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Otto Cycle Thermal Efficiency

1900
Otto cycle engine in a 1900 mechanical workshop, thermodynamics application.

(generated image for illustration only)

The thermal efficiency (\(\eta_{th}\)) of an ideal Otto cycle is a function of the compression ratio (\(r\)) and the specific heat ratio (\(\gamma\)) of the working fluid. The formula is \(\eta_{th} = 1 – \frac{1}{r^{\gamma-1}}\). This equation shows that efficiency increases with the compression ratio, providing a fundamental principle for engine design and performance optimization.

The derivation of the Otto cycle thermal efficiency formula begins with the general definition of thermal efficiency for any heat engine: \(\eta_{th} = \frac{W_{net}}{Q_{in}} = 1 – \frac{Q_{out}}{Q_{in}}\), where \(W_{net}\) is the net work output, \(Q_{in}\) is the heat added, and \(Q_{out}\) is the heat rejected. For the Otto cycle, heat is added at constant volume (process 2-3) and rejected at constant volume (process 4-1). Therefore, \(Q_{in} = m c_v (T_3 – T_2)\) and \(Q_{out} = m c_v (T_4 – T_1)\), where \(m\) is the mass of the working fluid, \(c_v\) is the specific heat at constant volume, and \(T\) represents the temperature at the numbered states of the cycle.

Substituting these into the efficiency equation gives \(\eta_{th} = 1 – \frac{T_4 – T_1}{T_3 – T_2}\). To simplify this in terms of volumes, we use the relationships for the isentropic processes (1-2 and 3-4). For an isentropic process, \(TV^{\gamma-1} = \text{constant}\). Thus, \(\frac{T_2}{T_1} = (\frac{V_1}{V_2})^{\gamma-1} = r^{\gamma-1}\) and \(\frac{T_3}{T_4} = (\frac{V_4}{V_3})^{\gamma-1} = r^{\gamma-1}\). This implies \(\frac{T_2}{T_1} = \frac{T_3}{T_4}\) or \(\frac{T_4}{T_1} = \frac{T_3}{T_2}\). Rearranging the efficiency equation to \(\eta_{th} = 1 – \frac{T_1(T_4/T_1 – 1)}{T_2(T_3/T_2 – 1)}\) and substituting the temperature ratio equality, the terms in the parentheses cancel out. This leaves \(\eta_{th} = 1 – \frac{T_1}{T_2}\). Finally, using the isentropic relation \(\frac{T_1}{T_2} = (\frac{V_2}{V_1})^{\gamma-1} = \frac{1}{r^{\gamma-1}}\), we arrive at the final formula: \(\eta_{th} = 1 – \frac{1}{r^{\gamma-1}}\).

UNESCO Nomenclature: 2212
– Thermodynamics

Type

Formula

Disruption

Foundational

Usage

Widespread Use

Precursors

  • Sadi Carnot’s work on heat engine efficiency
  • Rudolf Clausius’s formulation of the second law of thermodynamics
  • concept of specific heat capacities (cv and cp)
  • ideal gas law
  • mathematical description of adiabatic (isentropic) processes

Applications

  • engine design and optimization
  • performance comparison of different fuels
  • development of high-compression engines
  • turbocharging and supercharging analysis
  • automotive engineering education

Patents:

NA

Potential Innovations Ideas

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Related to: thermal efficiency, compression ratio, specific heat ratio, Otto cycle, thermodynamics, engine performance, isentropic process, ideal gas law, heat engine, automotive engineering.

Historical Context

Otto Cycle Thermal Efficiency

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1900-12-14
1902
1904

(if date is unknown or not relevant, e.g. "fluid mechanics", a rounded estimation of its notable emergence is provided)

Related Invention, Innovation & Technical Principles

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