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Second Law of
Thermodynamics
Limitations of First Law of Thermodynamics
โ€ข Heat flows from a system of higher temperature to a system of lower temperature and never from
lower temperature system to higher temperature system
โ€ข From first law of thermodynamics, โ€œHeat lost and heat gain must be equal in both the
processesโ€
โ€ข According to first law, it is assumed that the energy transfer can take place in either
direction, it does not specify the direction of energy transfer
Heat is transferred from hotter side to the colder side of the rod
But never from colder to hotter side by itself by itself
hotter side colder side
Why does energy
travel always
from higher value
to lower value?
โ€ข All work can be converted into heat but all heat cannot be converted into work
- For example: In internal combustion engine, all heat generated from combustion of fuel
is not converted into work, but a portion of input heat has to be rejected
to exhaust gases, oil, cooling water
Image source: http://teamspeed.com
QExhaust
QFuel
QFriction
QCooling Water
QOil
- Example : In power plants, all heat generated from combustion of coal is not converted
into work, but a portion of input heat has to be rejected in the condenser
Image source: http://google.com
What First Law of Thermodynamics Tells Us โ€“ Interpretations
First law of thermodynamics is a necessary condition but not sufficient condition for a
process to take place
First law of thermodynamics states โ€œwork can be converted into heat and heat into workโ€
First law makes no distinction between forms of energy, silent about the possibility of
energy conversion
First law is not sufficient to predict weather a system will or will not under go a particular
change
What Second Law of Thermodynamics Tells Us โ€“ Interpretations
Second law of thermodynamics indicates that, โ€œall heat cannot be converted into workโ€
According to second law of thermodynamics, โ€œheat will only be transferred from high
temperature to lower temperature and not vice versaโ€œ
โ€œFirst law of thermodynamicsโ€, is a quantitative statement and โ€œSecond law of
thermodynamicsโ€, is a qualitative statement
Second law states that whether it is possible for energy transfer to proceed along a
particular direction or not
A cycle can only occur if it satisfies both the first law and second law of thermodynamics
Energy Reservoirs
MER
WT
Wnet
Boiler
Turbine
Condenser
Pump
TERH
(SOURCE)
TERL
(SINK)
Wp
Q1
Q2
Thermal Energy reservoirs (TER): is defined as a large
body of infinite heat capacity, which is capable of
absorbing or rejecting an unlimited quantity of heat
without suffering appreciable change in its
thermodynamic coordinates. All process are quasi-static
Constant Temperature
Constant Temperature
Mechanical Energy reservoirs (MER): is a large body
enclosed by an adiabatic impermeable wall capable of
storing work as kinetic energy or potential energy. All
process are quasi-static
Heat Engine
โ€ข Heat Engine is a device which working in a cycle converts energy in form of heat into work
- Heat engines convert heat to work
โ€ข There are several types of heat engines, but they are characterized by the following:
- They all receive heat from a high-temperature source (oil furnace, nuclear reactor, etc.)
- They convert part of this heat to work
- They reject the remaining waste heat to a low-temperature sink
- They operate in a cycle
Heat Engine
Boiler
Pump
Condenser
QB / Q1
WT
WP
WT - WP
Net work output of the
system during cyclic process
Turbine
Boiler
Turbine
Condenser
Pump
Water
Steam
Water Steam
Water
Heat Source: Furnace
Heat Sink: Lake/River
QC / Q2
QB โ€“ QC = WT - WP
๐›ˆ =	
"#$%#$	'()*
+,%#$	-./$
=	
WT โˆ’ WP
Q1
๐›ˆ = 30% - 40%
=		
Q1 โ€“ Q2
Q1
Q2 = 60%- 70% Q1
=	1 -
Q2
		Q1
T1 = 500โˆ˜C
W
Q โ€“ W = Q2
Q1
T2 = 20โˆ˜C
Source
Sink
(atmosphere)
Heat
Engine
Q. Is it possible to save the rejected heat QC in a power cycle?
Answer: NO, because without the cooling in condenser the cycle cannot be completed
- Every heat engine must waste some energy by transferring it to a low-temperature
reservoir in order to complete the cycle, even in idealized cycle
๐‘ญ๐’“๐’๐’Ž	๐’‡๐’Š๐’“๐’”๐’•	๐‘ณ๐’‚๐’˜	๐’๐’‡	๐‘ป๐’‰๐’†๐’“๐’Ž๐’๐’…๐’š๐’๐’‚๐’Ž๐’Š๐’„๐’”	๐’‡๐’๐’“	๐’‚	๐’„๐’š๐’„๐’๐’Š๐’„	๐’‘๐’“๐’๐’„๐’†๐’”๐’”
โˆฎ๐๐‘ธ = โˆฎ๐๐‘พ
Q1 โ€“ Q2 = WT - WP
Refrigerator
Throttle
Compressor
QR/Q2
Refrigerator
W
โ€ข In nature, heat flows from high-temperature regions to low-temperature ones
โ€ข The reverse process, however, cannot occur by itself
โ€ข The transfer of heat from a low- temperature region to a high-temperature one requires special
devices called refrigerators
Refrigerators are cyclic devices, and the working fluids used in the cycles are called refrigerant
Condenser
QC/Q1
Win
Cold Environment
Warm House
Objectives of Refrigerator & Heat Pump
Heat
Pump
Win
Q1
Q2
Refrigerated Space
Warm Environment
Refrig
erator
Desired Output
Condenser
Evaporator
Expansion
Valve
Compressor Wc
T < T atm.
T = T atm.
Desired Output
T = T atm.
T > T atm.
