TURBINE SYSTEM
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United States of America Patent
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Issued Date -
Mar 10, 2016
app pub date -
Sep 5, 2014
filing date -
Sep 5, 2014
priority date (Note) -
Abandoned
status (Latency Note)
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Abstract
A turbine system including a compressor (3), a combustor arrangement having several combustors (4) fluidicallys connected to receive air from the compressor (3), and a turbine (5) fluidically connected to the combustors (4). Each combustor (4) has an air inlet ring chamber (7) with a flow cross-section defined by an inner tube (10) and an outer tube (11; 17) around the inner tube. The air inlet ring chamber is configured to introduce compressed air from the compressor (3) into the combustor (4). A radial distance (d) between the inner tube (10) and the outer tube (11; 17) of each air inlet ring chamber (7) at least partially varies along the circumference of the air inlet ring chamber (7).
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