Uthotho lweSuperalloy
0102030405
UHLELO LWEKHEMICAL
ISITHUBA | % | C | Cr | IN | Kuba | Kwi | Al | Kwe | Fe | B | Oku |
|
GH4037 | MIN | 0.03 | 13.00 | 5.00 | 2.00 | 0.10 | 1.70 | 1.80 | - | - |
|
|
MAX | 0.10 | 16.00 | 7.00 | 4.00 | 0.5 | 2.30 | 2.30 | 5.00 | 0.020 | 0.020 |
| |
% | Mnu | Kwaye | S | P | Nge | Pb | Nge | Sn | Sb | Njengoko | Kwi | |
MIN | - | - | - | - | - | - | - | - | - | - | ibhalansi | |
MAX | 0.50 | 0.40 | 0.010 | 0.015 | 0.07 | 0.001 | 0.0001 | 0.0012 | 0.0025 | 0.0025 | ibhalansi |
Iipropati Zomzimba
ukuxinana | Uluhlu lobushushu obunyibilikayo |
p=8.40g/cm | 1278-1346℃ |
IMALI yemveliso
Easy machinability
Amandla aphezulu e-thermal, ukusebenza kakuhle ngokubanzi kunye nokuzinza kwentlangano kwi-850 ℃.
Ukumelana ne-oxidation ephezulu kwi-850 ℃, umbutho ozinzile wokusetyenziswa kwexesha elide.
Ilungele ukusetyenziswa kwexesha elide iiblade ze-injini ye-aero-injini engaphantsi kwe-800~850℃.
Ukusebenza kakuhle kwe-welding
Isicelo semveliso
Ngenxa yamandla aphakathi kwe-thermal kunye nokusebenza kakuhle kokudinwa kwe-thermal ngaphantsi kwe-850 ℃, inokusetyenziswa ngokubanzi kwizicelo ezahlukeneyo ezifunayo.
1.Injini yomoya. 2.Igumbi lokutshisa . 3.Amalungu egumbi lokutsha elongezelelweyo. 4.Imekobume eneAcidic. 5.Iincakuba zokusebenza kweinjini yomoya.
