Fan blade for a gas-turbine engine

Rotary kinetic fluid motors or pumps – With bimetallic blade – vane – or adjustment means therefor

Reexamination Certificate

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Details

C415S119000, C416S235000, C416S500000

Reexamination Certificate

active

07033131

ABSTRACT:
For material reduction, a fan blade made of solid material for a gas-turbine engine is provided in the area of the blade tip with at least one cavity (5) extending from the face of the blade tip. Thus, apart from the aspect of weight saving, the vibration amplitudes and the centrifugal forces can be reduced considerably and the natural vibration behavior improved in a simple manner, ultimately increasing mechanical strength.

REFERENCES:
patent: 1970435 (1934-08-01), Sharp
patent: 2463340 (1949-03-01), Wiberg
patent: 4097192 (1978-06-01), Kulina
patent: 4497613 (1985-02-01), Carreno
patent: 5348446 (1994-09-01), Lee et al.
patent: 5692881 (1997-12-01), Leibfried
patent: 5738491 (1998-04-01), Lee et al.
patent: 6033186 (2000-03-01), Schilling et al.
patent: 577108 (1976-06-01), None
patent: 1627779 (1971-07-01), None
patent: 3507578 (1985-09-01), None
patent: 1089247 (1967-11-01), None
patent: 2155558 (1985-09-01), None
German Seach Report dated Jan. 18, 2003.

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