Montage intégré pour cadre de turbine moyenne
| N° de brevet: |
EP1882827 (A2) |
| Date de publication: |
2008-01-30 |
| Inventeur(s): |
NAGENDRA SOMANATH [US];KUMAR KESHAVA B [US];SOWA WILLIAM A [US]; |
| Demandeur(s): |
UNITED TECHNOLOGIES CORP [US]; |
| Classification: |
F01D25/16; |
| N° de demande: |
EP20070252955 20070726 |
| Numéro(s) de priorité: |
US20060494032 20060727 |
An engine casing (12) for a mid-turbine frame (14) having a plurality of radially extending struts (34) includes a ring structure (22) and at least one mount (30). The ring structure has an interior surface (24), an exterior surface (26), and a plurality of equally spaced dimples (28) along the exterior surface (26) and protruding from the interior surface (24). The ring structure (22) is connected to each of the plurality of struts (34) at the interior surface (24) at the dimples (28). The mount (34) is positioned within each of the dimples (28) and transfers load to the engine casing (12).
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