Non-Integral Turbine Blade Platforms and Systems

作者: Luke J. Ammann

DOI:

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摘要: In one embodiment, a turbine blade platform may be disposed between two blades. The include first exterior side configured to interface with blade. also second generally opposite the and

参考文章(199)
Padmakar M. Niskode, Michael W. Horner, William M. Farrell, Variable pitch rotor assembly for a gas turbine engine inlet ,(1996)
Geoffrey C. Todd, Arthur E. Sutton, Martin Kirkman, Sensor failure detection for a multi-actuator position control system ,(1999)
Douglas A. Keller, Gary B. Merrill, Malberto F. Gonzalez, Thermally insulated cmc structure with internal cooling ,(2007)
Charles J. Haap, Theodore T. Thomas, Delmer H. Landis, Floating seal for a variable area turbine nozzle ,(1977)
Marcel R. Soligny, Gerard E. A. Jourdain, Variable area nozzle vane ,(1983)
Elmore V. Sprunger, Arthur P. Adamson, Variable cycle engine ,(1977)