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公开(公告)号：US11305894B2
公开(公告)日：2022-04-19
申请号：US16697929
申请日：2019-11-27
Applicant: Gulfstream Aerospace Corporation
Inventor： Vincent DeChellis , Mike Lucas , Tongan Wang , Nicholas Ward , Paul Conti
Abstract: 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.
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公开(公告)号：US20200172269A1
公开(公告)日：2020-06-04
申请号：US16697929
申请日：2019-11-27
Applicant: Gulfstream Aerospace Corporation
Inventor： Vincent DeChellis , Mike Lucas , Tongan Wang , Nicholas Ward , Paul Conti
Abstract: 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.
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