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US 11,028,719 B2Granted
Brush seal repair method
AssigneeRaytheon Technologies Corporation
InventorsDavid E. Walker, Steven M. Cote
Life of this patent
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Abstract
A method of working a brush seal assembly for a turbine engine is disclosed and includes the steps of removing an alignment tab from a used brush seal assembly, restoring at least one dimension of the alignment tab to a desired condition and attaching the restored alignment tab to a new brush seal assembly.
Claims9
A method of repairing a brush seal assembly for a turbine engine, the method comprising:
- removing an alignment tab from a used brush seal assembly;
- restoring at least one dimension of the alignment tab to a desired condition;
- and
- attaching the restored alignment tab to a new brush seal assembly.
1 more element
Dependencies are inferred from the claim text.