| 摘要 |
<p>The invention concerns a method for resurfacing at least one arm (9) of an intermediate casing (4) of a turbomachine, such as a turbojet engine or a turboprop engine of an aircraft, comprising the steps consisting of: -striking off at least one end (11) of the arm (9) to be resurfaced, -resurfacing the struck-off end (11) of the arm (9) by adding filler metal (34) using a short-circuit transfer MIG welding method, also called CMT (Cold Metal Transfer) method, -machining the resurfaced portion (11) of the arm (9) so as to provide it with the required geometry.</p> |
