Gas Turbine engine casing construction

Details Gas Turbine engine casing construction Gas Turbine engine casing construction

1997-03-06

1999-03-23

Verdier, Christopher

Rotary kinetic fluid motors or pumps

Including destructible, fusible, or deformable non-reusable...

415200, F01D 2100

Patent

active

058850562

ABSTRACT:
Casing assembly for a gas turbine engine comprising an annular cross section casing around which a plurality of layers of flexible material are wound. One or more rigid panels are positioned between the wound flexible material and the annular casing. The rigid panel provides enhanced containment of a detached fan blade or part of a fan blade by distributing the load of the detached blade across the wound flexible material.

REFERENCES:
patent: 4534698 (1985-08-01), Tomich
patent: 4547122 (1985-10-01), Leech
patent: 4818176 (1989-04-01), Huether et al.
patent: 5336044 (1994-08-01), Forrester
patent: 5447411 (1995-09-01), Curley et al.
patent: 5516258 (1996-05-01), Newton

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