NOZZLE SEGMENT FOR USE WITH MULTIPLE DIFFERENT TURBINE ENGINES

A nozzle segment (100) includes an inner band (104), an outer band (106), and at least one nozzle vane (102) extending between the inner and outer bands (104, 106). The outer band (106) includes a hook (126) that extends radially outwardly from an outer surface (122). The hook (126) is oriented to c...

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Bibliographische Detailangaben
Hauptverfasser: BROWN, Joe T, BARRETT, Norman Andrew, II
Format: Patent
Sprache:eng ; fre ; ger
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