Q1
Q2
๐‘ญ๐’“๐’๐’Ž	๐’‡๐’Š๐’“๐’”๐’•	๐‘ณ๐’‚๐’˜	๐’๐’‡	๐‘ป๐’‰๐’†๐’“๐’Ž๐’๐’…๐’š๐’๐’‚๐’Ž๐’Š๐’„๐’”	๐’‡๐’๐’“	๐’‚	๐’„๐’š๐’„๐’๐’Š๐’„	๐’‘๐’“๐’๐’„๐’†๐’”๐’”
โˆฎ๐๐‘ธ = โˆฎ๐๐‘พ
W = Qc - QR
= Q1 - Q2
COPR =	
๐‘ฏ๐’†๐’‚๐’•	๐‘น๐’†๐’Ž๐’๐’—๐’†๐’…	๐’ƒ๐’š	๐’•๐’‰๐’†	๐‘น๐’†๐’‡๐’“๐’Š๐’ˆ๐’†๐’“๐’‚๐’•๐’๐’“
๐‘พ๐’๐’“๐’Œ	๐‘บ๐’–๐’‘๐’‘๐’๐’Š๐’†๐’…	
=		
Q2
W
=		
QR
QC โˆ’ QR
โ€ข The performance of refrigerators and heat pumps is
expressed in terms of the coefficient of performance (COP)
COPR =	
๐‘ฉ๐’†๐’๐’Š๐’‡๐’•
๐‘ช๐’๐’”๐’•	
W
T2 = - 4โˆ˜C
T1 = 35โˆ˜C
Refrigerator
Heat
Engine
Sink
(atmosphere)
Q1
=		
Q2
Q1 โˆ’ Q2
In a refrigerator, the desired effect is the amount of heat
removed Q2 from the space being heated
Q2
W
Q1
Q2
T2 = 4โˆ˜C
T1 = 25โˆ˜C
Heated Space
Atmoshpere
Heat Pump
Heat
Pump
โ€ข Heat pumps transfer heat from a low-temperature medium to a high-temperature
โ€ข Refrigerators and heat pumps are essentially the same devices; they differ in their objectives
only
โ€ข Refrigerator is to maintain the refrigerated space at a low temperature
โ€ข On the other hand, a heat pump absorbs heat from a low-temperature source and supplies the
heat to a warmer medium
In a heat Pump, the desired effect is the amount of heat supplied
Q1 to the space being heated
COPHP =		
๐‘ฏ๐’†๐’‚๐’•	๐‘บ๐’–๐’‘๐’‘๐’๐’Š๐’†๐’…		๐’ƒ๐’š	๐’•๐’‰๐’†	๐‘ฏ๐’†๐’‚๐’•	๐‘ท๐’–๐’Ž๐’‘
๐‘พ๐’๐’“๐’Œ	๐‘บ๐’–๐’‘๐’‘๐’๐’Š๐’†๐’…	
=		
Q1
W
=		
Q1
Q1 โˆ’ Q2
=	1 +
Q2
Q1 โˆ’ Q2
=	1 + COPR
The COP of a heat pump operating as a heat pump is higher that
the COP of the same machine operating as a refrigerator by unity
โ€ข The performance of air conditioners and heat pumps is often expressed in terms of the energy
efficiency ratio (EER) or seasonal energy efficiency ratio (SEER) determined by following
certain testing standards
- SEER : is the ratio the total amount of heat removed by an air conditioner or heat pump during a
normal cooling season (in Btu) to the total amount of electricity consumed (in watt-hours, Wh), and
it is a measure of seasonal performance of cooling equipment
- EER : is a measure of the instantaneous energy efficiency, and is defined as the ratio of the rate
of heat removal from the cooled space by the cooling equipment to the rate of electricity
consumption in steady operation
โ€ข Therefore, both EER and SEER have the unit Btu/Wh
- 1 kWh = 3.412 Btu (1 Wh = 3.412 Btu, a device that removes 1 kWh of heat from the cooled
space for each kWh of electricity it consumes (COP = 1) will have an EER of 3.412)
- Therefore, the relation between EER and COP, EER = 3.412.COPR
Performance of Refrigerators, Air-Conditioners, and Heat Pumps
The heat transfer rate is often given in terms of tones of heating or cooling
One ton = 12,000 Btu = 211 kJ/min
โ€ข Air conditioners or heat pumps SEER: 13 to 21, which correspond to COP values of 3.8 to 6.2.
- Most air conditioners have an EER between 8 to 12 (COP of 2.3 to 3.5)
โ€ข Best performance is achieved using units equipped with variable-speed drives (also called
inverters)
- Variable-speed compressors and fans allow the unit to operate at maximum efficiency for varying
heating/cooling needs and weather conditions as determined by a microprocessor
- In the air-conditioning mode, for example, they operate at higher speeds on hot days and at lower speeds
on cooler days, enhancing both efficiency and comfort
โ€ข The EER or COP of a refrigerator decreases with decreasing refrigeration temperature
- Therefore, it is not economical to refrigerate to a lower temperature than needed
โ€ข The COPs of refrigerators (range): 2.6 to 3.0 for cutting and preparation rooms
2.3 to 2.6 for meat, deli, dairy, and produce
1.2 to 1.5 for frozen foods
1.0 to 1.2 for ice cream units
Note: COP of freezers is about half of the COP of meat refrigerators
- It costs twice as much to cool the meat products with refrigerated air that is cold
enough to cool frozen foods
- It is good energy conservation practice to use separate refrigeration systems to meet
different refrigeration needs
W
Heat
Engine
Second Law of Thermodynamics: Kelvin Plankโ€™s Statement
- It is impossible for any device that operates on a cycle to receive
heat from a single reservoir and produce a net amount of work
- In other words, no heat engine can have a thermal efficiency of
100%
Source (TH)
A heat engine that violates the Kelvin-Planck
statement of the second law cannot be built
Thermal efficiency of 100%
Qin
Wnet = Qin
Qout = 0
โ€œIt is impossible for any system to operate in a thermodynamic cycle and deliver a net amount of
work to its surroundings while receiving an energy transfer by heat from a single thermal reservoirโ€
W
Heat
Pump
Second Law of Thermodynamics: Clausius Statement
- Heat cannot flow from itself from a system low temperature to a
system at high temperature.
