ADJUSTMENT SYSTEM FOR A COMPRESSOR
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United States of America Patent
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Issued Date -
Aug 15, 2024
app pub date -
Feb 12, 2024
filing date -
Feb 15, 2023
priority date (Note) -
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status (Latency Note)
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Abstract
The invention relates to an adjustment system for a compressor in a gas turbine, in particular in an aircraft gas turbine, for the adjustment of adjustable guide vanes, including an actuator device with a first actuator for the adjustment of the guide vanes and an adjusting device with a first adjusting valve for the hydraulic operation of the first actuator, wherein the adjusting device can adjust and lock in position the first actuator by way of the hydraulic operation, is characterized in that the actuator device is assigned a locking device for additional fixation and can be fixed in a position by the locking device.
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