Product Design, Manufacturing & Innovation Resources
» 奥托循环热效率

奥托循环热效率

1900
1900 年机械车间的奥托循环发动机,热力学应用。.

(图片仅供参考)

The thermal efficiency ([latex]\eta_{th}[/latex]) of an ideal Otto cycle is a function of the compression ratio ([latex]r[/latex]) and the specific heat ratio ([latex]\gamma[/latex]) of the working fluid. The formula is [latex]\eta_{th} = 1 – \frac{1}{r^{\gamma-1}}[/latex]. 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: [latex]\eta_{th} = \frac{W_{net}}{Q_{in}} = 1 – \frac{Q_{out}}{Q_{in}}[/latex], where [latex]W_{net}[/latex] is the net work output, [latex]Q_{in}[/latex] is the heat added, and [latex]Q_{out}[/latex] 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, [latex]Q_{in} = m c_v (T_3 – T_2)[/latex] and [latex]Q_{out} = m c_v (T_4 – T_1)[/latex], where [latex]m[/latex] is the mass of the working fluid, [latex]c_v[/latex] is the specific heat at constant volume, and [latex]T[/latex] represents the temperature at the numbered states of the cycle.

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

UNESCO Nomenclature: 2212
- 热力学

类型

计算公式

中断

基础

用法

广泛使用

前体

  • Sadi Carnot’s work on heat engine efficiency
  • 鲁道夫-克劳修斯对热力学第二定律的表述
  • 比热容(cv 和 cp)的概念
  • 理想气体定律
  • 绝热(等熵)过程的数学描述

应用程序

  • 发动机设计与优化
  • 不同燃料的性能比较
  • 高压缩比发动机的研发
  • 涡轮增压和机械增压分析
  • 汽车工程教育

专利:

NA

潜在创新理念

由于机器人流量被拦截(目前每天超过 4 万),此内容仅限社区成员查看。
> 登录 > 或者 > 注册 < (100% 免费)即可访问此内容,以及所有其他受限内容和工具。

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

历史背景

奥托循环热效率

1900
1900
1900
1900
1900
1902
1902
1900
1900
1900
1900
1900
1900-12-14
1902
1904

(如果日期未知或不相关,例如“流体力学”,则提供其显著出现的近似估计)

相关发明、创新和技术原理

只有注册会员才能免费获得 100% 的全尺寸图片和下载。.

> 登录 <