Turbomachine blade with fluidically cooled shroud

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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Reexamination Certificate

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07427188

ABSTRACT:
A turbomachine blade, in particular a turbine blade of a gas turbine includes a blade root with a cooling-fluid feed, a blade tip formed with a shroud element. At least one throughflow passage which extends in the blade longitudinal direction is arranged inside the airfoil. A shroud cooling passage is formed in the shroud element at least along a section of the latter, the shroud cooling passage being connected via an opening to the throughflow passage, and a cooling fluid flowing through this shroud cooling passage during operation of the turbomachine blade. At least one flow-guiding element for guiding at least some of the cooling-fluid flow flowing through the shroud cooling passage is arranged in the shroud cooling passage and/or in an inflow or outflow to or from the shroud cooling passage.

REFERENCES:
patent: 3800864 (1974-04-01), Hauser et al.
patent: 4820123 (1989-04-01), Hall
patent: 5320485 (1994-06-01), Bourguignon et al.
patent: 5350277 (1994-09-01), Jacala et al.
patent: 5413456 (1995-05-01), Kulak et al.
patent: 5498126 (1996-03-01), Pighetti et al.
patent: 5669759 (1997-09-01), Beabout
patent: 6132173 (2000-10-01), Tomita et al.
patent: 6471480 (2002-10-01), Balkcum, III et al.
patent: 7147439 (2006-12-01), Jacala et al.
patent: 2002/0098078 (2002-07-01), Beeck et al.
patent: 10131073 (2002-06-01), None
patent: 0649975 (1995-04-01), None
patent: 0955449 (1999-11-01), None
patent: 1074696 (2001-02-01), None
patent: 1215363 (2002-06-01), None
patent: 03194101 (1991-08-01), None
International Search Report for Application No. PCT.EP2005/054448, mailed on Jan. 18, 2006.
Swiss Search Report for Application No. CH1525/04, mailed on Dec. 16, 2004.

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