FIELD: process engineering.
SUBSTANCE: invention relates to production of gas turbine blades. In compliance with this method, blades are produced by making channels in blade body to fit inserts of copper alloy therein. Then, blank is forged and said inserts are withdrawn by chemical dissolution.
EFFECT: fast and efficient production, higher mechanical and chemical properties.
5 cl, 2 dwg
Title | Year | Author | Number |
---|---|---|---|
METHOD OF MANUFACTURE OF REINFORCING INSERTS FOR ALUMINIUM PISTONS OF INTERNAL COMBUSTION ENGINES | 0 |
|
SU1683866A1 |
METHOD OF FABRICATING WIDE-CHORD HOLLOW VANE OF GAS TURBINE ENGINE COMPRESSOR | 2009 |
|
RU2417147C1 |
METHOD TO PRODUCE BLADES OF GAS TURBINE ENGINE | 2013 |
|
RU2551333C1 |
METHOD FOR MAKING HOLLOW METALLIC OBJECTS | 1997 |
|
RU2210478C2 |
MANUFACTURING METHOD OF SYSTEM CONTAINING MANY BLADES INSTALLED IN PLATFORM | 2010 |
|
RU2532783C2 |
METHOD FOR PROCESSING RODS MADE OF ORTHO-TITANIUM ALLOYS FOR PRODUCING BLADES OF A GAS TURBINE ENGINE COMPRESSOR | 2021 |
|
RU2761398C1 |
METHOD OF MANUFACTURING GAS TURBINE ENGINE BLADE FROM TIAL | 2016 |
|
RU2706933C2 |
METHOD OF REPAIR OF GUIDE VANES ASSEMBLY OF GAS-TURBINE ENGINE COMPRESSOR | 1996 |
|
RU2109176C1 |
MAGNESIUM ALLOY-MADE PART (OPTIONS), AIR PUMP WITH ELECTRIC ACTUATOR, SOLUTION FOR PREPARING ANTICORROSIVE COATING, AND METHOD OF MANUFACTURING MAGNESIUM- ALLOY PART | 1999 |
|
RU2171861C2 |
ALUMINIUM ZINC PLATING | 2012 |
|
RU2610811C9 |
Authors
Dates
2013-11-10—Published
2009-03-17—Filed