- COP = Q/W = Q/0 = โˆž ( a condition not possible)
- The only alternative is that some external work must be
supplied to the machine
System (T1)
A heat engine that violates the Kelvin-Planck
statement of the second law cannot be built
Qin
Q2
โ€œHeat cannot, of itself, pass from a colder to a hotter body โ€
โ€œIt is impossible for a self acting machine working in a cyclic process unaided by any external
agency, to convey heat from a body at a lower temperature to a body at a higher temperatureโ€
System (T2)
Perpetual Motion Machine of the Second Kind (PMMK2)
โ€ข Without violating the first law, a machine can be imagined which would continuously absorb heat
from a single thermal reservoir and would convert this heat completely into work
- The efficiency of such a machine would be 100%
- This machine is called the perpetual motion machine of the second kind (PMM2)
W
Heat
Engine
Source (TH)
Qin
Wnet = Qin
Qout = 0
When the thermal energy is equivalent to the work done, this does not violate the law of
conservation of energy. However it does violate the more subtle second law of thermodynamics
Carnot Cycle
โ€ข The cycle was first suggested by Sadi Carnot, in 1824, which works on reversible cycle
โ€ข Any fluid may be used to operate the Carnot cycle, which is performed in an engine cylinder the
head of which is supposed alternatively to be perfect conductor or a perfect insulator of a heat
โ€ข Heat is caused to flow into the cylinder by the application of high temperature energy source to
the cylinder head during expansion, and to flow from the cylinder by the application of a lower
temperature energy source to the head during compression
Source, T1
Sink, T2
Working
Substance
Adiabatic
Cover
Diathermic
Cover
Cylinder Head
Heat Insulation
Heat Insulation
Piston
Piston motion
The assumptions made for describing the working of the Carnot engine are as follows :
1. The piston moving in a cylinder does not develop any friction during motion
2. The walls of piston and cylinder are considered as perfect insulators of heat
3. The cylinder head is so arranged that it can be a perfect heat conductor or perfect heat insulator
4. The transfer of heat does not affect the temperature of source or sink
5. Working medium is a perfect gas and has constant specific heat
6. Compression and expansion are reversible
Diathermic
Cover
Working
Substance
Adiabatic
Cover
Piston motion
Stage 1 โ€“ Isothermal Expansion
(Process 1-2)
- Hot energy source at temperature T1 is applied
- Heat Q1 is taken in whilst the fluid expands
isothermally and reversiblyat constant high
temperature T1
Q1
Stage 2 โ€“ Adiabatic Expansion
(Process 2-3)
- The cylinder becomes a perfect insulator so
that no heat flow takes place
- The fluid expands adiabatically and reversibly
whilst temperature falls from T1 to T2
Source,
T
1
Sink,
T
2
Working
Substance
Diathermic
Cover
Adiabatic
Cover
Stage 3 โ€“ Isothermal Compression
(Process 3-4)
- Cold energy source at temperature T2 is applied
- Heat Q2 flows from the fluid whilst it is
compressed isothermally and reversibly at
constant lower temperature T2
Q2
Stage 4 - Adiabatic Compression
(Process 4-1)
- Cylinder head becomes a perfect insulator so
that no heat flow occurs
- The compression is continued adiabatically and
reversibly during which temperature is raised
from T2 to T1
Q1 = W1-2 = P1 V1 In
	๐‘ฝ๐Ÿ		
๐‘ฝ๐Ÿ
Q1 = W1-2 = mRT1 In
	๐‘ฝ๐Ÿ		
๐‘ฝ๐Ÿ
Q2 = W3-4 = - P3 V3 In
	๐‘ฝ๐Ÿ’		
๐‘ฝ๐Ÿ‘
Q2 = W3-4 = mRT2 In
	๐‘ฝ๐Ÿ‘		
๐‘ฝ๐Ÿ’
Heat Rejected
Heat Added
๐œ‚ =	1 -
Q2
		Q1
๐œ‚ =
	๐‘ต๐’†๐’•	๐‘พ๐’๐’“๐’Œ	๐‘ถ๐’–๐’•๐’‘๐’–๐’•
		
๐‘ฏ๐’†๐’‚๐’•	๐‘ฐ๐’๐’‘๐’–๐’•
=
	๐‘พ๐’๐’†๐’•		
๐‘ธ๐Ÿ
๐‘ญ๐’“๐’๐’Ž	๐’‡๐’Š๐’“๐’”๐’•	๐‘ณ๐’‚๐’˜	๐’๐’‡	๐‘ป๐’‰๐’†๐’“๐’Ž๐’๐’…๐’š๐’๐’‚๐’Ž๐’Š๐’„๐’”	๐’‡๐’๐’“	๐’‚	๐’„๐’š๐’„๐’๐’Š๐’„	๐’‘๐’“๐’๐’„๐’†๐’”๐’”
โˆฎ๐๐‘ธ = โˆฎ๐๐‘พ							๐’๐’“										๐‘พ๐’๐’†๐’• = ๐‘ธ๐Ÿ	 โˆ’ ๐‘ธ๐Ÿ
๐œ‚ =	1 -
T2
T1
(V2/V1) = (V3/V4)
P2 V2
๐›พ = P3 V3
๐›พ
T1 V2
(๐›พ- 1)	= T2 V3
(๐›พ- 1)	
P4 V4
๐›พ = P1 V1
๐›พ
PV= nRT ; PV/T = nR =C
P2V2/T1 = P3V3/T2
P4V4/T2 = P1V1/T1
1
2
3
4
T1 V1
(๐›พ- 1)	= T2 V4
(๐›พ- 1)	
5
6
Dividing 1/3 and 2/4
Dividing 5/6
=	1 -
Q2
		Q1
Temperature
Entropy
Q1
Q2
T2
T1
4 3
2
1
Area of the rectangle a-b-c-d represents work output per cycle and it equals
Q1 โ€“ Q2 = (T1 โ€“ T2).dS
Isotherms
Frictionless
Adiabats
S1 =S4 S2 = S3
Efficiency of a Reversible Heat Engine
โ€ข From the above expression, it may be noted that as T2 decreases and T1 increases, efficiency of
the reversible cycle increases
โ€ข Since ๐œ‚ is always less than unity, T2 is always greater than zero and positive (+ ve)
Carnot Heat Pump
โ€ข An engine, which consists entirely of reversible processes, can operate in the reverse direction,
so that it follows the cycle as shown and operates as a heat pump
Work (W) will be needed
to drive the pump
The enclosed area represents this work which is exactly equal to that flowing from it when used as engine
(process 4-3)
Q2 is being taken in at the lower
temperature T2 during the
isothermal expansion
(process 2-1)
Q1 is being rejected at
the upper temperature T1
Q1
Q2
1. It is impossible to perform a frictionless process
2. It is impossible to transfer the heat without temperature potential
3. Isothermal process can be achieved only if the piston moves very slowly to allow heat transfer so
that the temperature remains constant
- Adiabatic process can be achieved only if the piston moves as fast as possible so that the heat
transfer is negligible due to very short time available
- The isothermal and adiabatic processes take place during the same stroke therefore the piston
has to move very slowly for part of the stroke and it has to move very fast during remaining
stroke
- This variation of motion of the piston during the same stroke is not possible
Carnot cycle cannot be performed in practice because of the following reasons
Equivalence of Clausius Statement to the Kelvin-Planck Statement
W = Q1 โ€“ Q2; Since, there is no heat interaction with the low temperature, it can be eliminated
Q1
Q2
Low Temperature Reservoir T2
Heat
Engine
Net Work
(W) = Q1 โ€“ Q2
High Temperature Reservoir T1
Heat
Pump
Q1
Q2
A heat pump which requires no
work and transfers an amount of
Q2 from a low temperature to a
higher temperature reservoir
(violation of the Clausius statement)
The combined system of the heat engine and heat pump acts then like a heat engine exchanging heat
with a single reservoir, which is the violation of the Kelvin-Planck statement
Heat rejected
Q1 > Q2
The Kelvinโ€™s and Clausiusโ€™s statements of the second law are equivalent. i.e. if we violate Kelvinโ€™s statement, then
we will automatically violate the Clausiusโ€™s statement of the second law (and vice-versa)
No Work
Q1
Q2 = 0
Low Temperature Reservoir T2
Heat
Engine
W = Q1
High Temperature Reservoir T1
Heat
Pump
Q1
Q2
A heat engine which converts all
heat to work, without rejecting
heat to low temperature
(Violation of the Kelvin Plank statement)
The combined system constitutes a device which transfers heat from low temperature reservoir to
high temperature without any work from external agency, which is the violation of the Clausius
statement
Q1 > Q2
Violation of Kelvin โ€“ Plank Statement leads to violation of Clausiusโ€™s statements
W = Q1
Can you beat Second Law
Can you cool your
room by leaving the
refrigerator door
open ?
