Blade of a turbine

Fluid reaction surfaces (i.e. – impellers) – Specific blade structure – Apertured or permeable

Reexamination Certificate

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Details

C416S235000

Reexamination Certificate

active

10931089

ABSTRACT:
The invention relates to a turbine blade (31) having a root region (33), a tip region (37) and a blade airfoil (35), a rounded portion (73) being formed between the root region (33) and the blade airfoil (35), and relief slots (51) passing through the blade trailing edge (41) in the region of this rounded portion (73), thermal expansions being compensated for and thus thermal stresses being minimized by these relief slots (51).

REFERENCES:
patent: 2193686 (1940-03-01), Craddock
patent: 4846629 (1989-07-01), Takigawa
patent: 6174135 (2001-01-01), Lee
patent: 6490791 (2002-12-01), Surace et al.
patent: 6929451 (2005-08-01), Gregg et al.
patent: 2001/0016163 (2001-08-01), Tomita et al.
patent: 2003/0138322 (2003-07-01), Boury et al.
patent: 55096303 (1980-07-01), None
patent: 63248902 (1988-10-01), None
patent: 10299408 (1998-11-01), None
patent: 2000018001 (2000-01-01), None

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