Chapter 9: Problem 6
How is the mean effective pressure for reciprocating engines defined?
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Key Concepts
These are the key concepts you need to understand to accurately answer the question.
Chapter 9: Problem 6
How is the mean effective pressure for reciprocating engines defined?
These are the key concepts you need to understand to accurately answer the question.
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Get started for freeA four-cylinder, four-stroke spark-ignition engine operates on the ideal Otto cycle with a compression ratio of 11 and a total displacement volume of 1.8 liter. The air is at \(90 \mathrm{kPa}\) and \(50^{\circ} \mathrm{C}\) at the beginning of the compression process. The heat input is \(1.5 \mathrm{kJ}\) per cycle per cylinder. Accounting for the variation of specific heats of air with temperature, determine \((a)\) the maximum temperature and pressure that occur during the cycle, \((b)\) the net work per cycle per cyclinder and the thermal efficiency of the cycle, \((c)\) the mean effective pressure, and \((d)\) the power output for an engine speed of \(3000 \mathrm{rpm}\)
An ideal diesel engine has a compression ratio of 20 and uses air as the working fluid. The state of air at the beginning of the compression process is \(95 \mathrm{kPa}\) and \(20^{\circ} \mathrm{C}\). If the maximum temperature in the cycle is not to exceed \(2200 \mathrm{K}\) determine \((a)\) the thermal efficiency and \((b)\) the mean effective pressure. Assume constant specific heats for air at room temperature.
Develop an expression for the thermal efficiency of an ideal Brayton cycle with an ideal regenerator of effectiveness 100 percent. Use constant specific heats at room temperature.
A gas turbine operates with a regenerator and two stages of reheating and intercooling. This system is designed so that when air enters the compressor at \(100 \mathrm{kPa}\) and \(15^{\circ} \mathrm{C}\) the pressure ratio for each stage of compression is \(3 ;\) the air temperature when entering a turbine is \(500^{\circ} \mathrm{C} ;\) and the regenerator operates perfectly. At full load, this engine produces \(800 \mathrm{kW} .\) For this engine to service a partial load, the heat addition in both combustion chambers is reduced. Develop an optimal schedule of heat addition to the combustion chambers for partial loads ranging from 400 to \(800 \mathrm{kW}\)
An ideal Stirling cycle filled with air uses a \(75^{\circ} \mathrm{F}\) energy reservoir as a sink. The engine is designed so that the maximum air volume is \(0.5 \mathrm{ft}^{3},\) the minimum air volume is \(0.06 \mathrm{ft}^{3},\) and the minimum pressure is 15 psia. It is to be operated such that the engine produces 2 Btu of net work when 5 Btu of heat are transferred externally to the engine. Determine the temperature of the energy source, the amount of air contained in the engine, and the maximum air pressure during the cycle.
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