FAN BLADE Russian patent published in 2006 - IPC F04D29/38 

Abstract RU 2272180 C2

FIELD: gas turbine engine engineering.

SUBSTANCE: fan blade (12) comprises fairing (18) provided with shank (26) and made in block with platform (20). The platform has front (34) and back (36) edges and arc-shaped first (38) and second (40) sides interposed between them. The shank of the fairing is shifted in the transverse direction so that the shank is closer to the first side of the platform than to the second side.

EFFECT: enhanced reliability.

10 cl, 5 dwg

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RU 2 272 180 C2

Authors

Anderson Bernard Dzhozef

Nassbaum Dzheffri Govard

Gomes Khuan Mario

Dates

2006-03-20Published

2001-06-29Filed