GAS TURBINE ENGINE

A gas turbine engine (20) comprises a turbine section (28) disposed adjacent to a combustor section (26), the turbine section including a turbine vane (62) having an inner platform (72) and an outer platform (74) joined together by an airfoil (70) having a pressure side (84) and a suction side (86)...

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Bibliographische Detailangaben
Hauptverfasser: FORBES, John David, LEON, Jeffrey, ANSELMI, Gregory, KAUFMAN, Eleanor D, BOTNICK, Christina E, KASHYAP, Tania Bhatia, ALLEN, Richard N, MACE, Gerald M, LEVINE, Jeffrey R, NADEAU, Daniel C
Format: Patent
Sprache:eng ; fre ; ger
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