The heat removed from the interior of the refrigerator is
deposited back into the kitchen by the coils on the back!
Second Law of Thermodynamics says that work is needed to
move the heat from cold to hot, so the actual amount of heat
added to the kitchen is MORE than the amount removed from
the refrigerator
โ€ข The second corollary to the Kelvin-Planck statement holds that โ€œAll reversible engines operating
between the same thermal reservoirs have the same ๐œ‚โ€
- This is independent of any details of the cycle or the materials involved
- The thermal efficiency, ๐œ‚, should depend only on the character of the reservoirs involved
Thermodynamic Temperature
Consider a case of reversible heat engine operating between two reservoirs
- Its thermal efficiency is given by ๐œ‚ =	
Q1 โˆ’ Q2
Q1
= 1 -
Q2
Q1
โ€ข The temperature of a reservoir remains uniform and fixed irrespective of heat transfer
- This means that reservoir has only one property defining its state and the heat transfer from a reservoir
is some function of that property, temperature.
Thus Q = ฯ† (K), where K is the temperature of reservoir
Q1
Q2
=
ฯ†(K1)
ฯ†(K2)
=>
Q1
Q2
=
T1
T2
; T1 and T2 are the thermodynamic temperatures of the reservoirs
Zero thermodynamic temperature (that temperature to which T2 tends, as the heat transfer Q2 tends to zero)
has never been attained and one form of third law of thermodynamics is the statement :
โ€˜โ€˜The temperature of a system cannot be reduced to zero in a finite number of processesโ€
The amounts of heat rejected by engines B and C must
be the same since engines A and B can be combined into
one reversible engine operating between the same
reservoirs as engine C and thus the combined engine will
have the same efficiency as engine C.
Since the heat input to engine C is the same as the heat
input to the combined engines A and B, both systems
must reject the same amount of heat
โ€ข After establishing the concept of a zero thermodynamic temperature, a reference reservoir is
chosen and assigned a numerical value of temperature
โ€ข Any other thermodynamic temperature may now be defined in terms of reference value and the
heat transfers that would occur with reversible engine,
T = Tref.
Q
Qref.
โ€ข Let us make an arbitrary choice to avoid ratios. We take, for convenience, the temperature of the
triple point of water to be 273.15 K. Thus for any system, the local T is
T = 273.3.
Q
Qref.
This implies we can connect our heat engine to a reservoir maintained at the triple point temperature
of water, and measure the associated Qs for the heat engine
โ€ข We would like to drive our efficiency to be as close to unity as possible, nature limits us
โ€ข Generally, we have little to no control over the environmental temperature TL, so it is a lower bound, usually
around TL โˆผ 300 K. And material properties for engines limit TH . For many metals, TH โˆผ 1500 K is approaching
values where material strength is lost
โ€ข So a practical upper bound based on these numbers tell us
โ€ข ฮทโˆผ 1 โˆ’ (300K)/(1500K) = 0.8 is may be the most we can expect. We plot ฮท as a function of TH for fixed TL =
300 K For real systems, with irreversible features, the values are much lower
โ€ข The determination of thermodynamic temperature cannot be made in this way as it is not possible
to build a reversible engine
โ€ข Temperatures are determined by the application of thermodynamic relations to other
measurements
โ€ข The SI unit of thermodynamic temperature is the kelvin (K)
โ€ข The relation between thermodynamic temperature and Celsius scale
- Thermodynamic temperature = Celsius temperature + 273.15ยฐ
- The kelvin unit of thermodynamic temperature is the fraction 1 temperature of โ€˜Triple pointโ€™ of
water
Carnot Theorem
โ€œIt states that of all engines operating between a given constant temperature source and a
given constant temperature sink, none has a higher efficiency than a reversible engineโ€
Let HEA be any heat engine and HEB be any reversible heat engine
We have to prove that efficiency of HEB is more than that of HEA
Let us assume that ๐œ‚A > ๐œ‚B
Q1A = Q1B = Q1
๐œ‚A = ๐œ‚B
๐‘พ๐‘จ
๐‘ธ๐Ÿ๐‘จ
=
๐‘พ๐‘ฉ
๐‘ธ๐Ÿ๐‘ฉ
WA > WB
Q1B
Q2A
Sink, T2
HEA
Source, T1
Q1A
Q2B
WA HEB
WB
HEB is reversed
Q1B
Q2A
Sink, T2
HEA
Source, T1
Q1A
Q2B
WA
HB
WB E
โ€ข Since HEB is a reversible heat engine, the magnitudes of heat and work transfer quantities will
remain the same, but their directions will be reversed
โ€ข Since WA > WB, some part of WA (equal to WB) may be fed to drive the reversed heat engine โˆƒHB.
Since Q1A = Q1B = Q1, the heat discharged by โˆƒHB may be supplied to HEA
โ€ข The source may, therefore, be eliminated
โ€ข The net result is that HEA and โˆƒHB together constitute a heat engine which, operating in a cycle
produces net work WA โ€“ WB while exchanging heat with a single reservoir at T2
โ€ข This violates the Kelvin-Planck statement of the second law Hence the assumption that ๐œ‚A>๐œ‚B is
wrong
The combined system of heat pump HEB and engine HEA, becomes a PMM2
Q1B = Q1
Q2A
Sink, T2
HEA
Q1A = Q1
Q2B
WA
HB
WB E
WA = WB
โ€˜โ€˜The efficiency of all reversible heat engines operating between the same temperature levels is
the sameโ€
Since, the efficiencies of all reversible engines operating between the same heat reservoirs are the
same, the efficiency of a reversible engine is independent of the nature or amount of the working
substance undergoing the cycle
โ€ข ๐œ‚A cannot be greater than ๐œ‚B
โ€ข HEA and โˆƒHB together violate the Kelvin-Planck statement, โˆด ๐œ‚B > ๐œ‚A
โ€ข Similarly, if we assume ๐œ‚B > ๐œ‚A and reverse the engine HEA, we observe that ๐œ‚B cannot be greater
than ๐œ‚A, โˆด ๐œ‚B = ๐œ‚A
Hopefully, you understand todayโ€™s lesson.
