Asymmetric load compensation system
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United States of America Patent
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Apr 24, 2018
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N/A
app pub date -
Apr 15, 2015
filing date -
Apr 15, 2015
priority date (Note) -
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Abstract
This disclosure relates to a variable area nozzle of a gas turbine engine. The variable area nozzle includes, among other things, a control unit, a translatable structure, and a plurality of actuators configured to adjust the position of the translatable structure. The plurality of actuators are fluidly coupled to a common fluid source. The control unit is configured to provide instructions to at least one of the actuators to compensate for an asymmetric load from the translatable structure.
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