| 摘要 |
The invention relates to a gas turbine engine comprising at least one first composite part (1) intended to be mounted in a second metal part (2) of the engine, said first composite part (1) having an interface surface (S2) intended to be in surface contact with the second metal part (2). The engine also includes a metal protector (3) removably mounted on the first composite part (1) and designed to cover the interface surface (S2). |