Otherwise, youโ€™ll end up like this cow.

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Thermodynamics

  • 2. Limitations of First Law of Thermodynamics โ€ข Heat flows from a system of higher temperature to a system of lower temperature and never from lower temperature system to higher temperature system โ€ข From first law of thermodynamics, โ€œHeat lost and heat gain must be equal in both the processesโ€ โ€ข According to first law, it is assumed that the energy transfer can take place in either direction, it does not specify the direction of energy transfer Heat is transferred from hotter side to the colder side of the rod But never from colder to hotter side by itself by itself hotter side colder side Why does energy travel always from higher value to lower value?
  • 3. โ€ข All work can be converted into heat but all heat cannot be converted into work - For example: In internal combustion engine, all heat generated from combustion of fuel is not converted into work, but a portion of input heat has to be rejected to exhaust gases, oil, cooling water Image source: http://teamspeed.com QExhaust QFuel QFriction QCooling Water QOil
  • 4. - Example : In power plants, all heat generated from combustion of coal is not converted into work, but a portion of input heat has to be rejected in the condenser Image source: http://google.com
  • 5. What First Law of Thermodynamics Tells Us โ€“ Interpretations First law of thermodynamics is a necessary condition but not sufficient condition for a process to take place First law of thermodynamics states โ€œwork can be converted into heat and heat into workโ€ First law makes no distinction between forms of energy, silent about the possibility of energy conversion First law is not sufficient to predict weather a system will or will not under go a particular change
  • 6. What Second Law of Thermodynamics Tells Us โ€“ Interpretations Second law of thermodynamics indicates that, โ€œall heat cannot be converted into workโ€ According to second law of thermodynamics, โ€œheat will only be transferred from high temperature to lower temperature and not vice versaโ€œ โ€œFirst law of thermodynamicsโ€, is a quantitative statement and โ€œSecond law of thermodynamicsโ€, is a qualitative statement Second law states that whether it is possible for energy transfer to proceed along a particular direction or not A cycle can only occur if it satisfies both the first law and second law of thermodynamics
  • 7. Energy Reservoirs MER WT Wnet Boiler Turbine Condenser Pump TERH (SOURCE) TERL (SINK) Wp Q1 Q2 Thermal Energy reservoirs (TER): is defined as a large body of infinite heat capacity, which is capable of absorbing or rejecting an unlimited quantity of heat without suffering appreciable change in its thermodynamic coordinates. All process are quasi-static Constant Temperature Constant Temperature Mechanical Energy reservoirs (MER): is a large body enclosed by an adiabatic impermeable wall capable of storing work as kinetic energy or potential energy. All process are quasi-static
  • 8. Heat Engine โ€ข Heat Engine is a device which working in a cycle converts energy in form of heat into work - Heat engines convert heat to work โ€ข There are several types of heat engines, but they are characterized by the following: - They all receive heat from a high-temperature source (oil furnace, nuclear reactor, etc.) - They convert part of this heat to work - They reject the remaining waste heat to a low-temperature sink - They operate in a cycle
  • 9. Heat Engine Boiler Pump Condenser QB / Q1 WT WP WT - WP Net work output of the system during cyclic process Turbine Boiler Turbine Condenser Pump Water Steam Water Steam Water Heat Source: Furnace Heat Sink: Lake/River QC / Q2
  • 10. QB โ€“ QC = WT - WP ๐›ˆ = "#$%#$ '()* +,%#$ -./$ = WT โˆ’ WP Q1 ๐›ˆ = 30% - 40% = Q1 โ€“ Q2 Q1 Q2 = 60%- 70% Q1 = 1 - Q2 Q1 T1 = 500โˆ˜C W Q โ€“ W = Q2 Q1 T2 = 20โˆ˜C Source Sink (atmosphere) Heat Engine Q. Is it possible to save the rejected heat QC in a power cycle? Answer: NO, because without the cooling in condenser the cycle cannot be completed - Every heat engine must waste some energy by transferring it to a low-temperature reservoir in order to complete the cycle, even in idealized cycle ๐‘ญ๐’“๐’๐’Ž ๐’‡๐’Š๐’“๐’”๐’• ๐‘ณ๐’‚๐’˜ ๐’๐’‡ ๐‘ป๐’‰๐’†๐’“๐’Ž๐’๐’…๐’š๐’๐’‚๐’Ž๐’Š๐’„๐’” ๐’‡๐’๐’“ ๐’‚ ๐’„๐’š๐’„๐’๐’Š๐’„ ๐’‘๐’“๐’๐’„๐’†๐’”๐’” โˆฎ๐๐‘ธ = โˆฎ๐๐‘พ Q1 โ€“ Q2 = WT - WP
  • 11. Refrigerator Throttle Compressor QR/Q2 Refrigerator W โ€ข In nature, heat flows from high-temperature regions to low-temperature ones โ€ข The reverse process, however, cannot occur by itself โ€ข The transfer of heat from a low- temperature region to a high-temperature one requires special devices called refrigerators Refrigerators are cyclic devices, and the working fluids used in the cycles are called refrigerant Condenser QC/Q1
  • 12. Win Cold Environment Warm House Objectives of Refrigerator & Heat Pump Heat Pump Win Q1 Q2 Refrigerated Space Warm Environment Refrig erator Desired Output Condenser Evaporator Expansion Valve Compressor Wc T < T atm. T = T atm. Desired Output T = T atm. T > T atm. Q1 Q2
  • 13. ๐‘ญ๐’“๐’๐’Ž ๐’‡๐’Š๐’“๐’”๐’• ๐‘ณ๐’‚๐’˜ ๐’๐’‡ ๐‘ป๐’‰๐’†๐’“๐’Ž๐’๐’…๐’š๐’๐’‚๐’Ž๐’Š๐’„๐’” ๐’‡๐’๐’“ ๐’‚ ๐’„๐’š๐’„๐’๐’Š๐’„ ๐’‘๐’“๐’๐’„๐’†๐’”๐’” โˆฎ๐๐‘ธ = โˆฎ๐๐‘พ W = Qc - QR = Q1 - Q2 COPR = ๐‘ฏ๐’†๐’‚๐’• ๐‘น๐’†๐’Ž๐’๐’—๐’†๐’… ๐’ƒ๐’š ๐’•๐’‰๐’† ๐‘น๐’†๐’‡๐’“๐’Š๐’ˆ๐’†๐’“๐’‚๐’•๐’๐’“ ๐‘พ๐’๐’“๐’Œ ๐‘บ๐’–๐’‘๐’‘๐’๐’Š๐’†๐’… = Q2 W = QR QC โˆ’ QR โ€ข The performance of refrigerators and heat pumps is expressed in terms of the coefficient of performance (COP) COPR = ๐‘ฉ๐’†๐’๐’Š๐’‡๐’• ๐‘ช๐’๐’”๐’• W T2 = - 4โˆ˜C T1 = 35โˆ˜C Refrigerator Heat Engine Sink (atmosphere) Q1 = Q2 Q1 โˆ’ Q2 In a refrigerator, the desired effect is the amount of heat removed Q2 from the space being heated Q2
