A turbine nozzle includes ceramic outer and inner bands and an integral ceramic vane aft segment. A metal vane forward segment adjoins the aft segment in a hybrid assembly.
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A turbine nozzle includes ceramic outer and inner bands and an integral ceramic vane aft segment. A metal vane forward segment adjoins the aft segment in a hybrid assembly. 19650300, Eickmann; US-3195901, 19650700, Mercier; US-3196901, 19650700, Phillipps; US-3421604, 19690100, Hobbs; US-3576153, 19
A turbine nozzle includes ceramic outer and inner bands and an integral ceramic vane aft segment. A metal vane forward segment adjoins the aft segment in a hybrid assembly. 19650300, Eickmann; US-3195901, 19650700, Mercier; US-3196901, 19650700, Phillipps; US-3421604, 19690100, Hobbs; US-3576153, 19710400, Doutt; US-3657783, 19720400, Eillis, 029/890.131; US-3759637, 19730900, Vuaille; US-3790179, 19740200, Scannell, 277/558; US-3953213, 19760400, Gasper; US-4013386, 19770300, Hardman et al.; US-4211152, 19800700, Colletti et al.; US-4386782, 19830600, Reverberi; US-5092125, 19920300, Leight-Monstevens et al.; US-5169160, 19921200, Gaskill et al.; US-5263404, 19931100, Gaucher et al.; US-5328178, 19940700, Niles; US-5495792, 19960300, Izumi et al.; US-5682861, 19971100, Stockner et al., 123/495; US-5901686, 19990500, Stockner et al.; US-5951022, 19990900, Gorman et al., 277/626; US-5992768, 19991100, Smith, III et al.
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Frey Gary A. ; Twardochleb Christopher Z., Airfoil structure.
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