I-NIMONIC® alloy 75 iyingxubevange engu-80/20 nickel-chromium enezengezo ezilawulwayo ze-titanium ne-carbon.Yaqala ukwethulwa ngeminyaka yawo-1940s kuma-turbine blades ezinjinini ze-Whittle jet eyisibonelo, manje isisetshenziswa kakhulu izinhlelo zokusebenza ezibiza i-oxidation kanye nokumelana nokukala okuhambisana namandla aphakathi nendawo emazingeni okushisa aphezulu okusebenza.Isasetshenziswa ebunjiniyela be-turbine yegesi kanye nasekucutshungulweni kokushisa kwezimboni, izingxenye zesithando somlilo kanye nemishini yokwelapha ukushisa.Akhiwe kalula futhi ashiselwe
Ingxubevange | % | Ni | Cr | Fe | Co | C | Mn | Si | Ti |
I-Nimonic 75 | Okuncane. | Ibhalansi | 18.0 | - | - | 0.08 | - | - | 0.2 |
Ubukhulu. | 21.0 | 5.0 | 0.5 | 0.15 | 1.0 | 1.0 | 0.6 |
Ukuminyana | 8.37 g/cm³ |
Iphoyinti lokuncibilika | 1340-1380 ℃ |
Isimo | Amandla aqinile I-Rm (i-anneal) (MPa) | Amandla esivuno (ukukhipha) (MPa) | Ukwelula Njengo-% | I-Elastic module (GPA) |
Ukwelashwa kwesixazululo | 750 | 275 | 42 | 206 |
Ibha/Induku | Intambo | I-Strip/Ikhoyili | Ishidi/Ipuleti | Ipayipi/Ipayipi |
BSHR 5, BS HR 504, DIN 17752, AECMA I-PREN2306, AECMA PrEN2307, AECMA I-PREN2402, ISO 9723-25 | BS HR 203, DIN 17750, AECMA PrEN2293, AECMA I-PREN2302, AECMA PrEN2411, ISO 6208 | I-BS HR 403, DIN 17751, I-AECMA PrEN2294, ISO 6207 |
•Ukushisela okuhle
•Ukucutshungulwa okuhle
•Ukumelana nokugqwala okuhle
•Izakhiwo ezinhle zemishini
•Ukumelana okuhle kwezinga lokushisa eliphezulu
•I-fastener ye-Aeronautical
•Ubunjiniyela be-turbine yegesi
•Izingxenye zesakhiwo sesithando somlilo sezimboni
•Imishini yokwelapha ukushisa
•Ubunjiniyela benuzi