Shroud ring aerofoil capture

Rotary kinetic fluid motors or pumps – Including destructible – fusible – or deformable non-reusable...

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Details

415114, 415174, F01D 1108

Patent

active

041993004

ABSTRACT:
A turbine for a gas turbine engine is provided with a rotary stage comprising an annular array of rotor blades surrounded by an annular shroud member. The shroud member is hollow, the hollow interior being provided with a heat transfer medium which, in operation, functions as a condensable vapor and liquid whereby the shroud member is a heat pipe. The shroud member is further provided with a wall adjacent the aerofoil blade which is adapted to be penetrable by a detached blade or blade portion. The wall of the shroud member is dimensioned so that any such detached blade or blade portion which penetrates the wall enters the hollow shroud ring and is retained within it.

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patent: 3537713 (1970-11-01), Matthews et al.
patent: 3627444 (1971-12-01), Lentz
patent: 3719365 (1973-03-01), Emmerson et al.

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