Aerofoil blade containment

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

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F04D 2940

Patent

active

053283244

ABSTRACT:
An aerofoil blade containment structure that is adapted to surround the low pressure turbine casing of a gas turbine engine includes an annular support member upon which is mounted a glass fiber knitted sleeve. The knitted sleeve is folded to define a plurality of interconnected secondary sleeves that are arranged in coaxial superposed relationship. Use of the containment structure obviates the use of thick, and therefore undesirably heavy, turbine casings.

REFERENCES:
patent: 1698514 (1929-01-01), Schmidt
patent: 3602602 (1971-08-01), Motta
patent: 3974313 (1976-08-01), James
patent: 4648795 (1987-03-01), Lardellier
patent: 4902201 (1990-02-01), Neubert
patent: 4934899 (1990-06-01), Patacca
patent: 4961685 (1990-10-01), Neubert

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