General Electric Company

Christopher Warren Childs

Robert Joseph Iasillo

Matthew John McKeever

Gregory Allan Crum

Sanjeev Shyam Heda

Steven William Backman

Scott Alan Wood

Karol Filip Leszczynski

Carlo Angelo Yon

Mitchel Merck

Alexander Maxim Libers

Horacio Repetto

David Matthew Clarida

A seal retaining assembly includes a first segment coupled to a first structure. Also included is a recess of the first segment, the recess defined by a first and second wall, the first wall defining a first wall aperture, the second wall defining a second wall aperture. Further included is a second segment having a tab disposed within the recess in fitted contact with the first and second wall to retain the second segment to the first segment in a radial direction, the tab defining a tab aperture, the first and second segment defining an axial gap therebetween, the first wall aperture, the second wall aperture and the tab aperture are aligned to form a passage. Yet further included is a flex seal within the axial gap. Also included is a pin in the passage to fix the second segment to the first segment in axial and circumferential directions.

Seal retaining assembly

A system for remote detection of surge in a fleet of turbine engines includes an on-site monitoring device coupled to each turbine engine of the fleet of turbine engines. The on-site monitoring device is configured to continuously receive operating parameter measurements indicative of operational and thermodynamic conditions of the turbine engine. The operational condition includes a compressor exit condition of the turbine engine compressor. The on-site monitoring device is configured to compile and transmit a snapshot of the operating parameter measurements to a remote monitoring unit. The remote monitoring unit is positioned remote from each turbine engine of the fleet of turbine engines. The remote monitoring unit is configured to receive the snapshot of operating parameter measurements from the on-site monitoring device. The remote monitoring unit is further configured to detect surge in the turbine engine based on analysis of the snapshot of operating parameter measurements.

Method and systems for detection of compressor surge

Systems and methods for continuous pressure change monitoring in turbine compressors. In one embodiment, a system can be provided. The system can include a dynamic pressure sensing device mounted to the turbine compressor. The dynamic pressure sensing device may be configured to provide continuous dynamic pressure data, which may be associated with one or more pressure change events. The system may further include a memory configured to store the continuous dynamic pressure data, and a processor configured to correlate the one or more pressure change events with one or more component failures of the turbine compressor, and, based at least in part on the correlation, diagnose the one or more component failures.

Systems and methods for continuous pressure change monitoring in turbine compressors

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Marietta, GA, United States of America

Christopher Warren Childs