Gas turbine moving blade

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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416 97R, 416 96A, 415115, F61D 518

Patent

active

059159235

ABSTRACT:
A gas turbine moving blade in which the moving blade operating in a high temperature operating gas is cooled from its interior by steam and the steam after being used for the cooling is recovered, by use of a simple structure. A supply side passage (10), through which steam (6) is supplied directly into a cooling passage (51) of a blade leading edge side (11), is provided within a blade root portion (2) and a pocket (19). One end of the pocket is connected to the supply side passage and the other end of which is connected to a cooling passage (52) of a blade trailing edge side (12). The pocket is covered with a plate, which extends in a blade chord direction on an outer peripheral side face of the blade root portion between a blade platform and a rotor plate. Thus, efficiency of the gas turbine can be effectively enhanced.

REFERENCES:
patent: 2873087 (1959-02-01), Terrell et al.
patent: 2920865 (1960-01-01), Lombard
patent: 3455537 (1969-07-01), Kozlin et al.
patent: 4259037 (1981-03-01), Anderson

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