Method for the maintenance of gas turbines

Metal working – Method of mechanical manufacture – Impeller making

Reexamination Certificate

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Details

C029S889200, C029S791000, C029S564100, C029S430000, C029S402080

Reexamination Certificate

active

07827686

ABSTRACT:
A method for the maintenance of gas turbines is provided. According to the method, a gas turbine is dismantled and modules, structural components, or component parts of the aeroplane mechanism are subsequently inspected and/or repaired. Then, an aeroplane mechanism consisting of inspected and/or repaired or new modules, structural components or component parts is mounted. Dismantling and/or mounting is divided into at least two work steps. A work station is provided for each work step and the aeroplane mechanism, modules, structural components or component parts of the aeroplane mechanism are displaced by the work station provided for carrying out one work step.

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J.W. Sawyer, P.E. Fellow, K. Hallberg, Turbomachinery Maintenance Handbook, 1980, Turbomachinery International Publications, Norwalk, USA, XP002293430; pp. 10-1 to 10-4.
C. Bremer, Kompressor- und Turbinenschaufeln automatisch reparieren, Werkstatt und Betrieb, Carl Hanser Verlag, Muenchen, DE, vol. 129, No. 7/8, pp. 672-674, XP 000678763, ISSN 0043-2792—English Summary.

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