FIELD: metallurgy.
SUBSTANCE: strips of alloyed metals are built-up in direction of lengthwise generatrix of blade body ensuring gaps between built-up strips at least on part of blade body and forming layer. As built-up metal there are used alloys on base of nickel with Co, Cr, Al, Mo, W, Ti, Y or their combination. Further, a blade body is mechanically processed ensuring its specified geometry. Successive thermal treatment corresponds to thermo-cycling.
EFFECT: manufacture of coating possessing high operational properties.
20 cl, 1 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| PROCEDURE FOR FORMING DISCRETE WELDED COATING ON BLADE BODY OF TURBO-MACHINE | 2009 |
|
RU2420610C1 |
| METHOD OF RECLAIMING TURBO MACHINE VANE BODY | 2009 |
|
RU2440877C2 |
| METHOD TO RECONDITION STEAM TURBINE VANES FROM ALLOYED STEELS | 2009 |
|
RU2426631C1 |
| METHOD OF RECLAIMING TURBO MACHINE VANES | 2009 |
|
RU2420383C2 |
| REPAIR METHOD OF BLADES MADE FROM STEEL ALLOY | 2006 |
|
RU2353496C2 |
| METHOD OF RECLAIMING OPERATING PROPERTIES OF VANES MADE FROM TITANIUM ALLOYS | 2009 |
|
RU2424887C2 |
| METHOD OF RECOVERING OPERATING PROPERTIES OF TURBO MACHINE VANES FROM ALLOYED STEELS | 2009 |
|
RU2424886C2 |
| METHOD OF RECONDITIONING TURBO MACHINE BLADE ROOT FACE WITH MAKING BRUSH SEAL | 2010 |
|
RU2479400C2 |
| METHOD OF REPAIRING VANES MADE FROM TITANIUM ALLOYS | 2009 |
|
RU2420382C2 |
| METHOD OF RECOVERING OPERATING PROPERTIES OF TURBO MACHINE VANES FROM ALLOYED STEELS | 2009 |
|
RU2420384C2 |
