Method for repairing and/or replacing individual elements of...

B - Operations – Transporting – 23 – K

Patent

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B23K 13/01 (2006.01)

Patent

CA 2657005

The invention relates to a method for repairing and/or replacing individual elements of a gas turbine component (10), particularly a blade or blade part arranged on a rotor support of a gas turbine, at least some of the components (10) being provided with at least one wear-resistant and/or erosion-resistant layer. The inventive method comprises the following steps: a) a coated or uncoated individual element that is damaged and/or needs to be replaced is removed from the component (10); b) a coated, partially coated, or uncoated replacement element (12) is provided; c) the replacement element (12) is fed and aligned relative to the component (10); and d) the replacement element (12) is connected to the component (10), corresponding contact areas (20, 22) of the replacement element (12) and the component (10) being connected by means of an inductive low-frequency or high-frequency pressure welding process.

La présente invention concerne un procédé de réparation et/ou de remplacement d'éléments individuels d'une pièce (10) d'une turbine à gaz, en particulier un procédé de réparation et/ou de remplacement d'une ailette, placée sur un pylône de rotor d'une turbine à gaz, ou d'une partie de l'ailette, les pièces (10) étant au moins partiellement pourvues d'au moins une couche de protection contre l'usure et/ou l'érosion. Le procédé consiste a) à séparer de la pièce (10) un élément individuel endommagé et/ou à remplacer enduit ou non, b) à préparer un élément de rechange (12) enduit, partiellement enduit ou non enduit, c) à amener et à orienter l'élément de rechange (12) par rapport à la pièce (10) puis d) à joindre l'élément de rechange (12) et ladite pièce (10), la jonction de surfaces de jonction correspondantes (20, 22) de l'élément de rechange (12) et de la pièce (10) étant réalisée par un procédé de soudage par pression haute ou basse fréquence et par induction.

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