Methods and apparatus for controlling engine clearance closures

F - Mech Eng,Light,Heat,Weapons – 01 – D

Patent

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Details

F01D 25/24 (2006.01) F02C 7/00 (2006.01) F02C 7/20 (2006.01) F02C 7/22 (2006.01)

Patent

CA 2448502

An apparatus 30 used in a gas turbine engine 10 is provided. The apparatus includes a first radial flange 34, a second radial flange 36 that is axially spaced from the first radial flange, and a plurality of circumferentially-spaced beams 38 that extend between the first radial flange and the second radial flange. At least one of the beams is tapered between the first and second radial flanges.

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