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AssigneeGeneral Electric Company
InventorsDavid Wayne Weber, Victor John Morgan, Neelesh Nandkumar Sarawate
Estimating the term…
A device including a conjoined laminate interface seal shaped for reducing inter-seal gap (e.g., an angled gap, an ‘L’-shaped gap, etc.) leakage in gas turbines is disclosed. In one embodiment, a seal device for a gas turbine includes: a first flange shaped to be disposed within a first slot of a first arcuate component and a first adjacent slot of a second arcuate component; a conjoined layer connected to a first surface of the first flange, the first surface configured to face a working fluid flow of the gas turbine; and a second flange shaped to be disposed within a second slot of the first arcuate component and a second adjacent slot of the second arcuate component, the second flange including a second surface connected to the conjoined layer.
A seal device, the seal device comprising:
A gas turbine, comprising:
A gas turbine, comprising:
Dependencies are inferred from the claim text.