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Combustion chambers

A combustion chamber can be ealeulated either based on kinetic theory (reaction rate equations) or a ehemical equilibrium constant. Knowledge about the exact value of partial pressures of the reactants is unnecessary this time, and simple calculations based on minimize of Gibbs free energy can be used. [Pg.142]

Usually, the combustion chamber works with a high ratio of oxidant (O2) to fuel, thus it can be assumed that all fuel is utihzed completely. In this case the combustion chamber model can be simplified to a mass and energy balance calculation for knowing the higher heating value (HHV) for a fuel. [Pg.142]

During off-design calculation, knowledge of the pressure drop across the combustion chamber is needed. The same relationships ean be used as for a heat exchanger model (see Eq. 5.46). [Pg.142]


Liquid injection incinerators. This t3q)e of incinerator has a cylindrical refractory-lined combustion chamber mounted verti-... [Pg.299]

Hearth incinerators. This type of incinerator is designed primarily to incinerate solid waste. Solids are moved through the combustion chamber mechanically using a rake. [Pg.300]

So//i/ fuels. Large coal-fired equipment normally uses pulverized fuel blown into the combustion chamber by a blast of air, similar to oil droplets. [Pg.70]

The diesel engine takes in and compresses the air. The fuel is injected into the cylinder in atomized form at the end of the compression stroke and is vaporized in the air. Ignition begins by auto-ignition in one or several zones in the combustion chamber where the conditions of temperature, pressure and concentration combine to enable combustion to start. [Pg.212]

The diesel engine operates, inherently by its concept, at variable fuel-air ratio. One easily sees that it is not possible to attain the stoichiometric ratio because the fuel never diffuses in an ideal manner into the air for an average equivalence ratio of 1.00, the combustion chamber will contain zones that are too rich leading to incomplete combustion accompanied by smoke and soot formation. Finally, at full load, the overall equivalence ratio... [Pg.212]

Moreover, a limit to maximum density is set in order to avoid smoke formation at full load, due to an increase in average equivalence ratio in the combustion chamber. [Pg.213]

For optimum combustion, the fuel should vaporize rapidly and mix intimately with the air. Even though the design of the injection system and combustion chamber play a very important role, properties such as volatility, surface tension, and fuel viscosity also affect the quality of atomization and penetration of the fuel. These considerations justify setting specifications for the density (between 0.775 and 0.840 kg/1), the distillation curve (greater than 10% distilled at 204°C, end point less than 288°C) and the kinematic viscosity (less than 8 mm /s at -20°C). [Pg.226]

In order to maintain high energy efficiency and ensure a long service life of the materials of construction in the combustion chamber, turbine and jet nozzle, a clean burning flame must be obtained that minimizes the heat exchange by radiation and limits the formation of carbon deposits. These qualities are determined by two procedures that determine respectively the smoke point and the luminometer index. [Pg.226]

Gasoline engine equipment such as carburetors, injectors, intake manifolds, valve systems and combustion chambers, are subject to fouling by the fuel itself, the gases recycled from the crankcase, or even dust and particulates arriving with poorly filtered air. Three types of problems then result ... [Pg.243]

Corrosion protection is indispensable, especially concerning certain vulnerable parts of the aircraft such as the combustion chamber and turbine. The potential hazards are linked to the presence of sulfur in various forms mercaptans, hydrogen sulfide, free sulfur, and sulfides. [Pg.251]

The Octane Requirement Increase, ORI, is a phenomenon manifested by the appearance of knocking and is due to the increase in engine octane demand with time. This phenomenon is correlated with the increase of solid deposits in the combustion chamber. Although the causes have not been determined with certainty, some companies have patented additives which modify the deposits. The effect is to limit the increase in octane demand (Bert et al., 1983 Chevron, 1988 Nelson et al., 1989). [Pg.347]

Moreover, the same surfactant structures that favor dispersion of fuel droplets in the combustion chamber most iikely play a role in reducing particulate emissions. (... [Pg.350]

