Combustion chamber structure of gas turbine
A gas turbine and combustor technology, which is applied in gas turbine devices, combustors, continuous combustors, etc., can solve problems such as reducing turbine efficiency
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[0022] In these figures, the same parts are provided with the same reference numerals.
[0023] figure 1 A partially cutaway perspective view of a combustion chamber arrangement 1 according to the invention is shown. A plurality of separate combustion chambers 2 arranged substantially in the shape of a circle and of cylindrical configuration open into a common annular combustion chamber 3 . The annular combustion chamber 3 has a double-shell housing with an outer shell 8 and an inner shell 6 . The casing of discrete combustion chamber also all has double shell structure, has corresponding inner shell 5 and outer shell 7 (see figure 2 ). In order to operate a gas turbine equipped with a combustor structure 1 according to the invention, an air / fuel mixture is fed into each separate combustor 2 where it is ignited. In a first phase, the combustion then takes place in the individual combustion chambers 2 , but then also continues into the common annular combustion chamber 3 ....
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