FIELD: welding production, possibly turbine manufacture, machine engineering. SUBSTANCE: method comprises steps of mechanically trimming end face of blade vane until complete removal of blackened spots caused by exploitation; then trimming lateral surface of vane adjoining to its end. Width of trimmed lateral surface consists 1-2 width values of vane wall. Prepared surfaces are subjected to abrasive grain blasting until achieving uniform dull color. Occurrence of bright or dark spots is prevented. Blade is mounted and fixed in water cooled attachment. Electric-arc gas-shield surfacing of end of vane is realized with use of non-consumable electrode by means of constant value and sign electric current. Electric arc is ignited in water cooled attachment and it is transferred to additive metal for further surfacing end of blade along it. EFFECT: enhanced strength of surfaced blade due to optimal state of surfaced faces of vane. 2 cl, 1 tbl
Title | Year | Author | Number |
---|---|---|---|
METHOD FOR RESTORING LENGTH OF BLADES OF COMPRESSOR OF GAS TURBINE ENGINE AND APPARATUS FOR PERFORMING THE SAME | 1998 |
|
RU2153965C1 |
METHOD OF RECOVERY OF VANE FEATHER LENGTH OF GAS-TURBINE ENGINE | 1998 |
|
RU2138382C1 |
METHOD FOR REPAIRING COOLED WORKING VANE OF TURBINE OF GAS-TURBINE ENGINE | 2001 |
|
RU2177863C1 |
METHOD OF WELDING OR SURFACING OF HEAT-RESISTANT HIGH ALLOYS | 1998 |
|
RU2146988C1 |
METHOD OF RESTORATION OF LENGTH OF AIRFOIL PORTION OF BLADES OF GAS-TURBINE ENGINE COMPRESSOR | 0 |
|
SU1734977A1 |
METHOD FOR REPAIRING CONTACT SURFACE OF BANDAGE FLANGE OF WORKING VANE OF TURBINE | 2001 |
|
RU2179915C1 |
METHOD OF FUSING HEAT-RESISTANT HIGH ALLOY | 2004 |
|
RU2257285C1 |
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 REPAIRING A COOLED BLADE FROM A HEAT-RESISTANT SUPERALLOY OF A TURBINE OF A GAS TURBINE ENGINE | 2018 |
|
RU2686499C1 |
Authors
Dates
2002-10-10—Published
1999-06-28—Filed