| 摘要 |
<p>A method and apparatus for brazing a honeycomb sealing (14) at a turbine, in particular a gas turbine, include: applying a brazing filler material (18) to the honeycomb sealing (14), placing the honeycomb sealing (14) at a turbine component (10), directing a laser beam (20) to the brazing filler material (18), and melting the brazing filler material (18) by means of the laser beam (20) for bonding the honeycomb sealing (14) to the turbine component (10).</p> |
