Cov hlau no yog cua melted npib tsib xee-puag alloy, tau tsim los ntawm Rolls Royce (1971) Ltd. los muab cov ntaub ntawv uas tuaj yeem tsim tau yooj yim thiab yuav muab kev txhim kho ductility hauv welded sib dhos los hloov NIMONIC alloy 80A. kom ua tau raws li cov qauv tsim tshwj xeeb hauv cov ntsiab lus ntawm cov pov thawj kev ntxhov siab thiab lub zog creep.Nws yog tam sim no muaj nyob rau hauv tag nrho cov qauv qauv.Cov txheej txheem vuam rau cov hlau no zoo ib yam li cov siv rau lwm cov hnub nyoog-hardenable npib tsib xee puag alloys.uring salvage welding operations, pre-welding heat-treatment tsis tsim nyog rau lub hnub nyoog-hardened sib dhos tab sis lub hnub nyoog tom ntej-hardening kev kho mob yog xav tau tom qab tag nrho cov salvage welding tiav. Cov khoom yuav muaj hnub nyoog hauv kev pabcuam yog tias kub siab tshaj 750 degree.
C | Cr | Ni | Fe | Mo | Cu | Al | Ti |
0.04-0.08 Nws | 19.0-21.0 Nws | tshuav nyiaj li cas | ≦ 0.7 | 5.6-6.1 | ≦ 0.2 | ≦ 0.6 | 1.9-2.4 Nws |
Co | Bi | B | Mn | Si | S | Ag | Pb |
19.0-21.0 Nws | ≦0.0001 | ≦0.005 | ≦ 0.6 | ≦ 0.4 | ≦0.007 | ≦0.0005 | ≦0.002 |
Qhov ntom (g / cm3) | Melting point (℃) | Tshwj xeeb kub muaj peev xwm (J / kg ℃) | Hluav taws xob resistivity (Ω·cm) | Thermal expansion coefficient (20-100 ℃) / K |
8.36 ib | 1300-1355 Nws | 461 ib | 115 × 10 E-6 | 10.3 × 10 E-6 |
Ntsuas kub ℃ | Tensile zog MPa | Yield zog (0.2 tawm taw tes) MPa | Elongation % | Lub shrinkage ntawm cheeb tsam % | Kinetic Young's Modulus GPa |
20 | 1004 | 585 ib | 45 | 41 | 224 |
300 | 880 ua | 505 | 45 | 50 | 206 |
600 | 819 ib | 490 ib | 43 | 50 | 185 |
900 | 232 | 145 | 34 | 58 | 154 |
1000 | 108 | 70 | 69 | 72 | 142 |
•High-strength alloy, nag lossis daus hardening.
•Lub formability ntawm alloy nyob rau hauv daim ntawv thov vuam yog zoo
•Zoo heev ductility.
Nimonic 263 Daim Ntawv Thov:
Haum rau kev tsim steel qauv thiab aircraft cav thiab roj turbine Cheebtsam.