OPTIMAL LIFT DESIGNS FOR GAS TURBINE ENGINES

Turbine assemblies for gas turbine engines are provided. In one embodiment, a turbine assembly 75 includes a row 84 of circumferentially adjacent turbine rotor blades 74, each blade 74 in the row 84 of blades 74 including an airfoil 86 defining a chord ( c ) extending axially between opposite leadin...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	DAILEY, Lyle Douglas, WADIA, Aspi Rustom, JOHNSON, Christopher Ryan, MOLLMANN, Daniel Edward
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	BLASTING ENGINE PLANTS IN GENERAL HEATING LIGHTING MACHINES OR ENGINES IN GENERAL MECHANICAL ENGINEERING NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES STEAM ENGINES WEAPONS
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