Hollow turbine blade

Fluid reaction surfaces (i.e. – impellers) – With heating – cooling or thermal insulation means – Changing state mass within or fluid flow through working...

Reexamination Certificate

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Details

C416S233000, C416S23600R

Reexamination Certificate

active

07845905

ABSTRACT:
A hollow turbine blade is provided including an airfoil profile which is formed by a suction-side profile wall and a pressure-side profile wall and around which a hot gas can flow and which has a profile height, directed along a blade axis, from a platform up to a profile tip, having at least one supporting rib which is provided in the interior of the turbine blade and connects the pressure-side profile wall to the suction-side profile wall in a respective connecting region, and having at least one slot provided in the profile wall on the hot-gas side and extending along the blade axis. The slot of the turbine blade, on the hot-gas side in the profile wall, is opposite the connecting region formed by the supporting rib and the profile wall.

REFERENCES:
patent: 2807870 (1957-10-01), Harness
patent: 2882974 (1959-04-01), Boegehold
patent: 2933286 (1960-04-01), Klint et al.
patent: 3290004 (1966-12-01), Ishibashi
patent: 5690473 (1997-11-01), Kercher
patent: 7318699 (2008-01-01), Serafini et al.
patent: 1 508 399 (2005-02-01), None
patent: 1 512 489 (2005-03-01), None
patent: 1 525 942 (2005-04-01), None
patent: 10 061406 (1998-03-01), None
patent: 2000 018 01 (2000-01-01), None

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