GAS TURBINE ENGINE INCLUDING PNEUMATIC ACTUATOR SYSTEM
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United States of America Patent
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Issued Date -
Oct 9, 2014
app pub date -
Feb 6, 2014
filing date -
Apr 8, 2013
priority date (Note) -
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Abstract
A gas turbine engine that includes a compressor section and a pneumatic actuator system is delivered. The pneumatic actuator system includes a bleed air duct that receives bleed air from the compressor section and delivers the bleed air through an accumulator and to an actuator. The accumulator includes a chamber that attenuates a fluctuation in a pressure of the bleed air.
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