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
- Patent Title: Microchannel exhaust for cooling and/or purging gas turbine segment gaps
- Patent Title (中): 用于冷却和/或吹扫燃气轮机段间隙的微通道排气
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Application No.: US14064867Application Date: 2013-10-28
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Publication No.: US09518478B2Publication Date: 2016-12-13
- Inventor: Aaron Ezekiel Smith , David Wayne Weber
- Applicant: General Electric Company
- Applicant Address: US NY Schenectady
- Assignee: General Electric Company
- Current Assignee: General Electric Company
- Current Assignee Address: US NY Schenectady
- Agency: Nixon & Vanderhye P.C.
- Main IPC: F01D25/12
- IPC: F01D25/12 ; F01D11/00 ; F01D9/04

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.
Public/Granted literature
- US20150118033A1 MICROCHANNEL EXHAUST FOR COOLING AND/OR PURGING GAS TURBINE SEGMENT GAPS Public/Granted day:2015-04-30
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