METHOD FOR REPAIR AND MANUFACTURE OF GAS TURBINE ENGINE COMPONENTS AND GAS TURBINE ENGINE COMPONENTS REPAIRED OR MANUFACTURED WITH ITS USE Russian patent published in 2017 - IPC B23P6/00 B23K35/30 

Abstract RU 2635688 C2

FIELD: engines and pumps.

SUBSTANCE: after pre-welding preparation of base metal of component under repair, a transition layer is applied by fusion welding using a first additive material based on nickel containing from about 0.05 to about 1.2 wt % of boron and other alloying elements. Thermal treatment of transition layer providing diffusion of boron into base metal is carried out. An oxidation-resistant upper layer is applied to the transition layer using a second additive material based on nickel containing, wt %: 3-6 Al, 0.5-6 Si, 12-25 Cr and other alloying elements. Post-welding heat treatment is carried out to relieve stresses of the base material and restore the geometry of repaired area.

EFFECT: conducting fusion welding at ambient temperature, simplified repair technology and reduction of its cost.

18 cl, 4 dwg, 4 tbl, 3 ex

Similar patents RU2635688C2

Title Year Author Number
NICKEL-BASED SUPERALLOY REINFORCED WITH GAMMA-STROKE PHASE, ITS USE AND METHOD FOR PRODUCTION OF COMPONENTS OF GAS TURBINE ENGINE 2018
  • Goncharov Aleksandr B.
  • Liburdi Dzho
  • Lauden Pol
RU2777822C2
METHOD OF CLADDING AND FUSION WELDING OF SUPERALLOYS 2012
  • Goncharov Alexander B.
  • Liburdi Joseph
  • Lowden Paul
  • Hastie Scott
RU2610198C2
PRECIPITATION STRENGTHENED NICKEL BASED WELDING MATERIAL FOR FUSION WELDING OF SUPERALLOYS 2013
  • Goncharov Alexander B.
  • Liburdi Joseph
  • Lowden Paul
RU2679503C2
COMPOSITION WELDING WIRE 2012
RU2613006C2
DUCTILE BORON-BEARING NICKEL BASED WELDING MATERIAL 2014
  • Goncharov Alexander B.
  • Liburdi Joseph
  • Lowden Paul
RU2666822C2
METHOD OF REPAIRING A COOLED BLADE FROM A HEAT-RESISTANT SUPERALLOY OF A TURBINE OF A GAS TURBINE ENGINE 2018
  • Fursenko Evgenij Nikolaevich
  • Kotelnikov Albert Viktorovich
  • Kurchev Aleksej Igorevich
  • Ivanov Artem Mikhajlovich
RU2686499C1
TURBINE ENGINE COMPONENT MANUFACTURING METHOD 2015
  • Mottin Jean-Baptiste
RU2703666C2
LOCALIZED REPAIR OF THE COMPONENT FROM SUPERALLOY 2014
  • Bruk Dzherald Dzh.
  • Kamel Akhmed
RU2624884C2
METHOD FOR RESTORING THE CHORD LINE OF THE FEATHER FROM A HEAT-RESISTANT NICKEL ALLOY 2022
  • Fursenko Evgenii Nikolaevich
  • Ivanov Artem Mikhailovich
  • Kotelnikov Albert Viktorovich
  • Starkov Dmitrii Aleksandrovich
RU2791745C1
METHOD FOR RESTORING THE END PART OF THE FEATHER OF A COOLED TURBINE BLADE OF A GAS TURBINE ENGINE 2021
  • Ermolaev Aleksandr Sergeevich
  • Kotelnikov Albert Viktorovich
  • Fursenko Evgenij Nikolaevich
  • Yasinetskij Vadim Vladislavovich
  • Ivanov Artem Mikhajlovich
  • Starkov Dmitrij Aleksandrovich
RU2770156C1

RU 2 635 688 C2

Authors

Goncharov Aleksandr B.

Liburdi Dzho

Lauden Pol

Dates

2017-11-15Published

2015-11-02Filed