FIELD: mechanical engineering; method of manufacture (versions) of the details or semi-finished products containing the intermetallic titanium-aluminide alloys.
SUBSTANCE: the invention is used for manufacture of the rotor disks or the vanes of the turbines to the set of the laminated bodies made out of one or several titanium-aluminide alloys add the coarse outlines with production of the having the enlarged dimensions preform with the geometry of the being manufactured detail or the semi-finished product, then join them to each other for formation of the common body and shape the desirable final form of the common body. The joining and shaping of the final form is exercised within one work operation. Adding of the coarse outlines to the laminated bodies is exercised by the pressure shaping or cutting. Joining of the stockpiled laminated bodies is exercised by the diffusion welding or by the soldering, and the shaping of the final form of the common body is exercised by the forging of the common body. At that the indicated operations may be conducted in the vacuum environment or in the atmosphere of the inert gases. The laminated bodies forming the common body consist of the various titanium-aluminide alloys have the different microstructure and the texture. Orientation of the surfaces of the stockpiled laminated bodies is set concerning the orientation of the direction of the basic loading of the generated final form. The invention allows to manufacture of the products capable to withstand the great loading, possessing the high geometrical stretching and the thermal stability.
EFFECT: the invention ensures manufacture of the products capable to withstand the great loading, possessing the high geometrical stretching and the thermal stability.
34 cl, 8 dwg, 3 ex
Title | Year | Author | Number |
---|---|---|---|
FORGED PART MADE OF BAINITE STEEL AND ITS MANUFACTURING METHOD | 2019 |
|
RU2763027C1 |
METHOD FOR MANUFACTURING HOLLOW BLADE FOR TURBINE MACHINES | 2005 |
|
RU2364486C2 |
ALLOY ON BASE OF TITANIUM ALUMINIDES | 2005 |
|
RU2370561C2 |
METHOD OF MANUFACTURING GAS TURBINE ENGINE BLADE FROM TIAL | 2016 |
|
RU2706933C2 |
METHOD FOR MANUFACTURING OF SEMI-FINISHED SHEET PRODUCT FROM TITANIUM ALLOY | 2006 |
|
RU2320771C1 |
METHOD OF ROLLING PARTS THAT FORM HOLLOW VANE | 2005 |
|
RU2404039C2 |
METHOD OF MANUFACTURE OF DETAIL FROM NICKEL-BASED SUPERALLOY AND DETAIL OBTAINED BY NAMED METHOD | 2010 |
|
RU2531217C2 |
HIGH STRENGTH AND PLASTICITY STEEL SHEETS AND METHOD OF MANUFACTURING THE SAME | 2008 |
|
RU2451764C2 |
METHOD OF MANUFACTURING COMPOSITE WORKPIECES OF DISC-DISC AND DISC-SHAFT TYPE OUT OF HEAT-RESISTANT TITANIUM AND NICKEL ALLOYS | 2015 |
|
RU2610658C2 |
METHOD OF FABRICATION OF THIN SHEETS FROM TWO-PHASE TITANIUM ALLOY AND PRODUCT FROM THESE SHEETS | 2013 |
|
RU2555267C2 |
Authors
Dates
2007-09-20—Published
2005-02-25—Filed