Blade for a gas turbine engine

Rotary kinetic fluid motors or pumps – With passage in blade – vane – shaft or rotary distributor...

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Details

415137, 415200, F01D 518, F01D 902

Patent

active

042603269

ABSTRACT:
A stator blade for a gas turbine engine comprises a stack of laminar sections and means adapted to resiliently hold the sections together in compression to allow for differential expansion between the stack and supporting structure.

REFERENCES:
patent: 2254821 (1941-09-01), Haw
patent: 3301526 (1967-01-01), Chamberlain
patent: 3353359 (1967-11-01), Webb
patent: 3378228 (1968-04-01), Davies et al.

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