FIELD: manufacture and repair of blades of gas- turbine engines, propellers, helicopter blades, rotors and hydrofoils in shipbuilding. SUBSTANCE: method consists in removal of part of blade, cleaning of surface, manufacture of new member whose sizes and shape correspond to these of removed part. Then, surfaces of blade and new member are matched and blade and new member are connected. New member is made in form of perforated cover plate. Then, adhesive is applied on surfaces of blade and new member, adhesive is forced into perforations, thus filling them and forming polymer antierosion coat. EFFECT: extended service life of damaged blade at retained strength. 7 cl, 5 dwg
Title | Year | Author | Number |
---|---|---|---|
WHEEL OF AXIAL TURBOMACHINE | 2002 |
|
RU2241834C2 |
DEVICE TO SUPPLY COOLING AIR TO WORKING OF TURBINE WHEEL | 2004 |
|
RU2289029C2 |
COOLED BLADE FOR GAS TURBINE | 1989 |
|
RU1662175C |
STATOR BLADE TURNING MECHANISM OF AXIAL-FLOW TURBO-MACHINE | 1996 |
|
RU2145391C1 |
AXIAL-FLOW TURBOMACHINE RUNNER | 2005 |
|
RU2296864C1 |
DEVICE FOR FASTENING BLADES OF ROTOR WHEELS OF AXIAL-FLOW TURBOMACHINE | 2006 |
|
RU2315868C1 |
JET ENGINE REVERSER AEROFOIL CASCADE | 1998 |
|
RU2145672C1 |
TURBOMACHINE COMPOSITE BLADE | 1984 |
|
RU1313055C |
JACKET OF TURBOJET ENGINE WITH MULTILAYER PANELS AND DRAINAGE SYSTEM | 2019 |
|
RU2716802C1 |
GAS-TURBINE ENGINE COMBUSTION CHAMBER | 2001 |
|
RU2219440C2 |
Authors
Dates
2001-08-20—Published
1999-08-18—Filed