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Gas Turbine Handbook : Principles and Practices

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2 <strong>Gas</strong> <strong>Turbine</strong> <strong>H<strong>and</strong>book</strong>: <strong>Principles</strong> <strong>and</strong> <strong>Practices</strong><br />

However, even in this period of unsuccessful attempts at producing a<br />

working prototype, progress was still being made.<br />

• In 1808 John Dumball envisioned a multi-stage turbine. Unfortunately<br />

his idea consisted only of moving blades without stationary<br />

airfoils to turn the flow into each succeeding stage. 1,3,4<br />

Had he realized the need for a stationary stage between each<br />

rotating stage he would have originated the concept of an axial<br />

flow turbine.<br />

• In Paris in 1837, Bresson’s idea was to use a fan to drive pressurized<br />

air into a combustion chamber. Here, the air was mixed<br />

with fuel gas <strong>and</strong> burnt. These combustion products were cooled<br />

by the addition of more air, <strong>and</strong> this final product was used to<br />

drive turbine blades. 1,2<br />

• In 1850, in Engl<strong>and</strong>, Fernimough suggested a mixed steam <strong>and</strong><br />

gas turbine, in which air was blown through a coal grate while<br />

water was sprayed into the hot gases. The gas <strong>and</strong> steam mixture<br />

then acted to drive a two-bladed rotor. 1<br />

• Not until 1872 did Dr. Franz Stolze combine the ideas of Barber<br />

<strong>and</strong> Dumball to develop the first axial compressor driven by an<br />

axial turbine. 1 Due to a lack of funds, he did not build his machine<br />

until 1900. Dr. Stolze’s design consisted of a multi-stage<br />

axial flow compressor, a single combustion chamber, a multistage<br />

axial turbine, <strong>and</strong> a regenerator utilizing exhaust gases to<br />

heat the compressor discharge air. This unit was tested between<br />

1900 <strong>and</strong> 1904, but never ran successfully.<br />

As will be discussed in Chapter IX, Bresson’s ideas are the basis<br />

of air cooling (to extend hot gas path part life), Fernimough’s ideas<br />

are the basis for water injection (for power augmentation <strong>and</strong> later<br />

NO x<br />

control), <strong>and</strong> Stolze’s ideas led the way for application of both<br />

the present day trends in gas turbine design <strong>and</strong> the regenerator for<br />

improved efficiency.<br />

It was not until 1884 with Sir Charles Parsons’ patent for a reaction<br />

steam turbine <strong>and</strong> gas turbine, <strong>and</strong> 1888, with Charles de Laval’s<br />

application of Giovanni Branca’s idea for an impulse steam turbine

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