FIELD: metallurgy.
SUBSTANCE: invention can be used in aircraft instrument making with manufacturing of high-precision parts. Parts are subject to tempering, artificial aging at 190°C and mechanical operation. Artificial aging is implemented in two stages during 5.5 hours per each, and mechanical operation is implemented after the first stage of aging.
EFFECT: it is reduced process duration and more effectively implemented scantling stabilisation.
1 tbl, 1 ex
| Title | Year | Author | Number |
|---|---|---|---|
| PROCEDURE FOR THERMAL TREATMENT OF HIGH-PRECISION PARTS OF ALLOY AK4-1 ch FOR STABILISATION OF THEIR DIMENSIONS | 2010 |
|
RU2434971C1 |
| METHOD OF THERMAL STABILISATION OF SIZES OF PRECISION INSTRUMENT PARTS FROM D20 HARDENED ALUMINIUM ALLOY | 2011 |
|
RU2461643C1 |
| METHOD OF THERMAL TREATMENT OF STORAGE MADE OF ALUMINIUM ALLOY D16 | 2006 |
|
RU2324000C1 |
| METHOD OF QUENCHING BLANKS FROM D16 ALUMINIUM ALLOY | 2011 |
|
RU2487961C2 |
| PROCEDURE OF QUENCHING CASTS OUT OF ALLOY AK8M | 2008 |
|
RU2385361C1 |
| THERMAL TREATMENT OF CASTINGS OUT OF ALUMINIUM ALLOY PRODUCED BY HIGH PRESSURE DIE-CASTING PROCEDURE | 2005 |
|
RU2398911C2 |
| PROCEDURE FOR TEMPERING CASTS OUT OF CAST ALLOY ON BASE OF ALUMINIUM AK7pch | 2008 |
|
RU2397273C1 |
| METHOD OF THERMAL TREATMENT OF ALUMINIUM-LITHIUM WASED ALLOYS | 0 |
|
SU707373A1 |
| METHOD OF HEAT TREATMENT OF THE LAP | 0 |
|
SU1735393A1 |
| METHODS FOR THERMOMECHANICAL TREATMENT OF CONDUCTIVE Al-Mg-Si SYSTEM ALLOYS | 2019 |
|
RU2749601C2 |
