GAS TURBINE ENGINES AND CORRESPONDING MAINTENANCE METHOD

A gas turbine engine (20) includes a compressor (44, 52), a combustor (56) fluidly connected to the compressor (44, 52) via a flow path, and a turbine (46, 54) fluidly connected to the combustor (56) via the flow path. At least one multi-piece structure (100; 200; 300) is disposed within the flow pa...

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Bibliographische Detailangaben
1. Verfasser: CARR, JESSE M
Format: Patent
Sprache:eng ; fre ; ger
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