Turbine exhaust case and method of making

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

Patent

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Details

F01D 25/24 (2006.01) B23K 26/00 (2006.01) B23K 33/00 (2006.01) B23P 15/00 (2006.01) F01D 25/16 (2006.01) F01D 25/30 (2006.01)

Patent

CA 2573342

A structural turbine exhaust case (25) of a gas turbine engine, comprises inner and outer case portions (27, 29); a bearing housing (33) connected to the inner case portion (27) for supporting a main spool (12) of the gas turbine engine; and a plurality of airfoils (31) extending between the inner and outer case portions (27, 29), airfoils (31) structurally connecting the inner case portion (27) to the outer case portion (29).

Carter structurel d'échappement (25) de moteur à turbine à gaz comprenant des parties intérieure et extérieure (27, 29), un carter de pallier (33) accouplé à la partie intérieure (27) afin de supporter une bobine principale (12) du moteur de turbine à gaz et une pluralité d'ailettes à profil aérodynamique (31) s'étendant entre les parties intérieure et extérieure (27, 29) du carter, ces ailettes à profil aérodynamique (31) accouplant la partie intérieure (27) à la partie extérieure (29) du carter.

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