  • 14. W Q1 Q2 T2 = 4โˆ˜C T1 = 25โˆ˜C Heated Space Atmoshpere Heat Pump Heat Pump โ€ข Heat pumps transfer heat from a low-temperature medium to a high-temperature โ€ข Refrigerators and heat pumps are essentially the same devices; they differ in their objectives only โ€ข Refrigerator is to maintain the refrigerated space at a low temperature โ€ข On the other hand, a heat pump absorbs heat from a low-temperature source and supplies the heat to a warmer medium In a heat Pump, the desired effect is the amount of heat supplied Q1 to the space being heated COPHP = ๐‘ฏ๐’†๐’‚๐’• ๐‘บ๐’–๐’‘๐’‘๐’๐’Š๐’†๐’… ๐’ƒ๐’š ๐’•๐’‰๐’† ๐‘ฏ๐’†๐’‚๐’• ๐‘ท๐’–๐’Ž๐’‘ ๐‘พ๐’๐’“๐’Œ ๐‘บ๐’–๐’‘๐’‘๐’๐’Š๐’†๐’… = Q1 W = Q1 Q1 โˆ’ Q2 = 1 + Q2 Q1 โˆ’ Q2 = 1 + COPR The COP of a heat pump operating as a heat pump is higher that the COP of the same machine operating as a refrigerator by unity
  • 15. โ€ข The performance of air conditioners and heat pumps is often expressed in terms of the energy efficiency ratio (EER) or seasonal energy efficiency ratio (SEER) determined by following certain testing standards - SEER : is the ratio the total amount of heat removed by an air conditioner or heat pump during a normal cooling season (in Btu) to the total amount of electricity consumed (in watt-hours, Wh), and it is a measure of seasonal performance of cooling equipment - EER : is a measure of the instantaneous energy efficiency, and is defined as the ratio of the rate of heat removal from the cooled space by the cooling equipment to the rate of electricity consumption in steady operation โ€ข Therefore, both EER and SEER have the unit Btu/Wh - 1 kWh = 3.412 Btu (1 Wh = 3.412 Btu, a device that removes 1 kWh of heat from the cooled space for each kWh of electricity it consumes (COP = 1) will have an EER of 3.412) - Therefore, the relation between EER and COP, EER = 3.412.COPR Performance of Refrigerators, Air-Conditioners, and Heat Pumps The heat transfer rate is often given in terms of tones of heating or cooling One ton = 12,000 Btu = 211 kJ/min
  • 16. โ€ข Air conditioners or heat pumps SEER: 13 to 21, which correspond to COP values of 3.8 to 6.2. - Most air conditioners have an EER between 8 to 12 (COP of 2.3 to 3.5) โ€ข Best performance is achieved using units equipped with variable-speed drives (also called inverters) - Variable-speed compressors and fans allow the unit to operate at maximum efficiency for varying heating/cooling needs and weather conditions as determined by a microprocessor - In the air-conditioning mode, for example, they operate at higher speeds on hot days and at lower speeds on cooler days, enhancing both efficiency and comfort โ€ข The EER or COP of a refrigerator decreases with decreasing refrigeration temperature - Therefore, it is not economical to refrigerate to a lower temperature than needed โ€ข The COPs of refrigerators (range): 2.6 to 3.0 for cutting and preparation rooms 2.3 to 2.6 for meat, deli, dairy, and produce 1.2 to 1.5 for frozen foods 1.0 to 1.2 for ice cream units Note: COP of freezers is about half of the COP of meat refrigerators - It costs twice as much to cool the meat products with refrigerated air that is cold enough to cool frozen foods - It is good energy conservation practice to use separate refrigeration systems to meet different refrigeration needs
  • 17. W Heat Engine Second Law of Thermodynamics: Kelvin Plankโ€™s Statement - It is impossible for any device that operates on a cycle to receive heat from a single reservoir and produce a net amount of work - In other words, no heat engine can have a thermal efficiency of 100% Source (TH) A heat engine that violates the Kelvin-Planck statement of the second law cannot be built Thermal efficiency of 100% Qin Wnet = Qin Qout = 0 โ€œIt is impossible for any system to operate in a thermodynamic cycle and deliver a net amount of work to its surroundings while receiving an energy transfer by heat from a single thermal reservoirโ€
  • 18. W Heat Pump Second Law of Thermodynamics: Clausius Statement - Heat cannot flow from itself from a system low temperature to a system at high temperature. - COP = Q/W = Q/0 = โˆž ( a condition not possible) - The only alternative is that some external work must be supplied to the machine System (T1) A heat engine that violates the Kelvin-Planck statement of the second law cannot be built Qin Q2 โ€œHeat cannot, of itself, pass from a colder to a hotter body โ€ โ€œIt is impossible for a self acting machine working in a cyclic process unaided by any external agency, to convey heat from a body at a lower temperature to a body at a higher temperatureโ€ System (T2)
  • 19. Perpetual Motion Machine of the Second Kind (PMMK2) โ€ข Without violating the first law, a machine can be imagined which would continuously absorb heat from a single thermal reservoir and would convert this heat completely into work - The efficiency of such a machine would be 100% - This machine is called the perpetual motion machine of the second kind (PMM2) W Heat Engine Source (TH) Qin Wnet = Qin Qout = 0 When the thermal energy is equivalent to the work done, this does not violate the law of conservation of energy. However it does violate the more subtle second law of thermodynamics
  • 20. Carnot Cycle โ€ข The cycle was first suggested by Sadi Carnot, in 1824, which works on reversible cycle โ€ข Any fluid may be used to operate the Carnot cycle, which is performed in an engine cylinder the head of which is supposed alternatively to be perfect conductor or a perfect insulator of a heat โ€ข Heat is caused to flow into the cylinder by the application of high temperature energy source to the cylinder head during expansion, and to flow from the cylinder by the application of a lower temperature energy source to the head during compression Source, T1 Sink, T2 Working Substance Adiabatic Cover Diathermic Cover Cylinder Head Heat Insulation Heat Insulation Piston Piston motion
