Rapid processing of laminar composite components
US-12180120-B2 · Dec 31, 2024 · US
US8943835B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-8943835-B2 |
| Application number | US-77653510-A |
| Country | US |
| Kind code | B2 |
| Filing date | May 10, 2010 |
| Priority date | May 10, 2010 |
| Publication date | Feb 3, 2015 |
| Grant date | Feb 3, 2015 |
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Official abstract text for this publication.
A combustor for a gas turbine engine is disclosed. The combustor is described as comprising a dome plate coupled to a liner thereof, with at least one heat shield comprised of a ceramic matrix composite coupled at the aft end of the dome plate. Also described is a method for assembling a combustor for a gas turbine engine, including releasing a metal alloy heat shield from a dome plate and providing a ceramic matrix composite heat shield as replacement.
Opening claim text (preview).
What is claimed is: 1. A combustor for a gas turbine engine, the combustor comprising: a combustion chamber comprising an inner liner and an outer liner; a dome plate coupled to at least one of the inner liner and outer liner, the dome plate having a forward end and an aft end and including at least one opening therethrough; at least one heat shield comprised of a ceramic matrix composite coupled at the aft end of the dome plate; a threaded member provided as at least one bo…
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