MID-TURBINE FRAME

A mid-turbine frame (12) connected to at least one mount (16) of a gas turbine engine (10) transfers a first load from a first bearing (18) and a second load from a second bearing (20) to the mount (16). The mid-turbine frame (12) includes a single point load structure and a plurality of struts (24)...

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Bibliographische Detailangaben
Hauptverfasser: SOWA, William A, KUMAR, Keshava B, NAGENDRA, Somanath
Format: Patent
Sprache:eng ; fre ; ger
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Zusammenfassung:A mid-turbine frame (12) connected to at least one mount (16) of a gas turbine engine (10) transfers a first load from a first bearing (18) and a second load from a second bearing (20) to the mount (16). The mid-turbine frame (12) includes a single point load structure and a plurality of struts (24). The single point load structure combines the first load and the second load into a combined load. The plurality of struts (24) is connected to the single point load structure and transfers the combined load from the single point load structure to the mount (16).