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Define the compression ratio for reciprocating engines.

Short Answer

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Answer: The compression ratio of a reciprocating engine is a fundamental characteristic that specifies the ratio of the volume of the combustion chamber when the piston is at its lowest point (Bottom Dead Center, BDC) to the volume when the piston is at its highest point (Top Dead Center, TDC). It can be calculated using the formula: CR = V_BDC/V_TDC where CR represents the compression ratio, V_BDC denotes the volume of the combustion chamber with the piston at BDC (including the clearance volume), and V_TDC denotes the volume of the combustion chamber with the piston at TDC (clearance volume). To calculate the compression ratio, first identify the volumes of the combustion chamber at BDC and TDC from engine specifications or engine geometry, and then divide the volume at BDC by the volume at TDC.

Step by step solution

01

Definition of Compression Ratio

The compression ratio (CR) is a fundamental characteristic of reciprocating engines that specifies the ratio of the volume of the combustion chamber when the piston is at its lowest point (Bottom Dead Center, BDC) to the volume when the piston is at its highest point (Top Dead Center, TDC). In mathematical terms, it can be represented as: CR = V_BDC/V_TDC where CR represents the compression ratio, V_BDC denotes the volume of the combustion chamber with the piston at BDC (including the clearance volume), and V_TDC denotes the volume of the combustion chamber with the piston at TDC (clearance volume).
02

Identify the volumes of the combustion chamber at BDC and TDC

To determine the compression ratio, first identify the volume of the combustion chamber when the piston is at BDC and TDC. These values can be found in engine specifications or calculated from engine geometry.
03

Calculate the compression ratio

Once you have the volumes of the combustion chamber at BDC and TDC, you can calculate the compression ratio using the formula mentioned above: CR = V_BDC/V_TDC By dividing the volume at BDC by the volume at TDC, you will obtain the compression ratio for the reciprocating engine. The compression ratio is a crucial parameter for engine performance, efficiency, and emissions. A higher compression ratio generally improves thermal efficiency, but could also lead to increased risks of engine knocking.

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Most popular questions from this chapter

An air-standard cycle, called the dual cycle, with constant specific heats is executed in a closed piston-cylinder system and is composed of the following five processes: \(1-2 \quad\) Isentropic compression with a compression ratio \(r=V_{1} / V_{2}\) \(2-3 \quad\) Constant volume heat addition with a pressure ratio, \\[ r_{p}=P_{3} / P_{2} \\] \(3-4 \quad\) Constant pressure heat addition with a volume ratio \\[ r_{c}=V_{4} / V_{3} \\] \(4-5 \quad\) Isentropic expansion while work is done until \(V_{5}=V_{1}\) \(5-1 \quad\) Constant volume heat rejection to the initial state (a) Sketch the \(P\) -V and \(T\) -s diagrams for this cycle. (b) Obtain an expression for the cycle thermal efficiency as a function of \(k, r, r_{c},\) and \(r_{p}\) (c) Evaluate the limit of the efficiency as \(r_{p}\) approaches unity and compare your answer with the expression for the Diesel cycle efficiency. (d) Evaluate the limit of the efficiency as \(r_{c}\) approaches unity and compare your answer with the expression for the Otto cycle efficiency.

An ideal Otto cycle with air as the working fluid has a compression ratio of \(8 .\) The minimum and maximum temperatures in the cycle are 540 and 2400 R. Accounting for the variation of specific heats with temperature, determine ( \(a\) ) the amount of heat transferred to the air during the heat-addition process, \((b)\) the thermal efficiency, and \((c)\) the thermal efficiency of a Carnot cycle operating between the same temperature limits.

Helium is used as the working fluid in a Brayton cycle with regeneration. The pressure ratio of the cycle is 8 the compressor inlet temperature is \(300 \mathrm{K},\) and the turbine inlet temperature is \(1800 \mathrm{K}\). The effectiveness of the regenerator is 75 percent. Determine the thermal efficiency and the required mass flow rate of helium for a net power output of \(60 \mathrm{MW},\) assuming both the compressor and the turbine have an isentropic efficiency of \((a) 100\) percent and \((b) 80\) percent.

The compression ratio of an ideal dual cycle is 14. Air is at \(100 \mathrm{kPa}\) and \(300 \mathrm{K}\) at the beginning of the compression process and at \(2200 \mathrm{K}\) at the end of the heat-addition process. Heat transfer to air takes place partly at constant volume and partly at constant pressure, and it amounts to \(1520.4 \mathrm{kJ} / \mathrm{kg} .\) Assuming variable specific heats for air, determine \((a)\) the fraction of heat transferred at constant volume and \((b)\) the thermal efficiency of the cycle.

When we double the compression ratio of an ideal Otto cycle, what happens to the maximum gas temperature and pressure when the state of the air at the beginning of the compression and the amount of heat addition remain the same? Use constant specific heats at room temperature.

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