Patent ID: 7255528
Filing Date: 2007-08-14
Classification: F01D,F04D,Y02T

Abstract:
1. A gas turbine engine casing comprising a generally cylindrical, or frustoconical, casing, the casing including at least one member secured to the casing, the member having a first portion extending radially from the casing and a second portion extending axially from the first portion of the member, at least one liner panel being positioned radially from the casing, a first end of the liner panel being removably securable on the member by at least one resilient spring finger, the at least one resilient spring finger being biased to move axially away from the first end of the liner panel to locate the at least one resilient spring finger on the second portion of the member wherein the at least one resilient spring finger being movably axially towards the center of the liner panel to remove the at least one resilient spring finger from the second portion of the member.