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
1992-03-01
Miscellaneous
No indication
English
Webasto develops stiffer, lighter cabrio
Online Contents | 2008
Life assessment of dovetail joints between blades and discs in aero-engines
Tema Archive | 1986
|Sprayable stiffer - damping adhesive (BPR[R])
British Library Conference Proceedings | 1995
|