Preloading brace for gas turbine engine transportation

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

Patent

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Details

F01D 25/28 (2006.01) B65D 85/68 (2006.01) F02C 7/06 (2006.01) F02C 7/20 (2006.01) F16C 39/00 (2006.01) F16C 41/04 (2006.01)

Patent

CA 2692712

An assembly for preventing damage to bearings of a gas turbine engine (10) during transportation is provided. The assembly comprises a turbofan gas turbine engine (10) having an engine casing (20) and at least one turbine shaft (22) supported by a plurality of bearings, and, a brace (24) secured relative to the engine casing and biasing the shaft (22) along an axial direction of the shaft (22).

L'invention concerne un ensemble permettant d'empêcher des dégâts à des paliers d'un moteur à turbine à gaz (10) pendant le transport. L'ensemble comprend un moteur à turbine à gaz à double flux (10) ayant un carter (20) et au moins un arbre de turbine (22) supporté par une pluralité de paliers, et, une entretoise (24) fixée par rapport au carter de moteur et sollicitant l'arbre (22) le long d'une direction axiale de l'arbre (22).

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