کد مقاله کد نشریه سال انتشار مقاله انگلیسی نسخه تمام متن
1578730 1514820 2011 8 صفحه PDF دانلود رایگان
عنوان انگلیسی مقاله ISI
Strengthening mechanisms of carbon in modified nickel-based superalloy Nimonic 80A
موضوعات مرتبط
مهندسی و علوم پایه مهندسی مواد دانش مواد (عمومی)
پیش نمایش صفحه اول مقاله
Strengthening mechanisms of carbon in modified nickel-based superalloy Nimonic 80A
چکیده انگلیسی

Nickel-based superalloy Nimonic 80A with various carbon contents has been developed. Various strengthening mechanisms of carbon were analyzed by optical microscope, X-ray diffraction, scanning electron microscope equipped with energy dispersive spectroscopy and transmission electron microscope. Detailed microstructural analysis revealed that with the increase of carbon content from 0.01% to 0.10%, both the lattice parameters of γ′ and γ phases decreased, and the misfit δ between the coherent γ′ and γ phases increased slightly from 0.289% to 0.317% after full heat treatment at 1070 °C/8 h, A.C. + 700 °C/16 h, A.C. The diameter of spherical γ′ phase decreased from 22.24 nm of 0.01%C alloy to less than 15.76 nm of 0.06%C and 0.10%C alloys. Cr23C6 carbide precipitated at the grain boundary in the alloys with carbon content higher than 0.06%, and when carbon content increased to 0.10%, Cr23C6 carbide had an orientation relationship with the γ   matrix: [001¯] Cr23C6[001¯]γ matrix and(100) Cr23C6 (1 0 0) γ matrix, which can enforce the grain boundary strength. The growth of room temperature tensile strength with the increase of carbon content was primarily due to the coherent strain strengthening and the precipitate strengthening of Cr23C6 carbide. After stress-rupture test at 750 °C/310 MPa, the misfit δ increased from 0.182% to 0.237% with the increase of carbon content, but the values were lower than those after full heat treatment. The precipitate of blocky Cr23C6 in 0.10%C alloy tended to become spherical and dislocation lines were found in the γ matrix channels between γ′ phases, the combination of the dislocation strengthening and precipitate strengthening of Cr23C6 carbide at grain boundary was beneficial to the stress-rupture properties.


► Misfit δ between γ′ and γ phases increased with the increase of carbon content.
► Cr23C6 has an orientation relationship with the γ matrix for the 0.10%C alloy.
► Cr23C6 at grain boundary enhance the grain boundary strengthening.
► Dislocation networks and precipitate strengthening benefit stress-rupture properties.

ناشر
Database: Elsevier - ScienceDirect (ساینس دایرکت)
Journal: Materials Science and Engineering: A - Volume 528, Issues 13–14, 25 May 2011, Pages 4600–4607
نویسندگان
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