  • 21. The assumptions made for describing the working of the Carnot engine are as follows : 1. The piston moving in a cylinder does not develop any friction during motion 2. The walls of piston and cylinder are considered as perfect insulators of heat 3. The cylinder head is so arranged that it can be a perfect heat conductor or perfect heat insulator 4. The transfer of heat does not affect the temperature of source or sink 5. Working medium is a perfect gas and has constant specific heat 6. Compression and expansion are reversible
  • 22. Diathermic Cover Working Substance Adiabatic Cover Piston motion Stage 1 โ€“ Isothermal Expansion (Process 1-2) - Hot energy source at temperature T1 is applied - Heat Q1 is taken in whilst the fluid expands isothermally and reversiblyat constant high temperature T1 Q1 Stage 2 โ€“ Adiabatic Expansion (Process 2-3) - The cylinder becomes a perfect insulator so that no heat flow takes place - The fluid expands adiabatically and reversibly whilst temperature falls from T1 to T2 Source, T 1
  • 23. Sink, T 2 Working Substance Diathermic Cover Adiabatic Cover Stage 3 โ€“ Isothermal Compression (Process 3-4) - Cold energy source at temperature T2 is applied - Heat Q2 flows from the fluid whilst it is compressed isothermally and reversibly at constant lower temperature T2 Q2 Stage 4 - Adiabatic Compression (Process 4-1) - Cylinder head becomes a perfect insulator so that no heat flow occurs - The compression is continued adiabatically and reversibly during which temperature is raised from T2 to T1
  • 24. Q1 = W1-2 = P1 V1 In ๐‘ฝ๐Ÿ ๐‘ฝ๐Ÿ Q1 = W1-2 = mRT1 In ๐‘ฝ๐Ÿ ๐‘ฝ๐Ÿ Q2 = W3-4 = - P3 V3 In ๐‘ฝ๐Ÿ’ ๐‘ฝ๐Ÿ‘ Q2 = W3-4 = mRT2 In ๐‘ฝ๐Ÿ‘ ๐‘ฝ๐Ÿ’ Heat Rejected Heat Added ๐œ‚ = 1 - Q2 Q1
  • 25. ๐œ‚ = ๐‘ต๐’†๐’• ๐‘พ๐’๐’“๐’Œ ๐‘ถ๐’–๐’•๐’‘๐’–๐’• ๐‘ฏ๐’†๐’‚๐’• ๐‘ฐ๐’๐’‘๐’–๐’• = ๐‘พ๐’๐’†๐’• ๐‘ธ๐Ÿ ๐‘ญ๐’“๐’๐’Ž ๐’‡๐’Š๐’“๐’”๐’• ๐‘ณ๐’‚๐’˜ ๐’๐’‡ ๐‘ป๐’‰๐’†๐’“๐’Ž๐’๐’…๐’š๐’๐’‚๐’Ž๐’Š๐’„๐’” ๐’‡๐’๐’“ ๐’‚ ๐’„๐’š๐’„๐’๐’Š๐’„ ๐’‘๐’“๐’๐’„๐’†๐’”๐’” โˆฎ๐๐‘ธ = โˆฎ๐๐‘พ ๐’๐’“ ๐‘พ๐’๐’†๐’• = ๐‘ธ๐Ÿ โˆ’ ๐‘ธ๐Ÿ ๐œ‚ = 1 - T2 T1 (V2/V1) = (V3/V4) P2 V2 ๐›พ = P3 V3 ๐›พ T1 V2 (๐›พ- 1) = T2 V3 (๐›พ- 1) P4 V4 ๐›พ = P1 V1 ๐›พ PV= nRT ; PV/T = nR =C P2V2/T1 = P3V3/T2 P4V4/T2 = P1V1/T1 1 2 3 4 T1 V1 (๐›พ- 1) = T2 V4 (๐›พ- 1) 5 6 Dividing 1/3 and 2/4 Dividing 5/6 = 1 - Q2 Q1
  • 26. Temperature Entropy Q1 Q2 T2 T1 4 3 2 1 Area of the rectangle a-b-c-d represents work output per cycle and it equals Q1 โ€“ Q2 = (T1 โ€“ T2).dS Isotherms Frictionless Adiabats S1 =S4 S2 = S3
  • 27. Efficiency of a Reversible Heat Engine โ€ข From the above expression, it may be noted that as T2 decreases and T1 increases, efficiency of the reversible cycle increases โ€ข Since ๐œ‚ is always less than unity, T2 is always greater than zero and positive (+ ve)
  • 28. Carnot Heat Pump โ€ข An engine, which consists entirely of reversible processes, can operate in the reverse direction, so that it follows the cycle as shown and operates as a heat pump Work (W) will be needed to drive the pump The enclosed area represents this work which is exactly equal to that flowing from it when used as engine (process 4-3) Q2 is being taken in at the lower temperature T2 during the isothermal expansion (process 2-1) Q1 is being rejected at the upper temperature T1 Q1 Q2
  • 29. 1. It is impossible to perform a frictionless process 2. It is impossible to transfer the heat without temperature potential 3. Isothermal process can be achieved only if the piston moves very slowly to allow heat transfer so that the temperature remains constant - Adiabatic process can be achieved only if the piston moves as fast as possible so that the heat transfer is negligible due to very short time available - The isothermal and adiabatic processes take place during the same stroke therefore the piston has to move very slowly for part of the stroke and it has to move very fast during remaining stroke - This variation of motion of the piston during the same stroke is not possible Carnot cycle cannot be performed in practice because of the following reasons
  • 30. Equivalence of Clausius Statement to the Kelvin-Planck Statement W = Q1 โ€“ Q2; Since, there is no heat interaction with the low temperature, it can be eliminated Q1 Q2 Low Temperature Reservoir T2 Heat Engine Net Work (W) = Q1 โ€“ Q2 High Temperature Reservoir T1 Heat Pump Q1 Q2 A heat pump which requires no work and transfers an amount of Q2 from a low temperature to a higher temperature reservoir (violation of the Clausius statement) The combined system of the heat engine and heat pump acts then like a heat engine exchanging heat with a single reservoir, which is the violation of the Kelvin-Planck statement Heat rejected Q1 > Q2 The Kelvinโ€™s and Clausiusโ€™s statements of the second law are equivalent. i.e. if we violate Kelvinโ€™s statement, then we will automatically violate the Clausiusโ€™s statement of the second law (and vice-versa) No Work
  • 31. Q1 Q2 = 0 Low Temperature Reservoir T2 Heat Engine W = Q1 High Temperature Reservoir T1 Heat Pump Q1 Q2 A heat engine which converts all heat to work, without rejecting heat to low temperature (Violation of the Kelvin Plank statement) The combined system constitutes a device which transfers heat from low temperature reservoir to high temperature without any work from external agency, which is the violation of the Clausius statement Q1 > Q2 Violation of Kelvin โ€“ Plank Statement leads to violation of Clausiusโ€™s statements W = Q1
