INLET SYSTEM FOR A GAS TURBINE
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United States of America Patent
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Issued Date -
Feb 9, 2017
app pub date -
Aug 7, 2015
filing date -
Aug 7, 2015
priority date (Note) -
Abandoned
status (Latency Note)
Importance
Abstract
An inlet system for a gas turbine includes an inlet duct, a silencer assembly disposed downstream from the inlet duct and an outlet duct disposed downstream from the silencer assembly. The silencer assembly may include a duct and a plurality of laterally spaced baffles disposed within the duct. The baffles may be arranged substantially parallel to a flow of air flowing through the inlet system. Each baffle includes a leading edge portion, a trailing edge portion that is longitudinally spaced from the leading edge portion and a pair of laterally opposing side walls that extend between the leading and trailing edges. Each baffle includes at least one acoustic panel that extends at least partially across one side wall of the pair of side walls.
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