engine may be defined as a device that operates in thermodynamic cycle and does a certain amount of net positive work as a result of heat transfer from a high-temperature body to a low-temperature body. Often the term heat engine is used in a broader sense to include all devices that produce work, either through heat transfer or combustion, even though the device does not operate in a thermodynamic cycle. The internal-combustion engine and the gas turbine are examples of such devices, and calling these heat engines is an acceptable use of the term."
  2. ^Mechanical efficiency of heat engines, p. 1 (2007) by James R. Senf: "Heat engines are made to provide mechanical energy from thermal energy."
  3. ^Kenelly, A.E. (December 1898)."Discussion of 'Thermo-electric and galvanic actions compared'".Journal of the Franklin Society.CXLVI: 442.
  4. ^Laurie, Arthur Pillans (17 January 1914)."Faraday society".The Electrical Review.72 (1834): 90. Retrieved11 February 2023.
  5. ^Thermal physics: entropy and free energies, by Joon Chang Lee (2002), Appendix A, p. 183: "A heat engine absorbs energy from a heat source and then converts it into work for us.... When the engine absorbs heat energy, the absorbed heat energy comes with entropy." (heat energyΔQ=TΔS{\displaystyle \Delta Q=T\Delta S}), "When the engine performs work, on the other hand, no entropy leaves the engine. This is problematic. We would like the engine to repeat the process again and again to provide us with a steady work source. ... to do so, the working substance inside the engine must return to its initial thermodynamic condition after a cycle, which requires to remove the remaining entropy. The engine can do this only in one way. It must let part of the absorbed heat energy leave without converting it into work. Therefore the engine cannot convert all of the input energy into work!"
  6. ^Eman, Mahmod Mohamed (June 2013)."Experimental Investigations on a Standing-Wave Thermoacoustic Engine".ResearchGate. Giza, Egypt:Cairo University. Retrieved21 January 2018.
  7. ^Where the Energy Goes: Gasoline Vehicles, US Dept of Energy
  8. ^Langston, Lee S."Efficiency by the Numbers". ASME.Archived from the original on 16 June 2009.
  9. ^"Ericsson's 1833 caloric engine".hotairengines.org.
  10. ^Lindsey, Rebecca (2009)."Climate and Earth's Energy Budget".NASA Earth Observatory.
  11. ^Junling Huang and Michael B. McElroy (2014)."Contributions of the Hadley and Ferrel Circulations to the Energetics of the Atmosphere over the Past 32 Years".Journal of Climate.27 (7):2656–2666.Bibcode:2014JCli...27.2656H.doi:10.1175/jcli-d-13-00538.1.S2CID 131132431.
  12. ^"Stirling's Dundee engine of 1841".hotairengines.org.
  13. ^N. A. Sinitsyn (2011). "Fluctuation Relation for Heat Engines".J. Phys. A: Math. Theor.44 (40) 405001.arXiv:1111.7014.Bibcode:2011JPhA...44N5001S.doi:10.1088/1751-8113/44/40/405001.S2CID 119261929.
  14. ^abcPlanck, M. (1945).Treatise on Thermodynamics. Dover Publications. p. § 90 & § 137.eqs.(39), (40), & (65).
  15. ^Fermi, E. (1956).Thermodynamics. Dover Publications (still in print). p. 48.eq.(64).
  16. ^abF. L. Curzon, B. Ahlborn (1975). "Efficiency of a Carnot Engine at Maximum Power Output".Am. J. Phys., Vol. 43, pp. 24.
  17. ^"Nuclear Reactors Concepts and Thermodynamic Cycles"(PDF). Archived fromthe original(PDF) on 18 March 2009. Retrieved22 March 2012.
  • Kroemer, Herbert; Kittel, Charles (1980).Thermal Physics (2nd ed.). W. H. Freeman Company.ISBN 0-7167-1088-9.
  • Callen, Herbert B. (1985).Thermodynamics and an Introduction to Thermostatistics (2nd ed.).John Wiley & Sons, Inc.ISBN 0-471-86256-8.
  • Robinson, Clark (1943).The Thermodynamics of Firearms. MaGraw-Hill Book Company Inc.
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