Bert, J.A., J.A. Gething, T.J. Hansel, H.K. Newhall, R.J. Peyla and D.A. Voss (1983), A gasoline additive concentrate removes combustion chamber deposits and reduces vehicle octane requirement . SAE paper No. 83-1709, Fuels and Lubricants meeting, San Francisco, CA. [Pg.453]

Fig. 6. Cyclone furnace in effect a high, temperature, slag removal combustion chamber auxiliary to the gas-cooling boiler furnace. Fig. 6. Cyclone furnace in effect a high, temperature, slag removal combustion chamber auxiliary to the gas-cooling boiler furnace.
K. K. Boon, "A Flexible Mathematical Model for Analy2ing Industrial P. F. Furnaces," M.S. thesis. University of Newcasde, AustraUa, Sept. 1978. R. H. Essenhigh, "A New AppHcation of Perfectly Stirred Reactor (P.S.R.) Theory to Design of Combustion Chambers," TechnicalEeport FS67-1 (u), Peimsylvania State University, Dept, of Euel Science, University Park, Pa., Mar. 1967. [Pg.148]

Knock is caused by unwanted chemical reactions in the combustion chamber. These reactions are a function of the specific chemical species which make up the fuel and the environmental conditions to which the fuel is subjected during the compression and power stroke in the engine. Therefore, both the chemical makeup of the fuel and the engine design parameters must be considered when trying to understand knock. [Pg.179]

Vehicle Fa.ctors. Because knock is a chemical reaction, it is sensitive to temperature and reaction time. Temperature can in turn be affected either by external factors such as the wall temperature or by the amount of heat released in the combustion process itself, which is directiy related to the density of the fuel—air mixture. A vehicle factor which increases charge density, combustion chamber temperatures, or available reaction time promotes the tendency to knock. Engine operating and design factors which affect the tendency to produce knocking are... [Pg.180]

Sulfur. Sulfur in diesel fuel should be kept below set limits for both environmental and operational reasons. Operationally, high levels of sulfur can lead to high levels of corrosion and engine wear owing to emissions of SO that can react with condensed water during start-up to form sulfuric acids. From an environmental perspective, sulfur bums to SO2 and SO, the exact spHt being a function of temperature and time in the combustion chamber. [Pg.192]

Detergent Additives. Diesel engine deposits ate most troublesome in the fuel dehvery system, ie, the fuel pump and both fuel side and combustion side of the injectors. Small clearances and high pressures mean that even small amounts of deposits have the potential to cause maldistribution and poor atomization in the combustion chamber. The same types of additives used in gasoline ate used in diesel fuel. Low molecular weight amines can also provide some corrosion inhibition as well as some color stabilization. Whereas detergents have been shown to be effective in certain tests, the benefit in widespread use is not fully agreed upon (77). [Pg.193]


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Adiabatic-combustion chamber

And combustion chamber deposits

Burning chamber — combustion

Case = combustion chamber

Catalytic combustion chamber

Combustion chamber deposits

Combustion chamber deposits , gasoline engine

Combustion chamber deposits , gasoline engine fuels

Combustion chamber design

Combustion chamber length

Combustion chamber pressurization

Combustion chamber thermal performance

Combustion chamber, cyclone

Combustion chamber, fuel rich

Combustors combustion chamber design

Laboratory combustion chamber

Pressure drops Combustion chamber

Pressurized chamber, pulse combustion dryer

Primary combustion chamber

Pulse combustion pressurized-chamber

Reacting Flow in An Aircraft Combustion Chamber

Secondary combustion chamber

Standard combustion chamber

THERMODYNAMICS, COMBUSTION CHAMBER EQUILIBRIA AND FLAME TEMPERATURE

The Well-Stirred Combustion Chamber (WSCC) Model

The chamber length for complete combustion

Volume, constant, combustion chamber

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