Blade platform

F - Mech Eng,Light,Heat,Weapons – 01 – D

Patent

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170/81

F01D 5/30 (2006.01) F01D 9/02 (2006.01) F04D 29/34 (2006.01)

Patent

CA 1254840

13DV-8562 BLADE PLATFORM ABSTRACT OF THE DISCLOSURE The present invention discloses a turbomachinery blading configuration. The configuration includes a circumferential recess in a blade support structure and a plurality of blades. Each blade has a platform for mounting the blade within the recess. Each platform includes oppositely directed, generally circumferentially facing edges, each edge having first and second axial surfaces separated by a recess. The surfaces contact matching surfaces on adjacent blades thereby determining predictable load paths for tangential and twisting moment reaction forces acting on the blades.

498349

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