Gas turbine engine blade containment using wire wrapping

Details Gas turbine engine blade containment using wire wrapping Gas turbine engine blade containment using wire wrapping

F - Mech Eng,Light,Heat,Weapons

01

D

F01D 25/24 (2006.01)

Patent

CA 2639028

A blade containment of a gas turbine engine comprises a casing defining an annular wall radially spaced from and immediately surrounding a plurality of blades radially extending from a rotor, and at least one layer of metal wires wrapped around and directly attached to the annular wall.

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