Seal assembly to seal corner leaks in gas turbine
AssigneeGeneral Electric Company
InventorsBodhayan Dev, Robert Carl Meyer, Neelesh Nandkumar Sarawate, Jason Edward Albert, Gary Michael Itzel
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AssigneeGeneral Electric Company
InventorsBodhayan Dev, Robert Carl Meyer, Neelesh Nandkumar Sarawate, Jason Edward Albert, Gary Michael Itzel
Estimating the term…
Various embodiments include gas turbine seals and methods of forming such seals. In some cases, a turbine includes: a first arcuate component adjacent to a second arcuate component, each arcuate component including one or more slots located in an end face, each of the one or more slots having a plurality of axial surfaces and radially facing surfaces extending from opposite ends of the axial surfaces and a seal assembly disposed in the slot. The seal assembly including an intersegment seal including a plurality of seal segments defining one or more corner regions. The intersegment seal disposed in a slot defining a high-pressure slot side and a low-pressure slot side, wherein the slot includes a plurality of slot segments. Each of the plurality of seal segments including at least one extended portion to either seal the one or more corner regions on a low-pressure slot side, form a recess in the intersegment seal, or both.
A seal assembly to seal a gas turbine hot gas path flow in a gas turbine, the seal assembly comprising:
A gas turbine comprising:
A method of assembling a seal in a turbine, the method comprising:
Dependencies are inferred from the claim text.