Methods and apparatuses for assembling a gas turbine engine

Details Methods and apparatuses for assembling a gas turbine engine Methods and apparatuses for assembling a gas turbine engine

F - Mech Eng,Light,Heat,Weapons

23

R

F23R 3/60 (2006.01) F01D 25/28 (2006.01) F02C 3/14 (2006.01)

Patent

CA 2568818

A method for assembling a gas turbine engine (13) includes coupling an axisymmetric structure within the gas turbine engine, wherein the axisymmetric structure includes a plurality of mounting bushings (112, 114) extending from a radially outer surface of the axisymmetric structure, inserting a first quantity of fixed pins (200) at least partially into a respective mounting bushing to facilitate securing the axisymmetric structure within the gas turbine engine, and inserting a second quantity of floating pins (210) at least partially into a respective mounting bushing to facilitate each floating pin moving in both an axial and tangential direction with respect to a gas turbine engine centerline axis (34).

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