Method for producing a blade plating on a blade for a...

B - Operations – Transporting – 23 – K

Patent

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B23K 1/00 (2006.01)

Patent

CA 2751406

The invention relates to a method for producing a blade tip plating (20) on a blade (10) for a turbomachine, in particular on a high-pressure rotating compressor blade for a gas turbine, comprising the following steps: - producing a particle composite material (24) having embedded hard material particles (18); - placing the particle composite material (24) on a solder (30) applied to the blade tip (16); and - heating the solder (30).

L'invention concerne un procédé de fabrication d'un blindage de pointe d'aube (20) sur une aube (10) de turbomachine, notamment sur une aube mobile de compresseur haute pression pour turbine à gaz, comprenant les étapes suivantes: produire un matériau composite particulaire (24) comprenant des particules de matériau dur (18) noyées, appliquer le matériau composite particulaire (24) sur un métal d'apport de brasage (30) appliqué sur la pointe d'aube (16), et chauffer le métal d'apport de brasage (30).

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