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US 2014/0234118 A1Published application
Turbine engine comprising a metal protection for a composite part
AssigneeSnecma
InventorsAntoine Jean-Philippe Beaujard, Didier Fabre, Jean Pierre Mareix
Life of this patent
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Abstract
A gas turbine engine including at least a first composite part configured for mounting in a second metal part of the engine, the first composite part including an interface surface configured to be in surface contact with the second metal part, the engine including a metal protection removably mounted on the first composite part and configured to cover the interface surface.
Claims9
1-8. (canceled)
A gas turbine engine comprising:
- at least a first composite part configured to be mounted in a second metal part of the engine, the first composite part including an interface surface configured to be in surface contact with the second metal part;
- a metal protection removably mounted on the first composite part and configured to cover the interface surface,
- wherein the first composite part includes a means for radial locking of the metal protection presented in a form of an annular groove.
Dependencies are inferred from the claim text.