Vertically oriented seal system for gas turbine vanes
AssigneeGeneral Electric Company
InventorsJohn Ellington Greene, Neelesh Nandkumar Sarawate
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AssigneeGeneral Electric Company
InventorsJohn Ellington Greene, Neelesh Nandkumar Sarawate
Estimating the term…
A seal system for a gas turbine vane includes a first seal layer and an optional second seal layer. Each first seal layer includes multiple seal segments, each of which includes a first leg, a second leg, and an intermediate portion between the first leg and the second leg. Each adjacent pair of seal segments of the first seal is separated by a gap. The seal segments define a substantially complete perimeter of a seal slot in which the first seal is installed. The second seal, which is also segmented, may or may not define the substantially complete perimeter of the seal slot. If present, the second seal segments are circumferentially offset from the first seal segments to block the gaps between the first seal segments. A turbine vane including the present seal system is also disclosed.
A seal system comprising:
Dependencies are inferred from the claim text.