Rebuilt shrouded turbine blade and method of rebuilding the same

Fluid reaction surfaces (i.e. – impellers) – Rotor having flow confining or deflecting web – shroud or... – Axially extending shroud ring or casing

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Details

2915688, 2940207, 2940218, 29530, F01D 512, F01D 514, F01D 520

Patent

active

048222488

ABSTRACT:
The shrouded turbine blade is provided with a wear resistant surface on the seals as well as along the abutment faces including the notched edges. The wear surfaces are characterized in being metallurgically bonded to the base material of the shroud without significant dilution by the base material. This is accomplished by using transparent plasma arc welding at a low amperage and a low temperature. The wear resistant surface can be of a material different from the base material of the shroud proper.

REFERENCES:
patent: 4028788 (1977-06-01), DeMusis
patent: 4155152 (1979-05-01), Cretella et al.
patent: 4291448 (1981-09-01), Cretella et al.
patent: 4386112 (1983-05-01), Eaton et al.
Metals Handbook, vol. 6, Welding & Brazing, 8th Ed., "Hard Facing by Plasma Arc Welding", pp. 159-160.
"Plasma Flame Spraying Rebuilds Jet Engine Parts", Welding Journal, vol. 50, No. 5 (Mar. 1972); p. 185.

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