Invention Grant
US09518478B2 Microchannel exhaust for cooling and/or purging gas turbine segment gaps 有权
用于冷却和/或吹扫燃气轮机段间隙的微通道排气

Microchannel exhaust for cooling and/or purging gas turbine segment gaps
Abstract:
A gas turbine stator component includes a composite, segmented ring made up of an annular array of arcuate segments, each having end faces formed with respective seal slots, with radial gaps formed between opposed end faces of adjacent arcuate segments. A seal is located between each pair of opposed seal slots to thereby seal the gaps, and a channel is provided in each of said arcuate segments adapted to be supplied with cooling air, the channel connecting to a passage extending between the channel and a respective one of the seal slots or radial gaps, on a lower-pressure side of the seal.
Information query
Patent Agency Ranking
0/0