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Modern Engineering Thermodynamics

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Problems 533<br />

72. Determine the value of the cutoff ratio that causes the Diesel<br />

cold ASC thermal efficiency to become zero for an engine with a<br />

20.0 to 1 compression ratio. Assume k=1.40.<br />

73. A Diesel cycle internal combustion engine has a compression<br />

ratio of 15.0 to 1. At the beginning of the compression process,<br />

the pressure is 14.7 psia and the temperature is 520. R. The<br />

maximum temperature of the cycle is 4868 R. Determine the<br />

cold ASC thermal efficiency. Assume k=1.40.<br />

74.* A two-cylinder, two-stroke Diesel cycle internal combustion<br />

engine with a 16.2 to 1 compression ratio and a total<br />

displacement of 1.50 L burns kerosene having a heating value<br />

of 40.0 × 10 3 kJ/kg when using an air–fuel ratio of 25.0 to 1.<br />

The intake temperature and pressure are 100. kPa and 15.0°C.<br />

When the engine is running at 1200. rpm and producing<br />

6.00 kW of power, determine (assuming k=1.40) the engine’s<br />

a. Cutoff ratio.<br />

b. Cold ASC thermal efficiency.<br />

c. Indicated power output.<br />

d. Mechanical efficiency.<br />

e. Actual thermal efficiency.<br />

75. The Atkinson cycle is similar to the Otto cycle except that the<br />

constant volume exhaust-intake stroke at the end of the Otto<br />

cycle power stroke has been replaced by a constant pressure<br />

process in the Atkinson cycle, as shown in Figure 13.70. Q H<br />

occurs during process 4s to 1, and Q L occurs during process 2s<br />

to 3 in each case.<br />

a. Sketch the T–s diagram for the Atkinson cycle numbering<br />

and labeling all the process path lines as in the p−V diagram<br />

of Figure 13.70.<br />

b. Determine the Atkinson cold ASC thermal efficiency for<br />

k=1.40, T 1 = 8000. R, T 3 = 520. R, and CR = v 3 /v 4s = 8.0.<br />

Design Problems<br />

The following are open-ended design problems. The objective is to<br />

carry out a preliminary thermal design as indicated. A detailed design<br />

with working drawings is not expected unless otherwise specified.<br />

These problems have no specific answers, so each student’s design is<br />

unique.<br />

76. Design a small, single-cylinder, piston-type steam engine and<br />

boiler that can be used to power a toy vehicle, such as a train or<br />

a tractor. Choose a convenient fuel such as alcohol, and design<br />

the boiler so that it can supply enough steam to your engine.<br />

Make sure the boiler has a pressure relief valve, and pay close<br />

attention to other safety considerations.<br />

77. Develop a preliminary design for a closed loop Rankine cycle<br />

steam power plant to be used in a compact automobile. The<br />

prime mover may be either a reciprocating piston or turbine and<br />

must produce a net output of 40.0 hp with a thermal efficiency<br />

in excess of 35.0%.<br />

a. Specify inlet and outlet states for the boiler, prime mover,<br />

condenser, and boiler feed pump.<br />

b. Choose typical values for the isentropic efficiencies of the<br />

prime mover and boiler feed pump, and calculate the overall<br />

thermal efficiency of the power plant.<br />

c. Specify the fuel to be used in the boiler.<br />

d. Estimate the overall power plant weight, including fuel<br />

storage.<br />

e. Specify conditions needed to meet part-load operation and<br />

prime mover speed control during vehicle acceleration and<br />

deceleration.<br />

f. Specify all additional equipment needed to connect the<br />

prime mover output shaft to the vehicle drive wheels.<br />

78. Design a small, single-cylinder Stirling or Ericsson cycle external<br />

combustion engine that can be used to demonstrate the<br />

operation of this type of engine in the classroom. Choose a<br />

convenient fuel such as alcohol. Provide detailed working<br />

drawings and a thermodynamic analysis.<br />

79. Design a Brayton cycle power system to propel a small drone<br />

aircraft that will be used for military target practice. The fueled<br />

drone must weigh less than 500. kg, and since these aircraft are<br />

not reusable, they must be produced at minimum cost.<br />

Determine or specify the air mass flow rate, pressure ratio,<br />

compressor and turbine isentropic efficiencies, turbine inlet<br />

temperature, thrust, thrust to weight ratio, exhaust temperature,<br />

and hot ASC thermal efficiency. A computer program will help<br />

you carry out parametric studies of the variables involved.<br />

80. Design a personal exercise machine that uses the otherwise<br />

dissipated human exercise energy in some productive way.<br />

For example, the exercise energy could be converted into<br />

mechanical, chemical, or electrical energy, which could then<br />

be used in some domestic device (for example, to power a<br />

computer, TV set, or kitchen appliance). Another solution would<br />

be to design a system that would feed the exercise energy<br />

directly into the local electrical power grid for credit against the<br />

1<br />

1<br />

s = c<br />

p<br />

4s<br />

V = c<br />

s = c<br />

2s<br />

V = c<br />

3<br />

p<br />

V = c<br />

s = c<br />

4s<br />

s = c<br />

3<br />

p = c<br />

2s<br />

V<br />

Otto cycle<br />

V<br />

Atkinson cycle<br />

FIGURE 13.70<br />

Problem 75.

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