Systems and methods for variable microchannel combustor liner cooling
US-11859818-B2 · Jan 2, 2024 · US
US8997501B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-8997501-B2 |
| Application number | US-201113152117-A |
| Country | US |
| Kind code | B2 |
| Filing date | Jun 2, 2011 |
| Priority date | Jun 2, 2011 |
| Publication date | Apr 7, 2015 |
| Grant date | Apr 7, 2015 |
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A system includes a combustor transition piece configured to mount between a combustor and a turbine of a gas turbine engine. The combustor transition piece includes a hollow body with an internal flow passage extending from an upstream end portion to a downstream end portion. The combustor transition piece also includes an aft frame coupled to the downstream end portion of the hollow body, an aft flange coupled to the aft frame, and a mounting lug removably coupled to the aft frame at a first joint. The mounting lug is configured to removably couple to a mounting bracket at a second joint.
Opening claim text (preview).
The invention claimed is: 1. A system, comprising: a combustor transition piece configured to mount between a combustor and a turbine of a gas turbine engine, wherein the combustor transition piece comprises: a hollow body comprising an internal flow passage extending from an upstream end portion to a downstream end portion; an aft frame coupled to the downstream end portion of the hollow body; a single aft flange coupled to a portion of the aft frame; and a mounting lug re…
Mechanical Engineering · mapped topic
Mechanical Engineering · mapped topic
Mechanical Engineering · mapped topic
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