Week-2
Refrigeration Cycle
Refrigeration cycles can be categorized
Gas cycle or air cycle
Vapors cycle
Vapor Cycle In a vapor cycle the working fluid undergoes phase change and refrigeration effect is due to the vaporization of refrigerant liquid. The required mass flow rates for a given refrigeration capacity will be much smaller compared to a gas cycle.
subdivided into vapor compression systems, vapor absorption systems, vapor jet systems
Air Cycle In a typical gas cycle, the working fluid (a gas) does not undergo phase change In gas cycles, heat rejection and refrigeration take place as the gas undergoes sensible cooling and heating.
Applications: Passenger air craft, jet aircraft Missiles
Air Refrigerator working on Reversed Carnot Cycle
Carnot Cycle is the ideal cycle with 100% efficiency.
It is the ideal Engine and if we reverse it, it will be the ideal Refrigeration Cycle.
Carnot heat engine
T-s Diagram
T
s
1
2 3 QH
4
QL
Cooling space at TL
QL
Atmosphere at TH
QH
Win
Condenser
Evaporator
Compressor Turbine
3 2
4 1
1-2 : Isentropic Compression
2-3 : Isothermal Heat rejection
3-4 : Isentropic Expansion
4-1 : Isothermal Heat addition
Carnot refrigeration cycle
Carnot cycle consists of reversible processes which make its
efficiency higher than could be achieved in an actual cycle
Why? Discuss the Carnot cycle if it is unattainable idea?
There are two reasons:
I. It serves as a standard of comparison
II. It provides a convenient guide to the temperatures that should
be maintained to achieve maximum effectiveness
Coefficient of Performance (COP)
Unlike Heat engine, we use COP in refrigeration system because the output in process 2-3 is usually wasted.
Net work= Heat absorbed in evaporator-Heat rejected in condenser
The heat transferred during isothermal processes 2-3 and 4-1 are given by:
Net Work output =Heat rejected- Heat absorbed
Wnet=Q2-3 Q4-1 Wnet=Th(S2 S3) TL(S1-S4)
Lh
L
Lh
LCarnot
netCarnot
TTT
SSTSSTSSTCOP
WQ
inputWorkabsorbedHeatCOP
=
=
==
)()()(
..
4132
41
14
COP can be maximized by maximizing TL (target temperature)
and minimizing Th (ambient temperature)
In summer performance of refrigerator decreases because Th increases.
In Refrigerator the value of TL is less than for AC, so COP of AC is higher than COP of Refrigerator.
Lh
LCarnot TT
TCOP
=
1. Higher temperature should be more than the temperature of
cooling air to which heat is to be rejected
2. Lower temperature should be less than the temperature of
substance to be cooled
Temperature Limitation
What control do we have? We can concentrate on keeping the T as small as possible. Reduction of T can be accomplished by increasing A or U in the equation
In order to decrease T to zero, either U or A would have to be infinite. Since infinite values of U and A would also require an infinite cost; the actual selection of equipment always stops short of reducing T to zero.
Difficulty of achieving isothermal heat transfer during processes 2-3 and 4-1. For a gas to have heat transfer isothermally, it is essential to carry out work transfer from or to the system when heat is transferred to the system (process 4-1) or from the system (process 2-3). This is difficult to achieve in practice. Frictional effects in compressor leads to irreversibility, hence completely isentropic compression is not possible to achieve. Perfect insulation cannot be made practically
Limitations of Carnot cycle:
Bell-Coleman or Reversed Brayton Cycle
Process 1-2: Reversible, adiabatic compression in a compressor
Process 2-3: Reversible, isobaric heat rejection in a heat
exchanger
Process 3-4: Reversible, adiabatic expansion in a turbine
Process 4-1: Reversible, isobaric heat absorption in a heat
exchanger
Process 1-2: Gas at low pressure is compressed isentropically from state 1 to state 2.
Process 2-3: Hot and high pressure gas flows through a heat exchanger and rejects heat sensibly and isobarically to a heat sink.
Process 3-4: High pressure gas from the heat exchanger flows through a turbine, undergoes isentropic expansion and delivers net work output.
Process 4-1: Cold and low pressure gas from turbine flows through the low temperature heat exchanger and extracts heat sensibly and isobarically from a heat source
]1[]1[
]1[
)()(
)()()(
..
4
14
3
23
4
14
4132
41
4132
41
=
=
==
TTT
TTT
TTT
TTTTTTCOP
TTCTTCTTC
doneWorkabsorbedHeatCOP
PP
P
4132
1
4
3
1
1
2
.,4
3..1
2
,21...
PPandPP
TTand
TT
processisentropicFor
PP
PP
==
==
Therefore COP of the cycle can be written as
Comparison of reverse Carnot and reverse Brayton cycle
COP of reverse Brayton cycle decreases as the pressure ratio rp increases
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