Turbomachinery blade with improved tip cap

Fluid reaction surfaces (i.e. – impellers) – With heating – cooling or thermal insulation means – Changing state mass within or fluid flow through working...

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Details

416213R, 416241R, 415172A, F01D 518

Patent

active

042472547

ABSTRACT:
A turbomachinery blade including a hollow interior is provided with an improved tip cap comprising first and second members each made of an alloy of a composition and properties different from the other. The first member, in the form of a closure plate bonded to sidewalls of the hollow body, is of a nickel-base or cobalt-base superalloy casting characterized by high mechanical strength properties at elevated temperatures. The second member is a rib of the shape of and bonded to the first member and is of a cast alloy characterized by the combination of resistance to oxidation, sulfidation and thermal fatigue at elevated temperatures. The second member provides an outer tip extension of the blade.

REFERENCES:
patent: 3389889 (1968-06-01), Penny
patent: 3615375 (1971-10-01), Beltran
patent: 3700427 (1972-10-01), Hoppin et al.
patent: 3759692 (1973-09-01), Zelahy
patent: 3854842 (1974-12-01), Caudill
patent: 3899267 (1975-08-01), Dennis et al.
patent: 3982851 (1976-09-01), Andersen et al.

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