Air leaving the compressor is split into a number of separate streams each

Air leaving the compressor is split into a number of

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made use of can (or tubular) combustors . Air leaving the compressor is split into a number of separate streams, each supplying a separate chamber. These chambers are spaced around the shaft connecting the compressor and turbine, each chamber having its own fuel jet fed from a common supply line . Well suited to engines with centrifugal compressors, where the flow is divided into separate streams in the diffuser.
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2. Tubo-annular- Individual flame tubes are uniformly spaced around an annular casing. Uses a reverse flow arrangement which allows a significant reduction in the overall length of the compressor-turbine shaft.
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3. Silo type- Large industrial gas turbines, where the space required by the combustion system is less critical, have used one or two large cylindrical combustion chambers . These large combustors allowed lower fluid velocities and hence pressure losses, and were capable of burning lower quality fuels .
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Manik singh jamwal(17bme022) Rajat sharma (17bme024) Anmol singh (17bm033) Presented by -: T H A N K Y O U
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