Monday 23 February 2015

MECHANICAL ENGINEERING – 2003,PAPER – II ,Section B

                    Time Allowed: Three Horus      Maximum marks: 200
Candidates should attempt Questions 1 and 5 which are compulsory and any THREE of the remaining questions selecting at least ONE question from each Section.
If any data is considered insufficient, assume suitable valur.
  
SECTION B
5.       Answer any four parts:

(a)    The evaporator and condenser temperatures in a reverse Carnot refrigeration cycle of 1 TR capacity are 263 K and 313LK respectively. The outlet of compression is saturated vapour and into to turbine is saturated liquid. Find the mass flow rate, work done condenser heat rejection and COP. Properties of refrigerant at saturation in SI units are as follows:

t (K)
hf
hg
S f
Sg
263
154.056
1450.22
0.82965
5.755
313
390.587
1490.42
1.64377
5.1558

(b)   Air enters a cooling coil at 30˚C, 75 % relative humidity. The apparatus dewpoint is 12˚ c and bypass factor is 0.15. Find the temperature and humidity ratio at outlet of cooling coil. If mass flow rate of air is 10 kg / s, find the condensate rate and cooling capacity of cooling coil. The partial pressures of water vapour at 12˚ C and 30˚C are 1.4017 and 4.2431 kPa respectively. Atmospheric pressure is 101.325 kPa. Enthalpy of condensate at 12˚C = 50.24 kJ / kg.
(c)    Explain the nomenclature Rabc for CFCs and inorganic compounds. What is meant by ozone depletion? Name at least two refrigerants that do not cause it.
(d)   State Buckingham’s  theorem. Using Buckingham’s  theorem obtain an expression for drag force on a partially submerged body moving with a relative velocity V in fluid, the other variables being linear dimension L height of surface roughness K, the fluid density ƿ and gravitational accelerating.
(e)   Discuss the criteria for the selection of site for steam and hydroelectric power plants.

6.       (a) A refrigeration system of 10 TR cooling capacity has condenser and evaporator temperatures of 45˚C and – 20 ˚C respectively. The vapour leaving the evaporator sub cools the liquid leaving the condenser from 45 ˚C to 25˚C. Draw schematic diagram and T.S fiagram considering isentropic compression, isobaric heat absorption and rejection. Determine mass flow rate, compressor work. Condenser heat rejection and COP. Use vapour specific heat at condenser pressure to find COP. USE vapour specific heat at condenser pressure to fin adiabatic discharge temperature and enthalpy. The properties in SI units at saturation are:


hf
hg
sg
C pg
Cpf
-20˚ C
17.8
178.7
0.7088
0.61
-
45˚C
79.7
204.9
0.6812
0.755
1.02

                        (b) Define thermodynamic wet bulb temperature t* and show that humidity ratio may be expressed as

W = W* h* fg  - 1.005 (t- t*)    /   hg (t) – h*f

Where enthalpy of moist air is expressed as h= 1.005 (t) + hg (t).

7.       (a)  Diabatic flow of dry air takes place through a frictionless constant area duct. At some particular section of the duct, the Mach number is 4.0 while stagnation temperature and static pressure are 280 K and 0.5 bar respectively. Calculate the stagnation temperature. Static and stagnation pressures at a section where the Mach numbers is 2.0 also find the amount of heat transfer which causes this reduction Mach number. Take Cp= 1.005 kJ/ kg and γ = 1.4.
M
P /ᵖP*
T/ T*
Tₒ/ Tₒ*
Pₒ / Pₒ*

2.0
0.364
0.529
0.793
1.503
4.0
0.1026
0.168
0.589
8.277
  
                                                                                                                 
          (b) Explain what you understand by specific speed of a turbo machine. Give its importance.
Calculate the specific speeds of the following cases:

             (i)                  A 2500 kW gas turbine is running at a speed of  18000 RPM. The entry and exit conditions of the gas are T₁ = 1100 K₁ P₁ =60 bar, P₂ = 30 bar.
            (ii)                A centrifugal compressor develops a pressure ratio of 1.5 while running at 24000 RPM and discharging 2.0 kg/s of air, the entry conditions are P₁ =1.0, T₁ = 290K.
1 or both cases take
γ + 1.4, R = 287 J / kg – k, Cᵨ =1.005 kJ / kg –k.

8.       (a) Explain clearly, “heat rate curve’ and “ Incremental rate curve’. Show that the incremental rate curve crosses the heat rate curve at the lowest value of heat rate.
The incremental fuel costs for two generating units A and B of a plant are given by
dF a / dPa  = 0.065 Pa + 25
dF b / dPb = 0.08 Pb + 20
where F is fuel cost in Re / hr and P is power output in MW. Find –

(i)                  The economic loading of the two units when the total load supplied by the power plant is 160 MW.
(ii)                The loss in fuel cost/ hr if the load is shared equally by the units.

(b) Discuss the importance of the terms, capacity factor and use factor from the economic point of view of the power plant.

A power station is said to have a sue factor of 50% and a capacity factor of 45%. How many hours the plant did not operate during the year?

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