Turbine air flow conditioner
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United States of America Patent
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Oct 31, 2017
Issued Date -
N/A
app pub date -
Jun 24, 2014
filing date -
Jun 24, 2014
priority date (Note) -
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Abstract
A turbine combustor section has a flow conditioner including a plurality of conduits arranged to convey pressurized air to an air chamber for entrance into a plurality of fuel nozzles. Each conduit includes an inlet configured to receive the pressurized air from an annular passage and an outlet configured to deliver the pressurized air to the air chamber. A cross-sectional area of each conduit varies between the inlet and the outlet so as to reduce a pressure drop across the flow conditioner.
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