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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Authors
Dates
2006-03-20—Published
2001-06-29—Filed