22-Mec-B3 Energy Conversion and Power Generation · December 2017
Question 2 of 8: Steam turbine on the Mollier chart
Nivaar worked solution (AI-drafted; not reviewed by a licensed engineer)
Notes on this paper
Paper format. 16-Mec-B3 Energy Conversion and
Power Generation, December 2017. Three hours, closed book. Section A is calculative
with five questions and Section B is descriptive with three; candidates answer four
from Section A and two from Section B, so six questions of 10 marks each constitute a
complete 60-mark paper. Reference data for particular questions are bound in as pages
10–13, reference formulae and constants as pages 14–17, and the steam tables
from Granet & Bluestein are provided. Every one of the eight printed questions
is answered below, because the set is a study resource rather than an examination
script.
Reference texts.
Granet & Bluestein, Thermodynamics and Heat Power, 6th ed. (steam tables,
vapour cycles, gas turbines);
El-Wakil, Powerplant Technology (heat balance diagrams, combined cycles,
cooling water, environmental impact of power generation);
Çengel & Boles, Thermodynamics: An Engineering Approach, 9th ed.
(Brayton and Rankine cycles, jet propulsion);
Rayaprolu, Boilers for Power and Process (pulverised firing, low-NOx
burners, ash handling);
Fox & McDonald, Introduction to Fluid Mechanics (hydraulic machines,
energy equation).
Question 2: Steam turbine on the Mollier chart (10 marks)
Given. A throttle-governed reheat turbine at part load, with the states named 1 (stop-valve inlet), 2 (throttled, HP inlet), 3 (HP exhaust), 4 (reheat outlet, LP inlet) and 5 (LP exhaust).
Point
Condition
Value
1
stop valve
16 MPa, 540 °C
2
after the throttle valve
8 MPa, h2 = h1
3
HP turbine exhaust
2 MPa, ηi = 0.90
4
after reheat
2 MPa, 500 °C
5
LP turbine exhaust
0.004 MPa, ηi = 0.80
—
steam flow through both cylinders
75 kg/s
Find. The expansion line on the h-s chart, the HP exhaust pressure and temperature, the LP exhaust moisture and temperature, and the total power at 75 kg/s.
Part (a): the process plotted on the Mollier chart. Throttling runs horizontally to the right (constant enthalpy), each expansion drops to its isentropic end point on the lower isobar and is then shortened by the internal efficiency, and the reheat line climbs back up the 2 MPa isobar.
Approach. Read h and s at the stop valve, carry the enthalpy horizontally across the throttle, drop vertically to each lower isobar to get the isentropic end point, shorten each drop by the internal efficiency, and multiply the sum of the two real drops by the mass flow. Chart readings are quoted to the nearest 10 kJ/kg, with the steam-table values alongside them, because the chart cannot be read more finely than that.
Part (a) — locate the stop-valve state and carry it across the throttle. At 16 MPa and 540 °C the chart reads about 3410 kJ/kg (tables: 3412.1) with $s_1 = 6.449$ kJ/kg·K. A throttle valve does no work and passes no heat, so the steady-flow energy equation collapses to $h_2 = h_1$: $$h_2 = h_1 = 3412\ \text{kJ/kg} \quad \text{at}\quad p_2 = 8\ \text{MPa}$$ Following the horizontal line to the 8 MPa isobar gives $t_2 \approx 505\ {}^\circ\text{C}$ and $s_2 = 6.743$ kJ/kg·K. The entropy has risen by 0.294 kJ/kg·K — that increase is the work the governing valve has destroyed before the steam ever reaches a blade.
Part (a) — the high pressure expansion. Dropping vertically from point 2 to the 2 MPa isobar gives the isentropic end point $h_{3s} \approx 3010$ kJ/kg, so $$\Delta h_{s,\text{HP}} = 3412 - 3010 = 402.5\ \text{kJ/kg}$$ The internal efficiency shortens that drop, $$\Delta h_{\text{HP}} = 0.90 \times 402.5 = \boxed{362.2\ \text{kJ/kg}}$$ and the real end state sits at $h_3 = 3412 - 362.2 = 3050$ kJ/kg on the 2 MPa line. The 40 kJ/kg by which point 3 lies above point 3s is the frictional reheating the question refers to.
Part (b) — the high pressure turbine outlet conditions. Reading along the 2 MPa isobar at $h_3 = 3050$ kJ/kg, the state is still well superheated: $$\boxed{p_3 = 2\ \text{MPa}, \qquad t_3 \approx 311\ {}^\circ\text{C}}$$ (saturation at 2 MPa is 212.4 °C, so the steam leaves the HP cylinder with about 99 K of superheat and the cold reheat pipework carries no moisture).
Part (a) — the reheat and the low pressure expansion. Reheating at constant pressure to 500 °C moves the state up the 2 MPa isobar to $h_4 = 3468$ kJ/kg, $s_4 = 7.434$ kJ/kg·K. Dropping vertically to the 0.004 MPa isobar reaches the wet region at $h_{5s} \approx 2240$ kJ/kg, i.e. a quality of 0.871: $$\Delta h_{s,\text{LP}} = 3468 - 2240 = 1228.6\ \text{kJ/kg}, \qquad \Delta h_{\text{LP}} = 0.80 \times 1228.6 = \boxed{982.9\ \text{kJ/kg}}$$ so the real exhaust enthalpy is $h_5 = 3468 - 982.9 = 2485$ kJ/kg.
Part (c) — the low pressure turbine outlet conditions. At 0.004 MPa the saturation values are $h_f = 121.4$ kJ/kg and $h_{fg} = 2432.3$ kJ/kg, so the exhaust quality and moisture are $$x_5 = \frac{2485.3 - 121.4}{2432.3} = 0.972, \qquad \text{moisture} = 1 - x_5 = \boxed{2.8\ \%}$$ and, because the exhaust is a saturated mixture, its temperature is simply the saturation temperature at 0.004 MPa: $$\boxed{t_5 = 28.96\ {}^\circ\text{C}}$$ The exhaust is unusually dry for a condensing turbine precisely because the LP cylinder is only 80 % efficient — the losses reappear as enthalpy in the steam. Had the machine been isentropic the moisture would have been 12.9 %, which is past the usual erosion limit of about 12 %.
Part (d) — the power output. With no extraction the same 75 kg/s passes through both cylinders, so the two real enthalpy drops simply add: $$P = \dot m\,(\Delta h_{\text{HP}} + \Delta h_{\text{LP}}) = 75 \times (362.2 + 982.9)$$ $$P = 75 \times 1345.1 = \boxed{100\,880\ \text{kW} = 100.9\ \text{MW}}$$ As a cross-check on the heat side, the reheater has to supply $\dot m (h_4 - h_3) = 75 \times 418.3 = 31\,370$ kW, which is 31 % of the output — the usual proportion for a single reheat at this pressure ratio.