Allan T. Kirkpatrick - Internal Combustion Engines

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Internal Combustion Engines: краткое содержание, описание и аннотация

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A comprehensive resource covering the foundational thermal-fluid sciences and engineering analysis techniques used to design and develop internal combustion engines Internal Combustion Engines: Applied Thermosciences, Fourth Edition This new 4th edition includes brand new material on: 
New engine technologies and concepts Effects of engine speed on performance and emissions Fluid mechanics of intake and exhaust flow in engines Turbocharger and supercharger performance analysis Chemical kinetic modeling, reaction mechanisms, and emissions Advanced combustion processes including low temperature combustion Piston, ring and journal bearing friction analysis The 
 expands on the combined analytical and numerical approaches used successfully in previous editions. Students and engineers are provided with several new tools for applying the fundamental principles of thermodynamics, fluid mechanics, and heat transfer to internal combustion engines. 
Each chapter includes MATLAB programs and examples showing how to perform detailed engineering computations. The chapters also have an increased number of homework problems with which the reader can gauge their progress and retention. All the software is ‘open source’ so that readers can see in detail how computational analysis and the design of engines is performed. A companion website is also provided, offering access to the MATLAB computer programs.

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Figure 27The Miller cycle For late inlet valve closing a portion of the - фото 395

Figure 2.7The Miller cycle.

For late inlet valve closing, a portion of the intake air is pushed back into the intake manifold before the intake valve closes at point 1. Once the inlet valve closes, there is less mixture to compress in the cylinder, and thus less compression work.

Performing a first‐law analysis of the Miller cycle, we first define the parameter, картинка 396, the ratio of the expansion ratio to the compression ratio:

(2.34) The energy rejection has two components 235 As detailed in Example 22 - фото 397

The energy rejection has two components

(2.35) As detailed in Example 22 below the thermal efficiency is 236 Equation - фото 398

As detailed in Example 2.2 below, the thermal efficiency is

(2.36) Equation 236 reduces to the Otto cycle thermal efficiency as Also - фото 399

Equation ( 2.36) reduces to the Otto cycle thermal efficiency as Also detailed in Example 22 the imep is 237 The thermal efficiency of - фото 400. Also detailed in Example 2.2, the imep is

(2.37) The thermal efficiency of the Miller cycle is not only a function of the - фото 401

The thermal efficiency of the Miller cycle is not only a function of the compression ratio and specific heat ratio but also a function of the expansion ratio and the load картинка 402. The ratio of the Miller cycle thermal efficiency to an equivalent Otto cycle efficiency with the same compression ratio is plotted in Figure 2.8for a range of compression ratios and картинка 403values. With values of and the Miller cycle is about 20 more efficient than the Otto cycle - фото 404and the Miller cycle is about 20 more efficient than the Otto cycle Figure - фото 405, the Miller cycle is about 20% more efficient than the Otto cycle.

Figure 28Ratio of Miller to Otto cycle thermal efficiency with same - фото 406

Figure 2.8Ratio of Miller to Otto cycle thermal efficiency with same compression ratio, картинка 407( картинка 408).

The ratio of the Miller/Otto cycle imep is plotted as a function of картинка 409in Figure 2.9. As картинка 410increases, the imep decreases significantly, since the fraction of the displacement volume картинка 411that is filled with the inlet fuel–air mixture decreases. This relative decrease in imep and engine power is a disadvantage of the Miller cycle, which is the reason supercharging of the inlet mixture or increase of the overall engine displacement volume is used to increase the imep.

Figure 29Ratio of Miller to Otto cycle imep with same compression ratio - фото 412

Figure 2.9Ratio of Miller to Otto cycle imep with same compression ratio, картинка 413( картинка 414).

A related cycle, the Atkinson cycle, is one in which the expansion stroke continues until the cylinder pressure at point 4 decreases to atmospheric pressure. This cycle is named after James Atkinson (1846–1914), an English engineer, who invented and built an engine he named the картинка 415engine in 1889. This engine had a two‐bar linkage between the connecting rod and the crankshaft so that the piston traveled through four unequal strokes in every crankshaft revolution. The expansion to intake stroke ratio was 1.78:1. Honda (Takita et al. 2011) has recently produced an Atkinson cycle engine by adding a trigonal link, swing rod, and eccentric shaft to a conventional connecting rod and crankshaft assembly. The engine is used in a micro combined heat and power generation (CHP) application. The engine картинка 416, with an expansion ratio картинка 417and compression ratio of картинка 418. The brake thermal efficiency is 26.3% compared to 22.5% for a conventional engine.

Example 2.2 Miller Cycle Analysis

Derive the equations for the Miller cycle efficiency, Equation ( 2.36), and the Miller cycle imep, Equation ( 2.37).

Solution

We need to write картинка 419and imep as a function of and Using a state by state cycle analysis 1 Miller cycle efficiency - фото 420and Using a state by state cycle analysis 1 Miller cycle efficiency - фото 421. Using a state by state cycle analysis,

1 Miller cycle efficiency derivationSolving for efficiency 2 Miller cycle - фото 422

1 Miller cycle efficiency derivation:Solving for efficiency:

2 Miller cycle imep derivation:

2.7 Ideal Four‐Stroke Process and Residual Fraction

The simple gas cycle models assume that the heat rejection process occurs at constant volume, and neglect the gas flow that occurs when the intake and exhaust valves are opened and closed. In this section, we use the energy equation to model the exhaust and intake strokes, and determine the residual fraction of gas remaining in the cylinder.

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