Detection of fan case liner damage during turbine engine operation
AssigneeGulfstream Aerospace Corporation
InventorsVincent DeChellis, Mike Lucas, Tongan Wang, Nicholas Ward, Paul Conti
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AssigneeGulfstream Aerospace Corporation
InventorsVincent DeChellis, Mike Lucas, Tongan Wang, Nicholas Ward, Paul Conti
Estimating the term…
An aircraft includes a turbine engine, a vibration sensor, and a processor. The vibration sensor is attached to the turbine engine and is configured to output a vibration sensor signal. The processor is programmed to determine whether the vibration sensor signal indicates that fan case liner damage has occurred due to icing conditions. The processor is further programmed to indicate that a fan case inspection should be conducted in response to the vibration sensor signal indicating that fan case liner damage has occurred.
An aircraft, comprising:
A device for damage monitoring of a turbine engine having a fan case with a fan case liner, the device comprising:
A device for damage monitoring of a turbine engine having a fan case with a fan case liner, the device comprising:
Dependencies are inferred from the claim text.