Blade for gas turbine

Fluid reaction surfaces (i.e. – impellers) – Specific blade structure – Coating – specific composition or characteristic

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Details

148404, 148902, 1641221, 1641222, F01D 514

Patent

active

056116705

ABSTRACT:
A gas-turbine moving blade made of a Ni-base superalloy containing less grain boundary strengthening elements, in which a blade portion is formed of a single crystal and the rest is formed of columnar crystals, and a gas turbine including the moving blade. A thermal efficiency of the gas turbine can be improved to 35% or more, and a thermal efficiency of complex power generation with a steam turbine can be improved to 45% or more.

REFERENCES:
patent: 3568757 (1971-03-01), Piearcey
patent: 3844728 (1974-10-01), Copley et al.
patent: 4033792 (1977-07-01), Giamei et al.
patent: 4184900 (1980-01-01), Erickson et al.
patent: 4190094 (1980-02-01), Giamei
patent: 4609029 (1986-09-01), Vishnevsky et al.
patent: 4637448 (1987-01-01), Burke et al.
Journal of Materials Engineering and Performance, vol. 2, No. 4, Aug. 1993, Materials Park, Ohio, U.S., pp. 481-487, by K. Harris et al, entitled "Development of Two Rhenium-Containing Supperalloys for single-Crystal Blade and Directionally solidified Vane Applications in Advanced Turbine Engines".

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