0102030405
UHLELO LWEKHEMICAL
ISITHUBA | % | C | Cr | Kwi | Co | Kuba | Al | Kwe | B | Zr | Fe | Mnu | Kwaye | P | S | Nge | Nge | Nge | Pb |
GH105 | MIN | 0.12 | 14.0 | ibhalansi | 18.0 | 4.5 | 4.5 | 1.18 | 0.0030 | 0.07 | - | - | - | - | - | - | - | - | - |
MAX | 0.17 | 15.7 | ibhalansi | 22.0 | 5.5 | 4.9 | 1.50 | 0.010 | 0.15 | 1.0 | 0.4 | 0.25 | 0.015 | 0.010 | 0.0005 | 0.2 | 0.0001 | 0.0010 |
Iipropati Zomzimba
ukuxinana | Indawo yokunyibilika |
7.97g/cm3 | 1340-1380℃ |
IMALI yemveliso
I-GH105 yi-Ni-Co-Cr esekelwe kwi-deposition deformation enzima kwi-alloy yobushushu obuphezulu kunye nobushushu obusebenzayo be-750℃-950℃. Ubushushu begumbi le-alloy kunye namandla obushushu obuphezulu buphezulu, umsebenzi wokumelana ne-oxidation ubalaseleyo, kodwa umsebenzi wokulungisa ubushushu kunye nomsebenzi we-welding jikelele. Isebenza ekwenziweni kwamagqabi einjini ye-aero-injini, iibholithi zobushushu obuphezulu kunye nezinye iindawo ezinobushushu obuphezulu. Iimveliso eziphambili ziquka imivalo eshushu kunye neeflethi, imivalo epholileyo ebandayo, iiprofayili kunye namakhonkco.
Isicelo semveliso
I-alloy isetyenziswe ekwenzeni iiblade ze-injini ye-aero-injini, izitywina zefeni kunye neebholithi zobushushu obuphezulu kunye nezinye iindawo, kunye nemveliso yebhetshi elungileyo kunye nokusetyenziswa. Ukuxhatshazwa kwe-deformation ye-alloy kukhulu, kwaye kufuneka kuthintelwe ekuqhekekeni ngexesha lokukhwabanisa kunye ne-rolling, kunye ne-bar-drawn-drawn bar ifanelekile kwiqondo lokushisa elimalunga ne-600 ° C. I-alloy ikwasetyenziswa ekwenzeni iiblade ze-injini ye-aero-injini, izitywina zefeni kunye neebholithi zobushushu obuphezulu.

