Turbine center frame having a connecting element
AssigneeMTU Aero Engines AG
InventorHermann Klingels
Life of this patent
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AssigneeMTU Aero Engines AG
InventorHermann Klingels
Estimating the term…
A turbine center frame for a gas turbine, in particular an aircraft gas turbine, having a hot gas-conveying, segmented annular duct (6), a radial outer casing (4) that is disposed at a distance around the annular duct (6), a hub element (7) that is disposed radially inwardly at a distance from the annular duct (6), a plurality of struts (5) that essentially extend in the radial direction (RR) through the annular duct (6) and that are coupled radially inwardly to the hub element (7) and radially outwardly to the outer casing (4), and having at least one connecting element (30), that is formed obliquely to the struts (5), that extends through the annular duct (6), and is coupled radially inwardly to a seal carrier element (20), the seal carrier element (20) being supported axially forwardly on the hub element (7). At least one connecting element (30) is coupled radially outwardly to one of the struts (5).
A turbine center frame for a gas turbine comprising:
A turbine center frame for a gas turbine comprising:
A turbine center frame for a gas turbine comprising:
Dependencies are inferred from the claim text.