ACTUATED BYPASS HOOD FOR GAS TURBINE AIR INLET SYSTEM AND METHODS
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United States of America Patent
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Issued Date -
May 8, 2014
app pub date -
Feb 25, 2013
filing date -
Nov 8, 2012
priority date (Note) -
Abandoned
status (Latency Note)
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Abstract
An inlet hood for use with a gas turbine or compressor air inlet system includes a frame and at least one pre-filter pivotably held by the frame in an operating position. The pre-filter is pivotable to a bypass position angled relative to the operating position. Methods of assembly and use are provided.
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