  • 32. Can you beat Second Law Can you cool your room by leaving the refrigerator door open ? The heat removed from the interior of the refrigerator is deposited back into the kitchen by the coils on the back! Second Law of Thermodynamics says that work is needed to move the heat from cold to hot, so the actual amount of heat added to the kitchen is MORE than the amount removed from the refrigerator
  • 33. โ€ข The second corollary to the Kelvin-Planck statement holds that โ€œAll reversible engines operating between the same thermal reservoirs have the same ๐œ‚โ€ - This is independent of any details of the cycle or the materials involved - The thermal efficiency, ๐œ‚, should depend only on the character of the reservoirs involved Thermodynamic Temperature Consider a case of reversible heat engine operating between two reservoirs - Its thermal efficiency is given by ๐œ‚ = Q1 โˆ’ Q2 Q1 = 1 - Q2 Q1 โ€ข The temperature of a reservoir remains uniform and fixed irrespective of heat transfer - This means that reservoir has only one property defining its state and the heat transfer from a reservoir is some function of that property, temperature. Thus Q = ฯ† (K), where K is the temperature of reservoir Q1 Q2 = ฯ†(K1) ฯ†(K2) => Q1 Q2 = T1 T2 ; T1 and T2 are the thermodynamic temperatures of the reservoirs Zero thermodynamic temperature (that temperature to which T2 tends, as the heat transfer Q2 tends to zero) has never been attained and one form of third law of thermodynamics is the statement : โ€˜โ€˜The temperature of a system cannot be reduced to zero in a finite number of processesโ€
  • 34. The amounts of heat rejected by engines B and C must be the same since engines A and B can be combined into one reversible engine operating between the same reservoirs as engine C and thus the combined engine will have the same efficiency as engine C. Since the heat input to engine C is the same as the heat input to the combined engines A and B, both systems must reject the same amount of heat
  • 35. โ€ข After establishing the concept of a zero thermodynamic temperature, a reference reservoir is chosen and assigned a numerical value of temperature โ€ข Any other thermodynamic temperature may now be defined in terms of reference value and the heat transfers that would occur with reversible engine, T = Tref. Q Qref. โ€ข Let us make an arbitrary choice to avoid ratios. We take, for convenience, the temperature of the triple point of water to be 273.15 K. Thus for any system, the local T is T = 273.3. Q Qref. This implies we can connect our heat engine to a reservoir maintained at the triple point temperature of water, and measure the associated Qs for the heat engine โ€ข We would like to drive our efficiency to be as close to unity as possible, nature limits us โ€ข Generally, we have little to no control over the environmental temperature TL, so it is a lower bound, usually around TL โˆผ 300 K. And material properties for engines limit TH . For many metals, TH โˆผ 1500 K is approaching values where material strength is lost โ€ข So a practical upper bound based on these numbers tell us โ€ข ฮทโˆผ 1 โˆ’ (300K)/(1500K) = 0.8 is may be the most we can expect. We plot ฮท as a function of TH for fixed TL = 300 K For real systems, with irreversible features, the values are much lower
  • 36. โ€ข The determination of thermodynamic temperature cannot be made in this way as it is not possible to build a reversible engine โ€ข Temperatures are determined by the application of thermodynamic relations to other measurements โ€ข The SI unit of thermodynamic temperature is the kelvin (K) โ€ข The relation between thermodynamic temperature and Celsius scale - Thermodynamic temperature = Celsius temperature + 273.15ยฐ - The kelvin unit of thermodynamic temperature is the fraction 1 temperature of โ€˜Triple pointโ€™ of water
  • 37. Carnot Theorem โ€œIt states that of all engines operating between a given constant temperature source and a given constant temperature sink, none has a higher efficiency than a reversible engineโ€ Let HEA be any heat engine and HEB be any reversible heat engine We have to prove that efficiency of HEB is more than that of HEA Let us assume that ๐œ‚A > ๐œ‚B Q1A = Q1B = Q1 ๐œ‚A = ๐œ‚B ๐‘พ๐‘จ ๐‘ธ๐Ÿ๐‘จ = ๐‘พ๐‘ฉ ๐‘ธ๐Ÿ๐‘ฉ WA > WB Q1B Q2A Sink, T2 HEA Source, T1 Q1A Q2B WA HEB WB
  • 38. HEB is reversed Q1B Q2A Sink, T2 HEA Source, T1 Q1A Q2B WA HB WB E โ€ข Since HEB is a reversible heat engine, the magnitudes of heat and work transfer quantities will remain the same, but their directions will be reversed โ€ข Since WA > WB, some part of WA (equal to WB) may be fed to drive the reversed heat engine โˆƒHB. Since Q1A = Q1B = Q1, the heat discharged by โˆƒHB may be supplied to HEA โ€ข The source may, therefore, be eliminated
  • 39. โ€ข The net result is that HEA and โˆƒHB together constitute a heat engine which, operating in a cycle produces net work WA โ€“ WB while exchanging heat with a single reservoir at T2 โ€ข This violates the Kelvin-Planck statement of the second law Hence the assumption that ๐œ‚A>๐œ‚B is wrong The combined system of heat pump HEB and engine HEA, becomes a PMM2 Q1B = Q1 Q2A Sink, T2 HEA Q1A = Q1 Q2B WA HB WB E WA = WB
  • 40. โ€˜โ€˜The efficiency of all reversible heat engines operating between the same temperature levels is the sameโ€ Since, the efficiencies of all reversible engines operating between the same heat reservoirs are the same, the efficiency of a reversible engine is independent of the nature or amount of the working substance undergoing the cycle โ€ข ๐œ‚A cannot be greater than ๐œ‚B โ€ข HEA and โˆƒHB together violate the Kelvin-Planck statement, โˆด ๐œ‚B > ๐œ‚A โ€ข Similarly, if we assume ๐œ‚B > ๐œ‚A and reverse the engine HEA, we observe that ๐œ‚B cannot be greater than ๐œ‚A, โˆด ๐œ‚B = ๐œ‚A
  • 41. Hopefully, you understand todayโ€™s lesson. Otherwise, youโ€™ll end up like this cow.