FIELD: restoration processes and equipment, namely restoration of heat pipes having flaws in the form of cracking for combustion chambers of gas turbine engines.
SUBSTANCE: method comprises steps of removing flaws in the form of cracking by mechanically removing of material with formation of groove subjected to further welding on; forming groove having width 1 - 3 mm, length exceeding by 2 - 3 mm length of cracking and depth consisting of 0.3 - 0.5 of thickness of cracked portion.
EFFECT: lowered labor consumption, improved operational reliability of restored heat pipe.
2 cl, 3 dwg, 1 ex
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METHOD FOR RESTORING VANE OF TURBOMACHINE | 1997 |
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GAS TURBINE ENGINE OVERHAUL METHOD (VERSIONS) AND GAS TURBINE ENGINE REPAIRED ACCORDING TO THIS METHOD (VERSIONS), OVERHAUL OF BATCH, RESUPPLIED GROUP OF GAS TURBINE ENGINES AND GAS TURBINE ENGINE REPAIRED BY THIS METHOD | 2013 |
|
RU2555936C2 |
Authors
Dates
2007-12-10—Published
2006-01-30—Filed