General Electric Company

General Electric Technology Gmbh

Steven Paul Byam

Joseph Anthony Weber

Brad Wilson Vantassel

Travis J Packer

Evan Andrew Sewall

Brad Wilson Van Tassel

A turbine of a gas turbine engine that includes a stationary shroud ring having inner shroud segments circumferentially stacked about a hot gas path. The inner shroud segments may include a first inner shroud segment that includes: a cooling configuration having cooling channels configured to receive and direct a coolant through an interior of the first inner shroud segment, where each of the cooling channels extends lengthwise between a first end and a second end that includes an outlet formed through an exterior surface of the first inner shroud segment; a circumferential edge; a slot formed in the circumferential edge; and a sealing member positioned within the slot. The outlet of at least one of the cooling channels may be positioned within the slot.

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Fountain Inn, SC, United States of America

Steven Paul Byam