WEAR RESISTANT AIRFOIL TIP

A gas turbine engine includes an engine static structure extending circumferentially about an engine centerline axis; a compressor section, a combustor section, and a turbine section within the engine static structure. At least one of the compressor section and the turbine section includes at least...

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Bibliographische Detailangaben
1. Verfasser: WUSATOWSKA-SARNEK, Agnieszka M
Format: Patent
Sprache:eng ; fre ; ger
Schlagworte:
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