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Calculations with Entropy - Thermodynamics - Solved Quiz, Exercises of Thermodynamics

Some of the topic in thermodynamics are: Property tables and ideal gases, First law for closed and open (steady and unsteady) systems, Entropy and maximum work calculations, Isentropic efficiencies, Cycle calculations (Rankine, refrigeration, air standard) with mass flow rate ratios. This quiz is about: Calculations with Entropy, Evaporator and the Condenser, Adiabatic Compressor, Interpolation, Superheat Region, Mass Flow Rate, Heat Transfer

Typology: Exercises

2013/2014

Uploaded on 02/01/2014

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Solution Calculations with Entropy
1
2
3
4
Evaporator
Compres sor
Condenser
Throttling
Valve
The ammonia refrigeration cycle shown at the
left has the following properties for both parts
(a) and (b) below: P1 = P4 = 100 kPa; P2 = P3 = 2
MPa; point 1 is a saturated vapor and Point 3 is
a saturated liquid; for the throttling valve, h3 =
h4; the compressor has no heat transfer, and,
the low temperature heat input to the cycle,
which is in the evaporator, is 1 MW.
Determine the power input to the compressor if
(a) T2 = 250oC, (b) the compressor work input is
a minimum.
We can apply the first law to both the evaporator and the condenser as steady-flow devices with
one inlet and one outlet. If we neglect kinetic and potential energies we have the following
equation for the first law:
inoutuhhmWQ
. We are given that there is no heat transfer in
the compressor and we see that there is no useful work in the evaporator. Writing the first law for
each device gives the following pair of equations.
2141 hhmWhhmQ compevap
For a steady flow cycle, the mass flow rate must be the same in both devices. Eliminating the
mass flow rate between these two equations gives the following equation for the compressor
power:
41
21
21
41 hh
hh
QhhmW
hh
Q
mevapcomp
evap
From the problem data we find h1 = hg(P1 = 100 kPa) = 1544.14 kJ/kg; h4 = h3 = hf(P3 = 2 MPa) =
563.87 kJ/kg. These data will be the same for parts (a) and (b). For part a, h2 = h2(P2 = 2 MPa,
T2 = 250oC) = 2170.59 kJ/kg and the required compressor work is found from the combined first-
law equation derived above.
MW
kg
kJ
kg
kJ
kg
kJ
kg
kJ
MW
hh
hh
QW evapcomp 6391.0
874.56314.1544
59.217014.1544
1
41
21
MWWincomp 6391.0
,
The minimum work input for this adiabatic compressor work input occurs when s2 = s1 = sg(100
kPa) = 6.15296 kJ/kg·K. The value of h2 for the minimum compressor work input is found at the
given value of P2 = 2 MPa and s2 = 6.15296 kJ/kg·K; this pair of values is seen to be in the
superheat region so we can find h2 by interpolation at P2 = 2 MPa.
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Solution Calculations with Entropy

1

(^32)

4

E vapo ra to r

Compres sor

Cond ens er

T hrottl i ng V al ve

The ammonia refrigeration cycle shown at the left has the following properties for both parts (a) and (b) below: P 1 = P 4 = 100 kPa; P 2 = P 3 = 2 MPa; point 1 is a saturated vapor and Point 3 is a saturated liquid; for the throttling valve, h 3 = h 4 ; the compressor has no heat transfer, and, the low temperature heat input to the cycle, which is in the evaporator, is 1 MW. Determine the power input to the compressor if (a) T 2 = 250oC, (b) the compressor work input is a minimum. We can apply the first law to both the evaporator and the condenser as steady-flow devices with one inlet and one outlet. If we neglect kinetic and potential energies we have the following

equation for the first law: Q  Wu mh outhin. We are given that there is no heat transfer in

the compressor and we see that there is no useful work in the evaporator. Writing the first law for each device gives the following pair of equations.

Qevap  mh 1 h 4  Wcompm h 1 h 2 

For a steady flow cycle, the mass flow rate must be the same in both devices. Eliminating the mass flow rate between these two equations gives the following equation for the compressor power:

1 4

1 2 1 2 1 4 h h

W mh h Q h h h h

Q

m evap comp evap 

From the problem data we find h 1 = hg(P 1 = 100 kPa) = 1544.14 kJ/kg; h 4 = h 3 = hf(P 3 = 2 MPa) = 563.87 kJ/kg. These data will be the same for parts (a) and (b). For part a, h 2 = h 2 (P 2 = 2 MPa, T 2 = 250oC) = 2170.59 kJ/kg and the required compressor work is found from the combined first- law equation derived above.

  MW

kg

kJ kg

kJ

kg

kJ kg

kJ MW h h

W Q h h comp evap 1544. 14 563. 874 0.^6391

1 4

Wcomp (^) ,in  0. 6391 MW

The minimum work input for this adiabatic compressor work input occurs when s 2 = s 1 = sg( kPa) = 6.15296 kJ/kg·K. The value of h 2 for the minimum compressor work input is found at the given value of P 2 = 2 MPa and s 2 = 6.15296 kJ/kg·K; this pair of values is seen to be in the superheat region so we can find h 2 by interpolation at P 2 = 2 MPa.

kg

kJ kg K

kJ kg K

kJ

kg K

kJ kg K

kJ

kg

kJ kg

kJ

kg

h kJ^6.^512966.^385922032.^91

  1. 52661 6. 38592

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We find the compressor work from the same formula used previously.

  MW

kg

kJ kg

kJ

kg

kJ kg

kJ MW h h

h h W (^) comp in Qevap s 1544. 14 563. 874 0. 4986

1 4

1 2 , 0 ,min  

W^  (^) comp ,min in 0. 4986 MW

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