Exhaust diffuser and method for manufacturing an exhaust diffuser

摘要

An exhaust diffuser and method for manufacturing an exhaust diffuser is provided. An exhaust diffuser for a torque-generating turbine, in particular a torque-generating gas turbine is provided herein. The exhaust diffuser having an inner member, the inner member having an outer surface and an outer member having an inner surface, the inner member and the outer member forming an annular channel, at least a first supporting strut connecting the inner member and the outer member, the first supporting strut extending essentially radially from the inner surface to the outer surface, the first supporting strut having a middle section having a first airfoil and an outer section having a second airfoil, and the second airfoil differing from the first airfoil in shape to be able to handle a higher range of angle of attack. Furthermore, it is described a method for manufacturing an exhaust diffuser.

主权项

1. An exhaust diffuser for a torque-generating turbine, the exhaust diffuser comprising:
an inner member having an outer surface and an outer member having an inner surface, the inner member and the outer member forming an annular channel, a first supporting strut connecting the inner member and the outer member, the first supporting strut extending essentially radially from the inner surface to the outer surface, a second supporting strut, wherein the first supporting strut and the second supporting strut form a mirror twin-strut with an in flow-direction narrowing channel therein between; the first supporting strut and the second supporting strut comprising a middle section having a first airfoil, an outer section having a second airfoil and an inner section having a third airfoil, the second airfoil differing from the first airfoil in shape to be able to handle a higher range of angle of attack with respect to the first airfoil, and wherein: the first airfoil comprises a smaller leading edge radius than the second airfoil and the third airfoil; or the first airfoil comprises a smaller camber than the second airfoil and the third airfoil; or the second airfoil comprises a higher angle of incidence than the first airfoil and the third airfoil comprises a lower angle of incidence than the first airfoil.