Multihook circumferential dovetail configuration for mounting blades around circumference of rotor disk in turbomachine reduces bending stresses in disk. Provides substantial section of post where most needed to resist maximum bending moment near lower hook.
Stiffer Circumferential Dovetail Mount For Turbine Blades
NASA Tech Briefs ; 16 , 3
01.03.1992
Sonstige
Keine Angabe
Englisch
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