FIELD: aircraft and machine engineering industry branches, possibly processes and equipment for welding on end surfaces of thin-wall products. SUBSTANCE: method comprises steps of cutting groove with radius and depth values in range 0.4-0.6 mm; using special alloy as additive metal in the form of cast ground rod with diameter 2.5-3 mm for welding it onto contact surface until cut groove; going on shield gas supply after termination of welding-on process for time period equal to 10-20 s; at finish working restoring groove with radius 0.6-0.8 mm; then realizing heat treatment of vane; sustaining electric current for welding on in range (50-60)A while using electrode with diameter 1.5-2 mm; performing heat treatment of vane in vacuum furnace for two hours at temperature 950 C and at evacuation degree 10-3-10-4 Hg mm; testing welded on surface and quality of its mechanical working by color flaw detection or with the aid of luminescent paint; then restoring protective coating of vane. EFFECT: enhanced quality of vanes designed for secondary use. 3 cl, 2 dwg, 1 ex
Title | Year | Author | Number |
---|---|---|---|
METHOD FOR REPAIRING COOLED WORKING VANE OF TURBINE OF GAS-TURBINE ENGINE | 2001 |
|
RU2177863C1 |
METHOD FOR REPAIRING VANE OF JET APPARATUS OF TURBINE OF GAS-TURBINE ENGINE | 2001 |
|
RU2177862C1 |
METHOD FOR RESTORING SECTORS OF SPLIT RING OF NOZZLE APPARATUS OF TURBINE OF GAS-TURBINE ENGINE | 2001 |
|
RU2194604C1 |
METHOD OF APPLICATION OF WEAR-RESISTANT COATING ON BANDAGE SHELTER OF SHOULDER OF TURBOMASHES FROM NICKEL ALLOYS | 2016 |
|
RU2641210C1 |
GAS TURBINE ENGINE PART WITH THE THIN-WALLED ELEMENT RESTORATION METHOD | 2017 |
|
RU2676937C1 |
METHOD OF RESTORATION OF LENGTH OF AIRFOIL PORTION OF BLADES OF GAS-TURBINE ENGINE COMPRESSOR | 0 |
|
SU1734977A1 |
METHOD FOR RESTORING LENGTH OF BLADES OF COMPRESSOR OF GAS TURBINE ENGINE AND APPARATUS FOR PERFORMING THE SAME | 1998 |
|
RU2153965C1 |
TURBOMACHINES BLADES SHROUDS FROM HEAT-RESISTANT NICKEL ALLOYS RECONSTRUCTION METHOD | 2017 |
|
RU2667110C1 |
METHOD OF RECOVERY OF VANE FEATHER LENGTH OF GAS-TURBINE ENGINE | 1998 |
|
RU2138382C1 |
METHOD FOR REPAIRING COMBS OF LABYRINTH SEALS OF TURBOMACHINE BLADES | 2006 |
|
RU2317182C1 |
Authors
Dates
2002-02-27—Published
2001-07-05—Filed