Integral shroud blade design

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

416191, 416203, 416500, 298892, F01D 516

Patent

active

051565293

ABSTRACT:
An integral shroud blade comprising a root portion for mounting the blade in a row on a turbine rotor; a platform portion; an airfoil portion extending upwardly from the platform portion and having a leading edge, a trailing edge, and a tip; a shroud formed on the tip of the airfoil portion and having two opposite tangential side surfaces and a top surface; and at least one pair of holes extending into the shroud, each of the two tangential sides having one hole of each pair being formed therein.

REFERENCES:
patent: 2430140 (1947-11-01), Phelan et al.
patent: 3649133 (1972-03-01), Wagner
patent: 4097192 (1978-06-01), Kulina
patent: 4699569 (1987-10-01), Gloor
patent: 4767273 (1988-08-01), Partington
patent: 4776764 (1988-10-01), Ortolano
patent: 4878810 (1989-11-01), Evans

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