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Gas Turbine Combustion: Alternative Fuels and Emissions (3rd by Arthur H. Lefebvre, Dilip R. Ballal

By Arthur H. Lefebvre, Dilip R. Ballal

Publish yr note: First released in 1983

Reflecting the advancements in fuel turbine combustion expertise that experience happened within the final decade, fuel Turbine Combustion replacement Fuels and Emissions, 3rd version presents an updated layout handbook and examine reference at the layout, manufacture, and operation of gasoline turbine combustors in purposes starting from aeronautical to strength iteration. primarily self-contained, the ebook basically calls for a reasonable volume of earlier wisdom of physics and chemistry.

In reaction to the fluctuating price and environmental results of petroleum gasoline, this 3rd version incorporates a new bankruptcy on replacement fuels. This bankruptcy offers the actual and chemical houses of traditional (petroleum-based) liquid and gaseous fuels for fuel generators; studies the houses of other (synthetic) fuels and conventional-alternative gas blends; and describes the effect of those diversified fuels and their blends on combustor functionality, layout, and emissions. It additionally discusses the particular requisites of airplane fuels and the issues encountered with fuels for business fuel generators. within the up-to-date bankruptcy on emissions, the authors spotlight the hunt for greater gas potency and decreasing carbon dioxide emissions in addition to the rules involved.

Continuing to provide specified assurance of multifuel services, flame flashback, excessive off-design combustion potency, and liner failure stories, this best-selling ebook is the leading consultant to fuel turbine combustion know-how. This variation keeps the fashion that made its predecessors so well known whereas updating the cloth to mirror the expertise of the twenty-first century. (less)

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Extra info for Gas Turbine Combustion: Alternative Fuels and Emissions (3rd Edition)

Example text

23 General Electric conventional industrial combustor. One of the most successful industrial units in the first category is the 80 MW GE MS7001 gas turbine. Each machine has ten sets of combustion hardware, and each set comprises a casing, an end cover, a set of fuel nozzles, a flow sleeve, a combustion liner, and a transition piece. 23. The flow sleeve is an axisymmetric cylinder/cone that surrounds much of the combustion liner to aid in distributing the compressor air uniformly to all liners and to improve the external liner-wall cooling [3].

A combustion wave) can propagate through a static gas mixture, it is usual to stabilize the flame at a fixed point and supply it with a continuous flow of combustible mixture. Under these conditions, flames can be divided into two main ­classes— premixed flames and diffusion flames—depending on whether the fuel and air are mixed before combustion, or mixed by diffusion in the flame zone. Depending on the prevailing flow velocities, both types of flame can be further classified as laminar or turbulent.

Their drawbacks include potential plugging of the small passages and orifices by contaminants in the fuel and an innate tendency toward high soot formation at high-combustion pressures. 2 Airblast Atomizer This atomizer employs a simple concept whereby fuel at low pressure is arranged to flow over a lip located in a high-velocity airstream. As the fuel flows over the lip it is atomized by the air, which then enters the combustion zone carrying the fuel droplets along with it. Minimum drop sizes are obtained by using designs that provide maximum physical contact between 20 Gas Turbine Combustion: Alternative Fuels and Emissions, Third Edition the air and the liquid.

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