TY - GEN
T1 - Mechanical properties of the AlSi10MnMg alloy with a different content of manganese and magnesium intended for light die-casting
AU - Wieszaa, R.
AU - Pitkowski, J.
AU - Kozuba, J.
N1 - Publisher Copyright:
© 2019 IEEE
PY - 2019/9
Y1 - 2019/9
N2 - The work shows selected mechanical properties (HB; Rm; RP; A) alloy AlSi10MnMg with different Mn content (0.4 and 0.6% mas) Magnesium (0.5; 0,75 and 1,0% mas.) of the m.in. for light pressure casts for the transport industry. The results of the mechanical properties are presented for cast and after T6 machining. It Was found that: The hardness of the test alloys is 105÷118 HB after T6 machining, Rm approx. 320÷340 MPa after T6 in relation to post-pour condition (240 MPa). The increase in the proportion of alloyed additives was also influenced by an increase of Rp to 140 Mpa For alloy AlSi10Mn0, 6MG1, 5 (for casted State) and up to 280 MPA after T6 treatment. It can therefore be concluded that the most in the direction of increase Rp alloys AlSiMnMg is additive 1.0-1.5% mas. Mg and approximately 0.6% of the MAS. Mn. Elongation is approximately 5. The, 5% (for casted state) and approximately 8-9% after the T6 heat treatment.
AB - The work shows selected mechanical properties (HB; Rm; RP; A) alloy AlSi10MnMg with different Mn content (0.4 and 0.6% mas) Magnesium (0.5; 0,75 and 1,0% mas.) of the m.in. for light pressure casts for the transport industry. The results of the mechanical properties are presented for cast and after T6 machining. It Was found that: The hardness of the test alloys is 105÷118 HB after T6 machining, Rm approx. 320÷340 MPa after T6 in relation to post-pour condition (240 MPa). The increase in the proportion of alloyed additives was also influenced by an increase of Rp to 140 Mpa For alloy AlSi10Mn0, 6MG1, 5 (for casted State) and up to 280 MPA after T6 treatment. It can therefore be concluded that the most in the direction of increase Rp alloys AlSiMnMg is additive 1.0-1.5% mas. Mg and approximately 0.6% of the MAS. Mn. Elongation is approximately 5. The, 5% (for casted state) and approximately 8-9% after the T6 heat treatment.
UR - https://www.scopus.com/pages/publications/85074784233
U2 - 10.1109/NTAD.2019.8875512
DO - 10.1109/NTAD.2019.8875512
M3 - Conference contribution
AN - SCOPUS:85074784233
T3 - NTinAD 2019 - New Trends in Aviation Development 2019 - 14th International Scientific Conference, Proceedings
SP - 214
EP - 217
BT - NTinAD 2019 - New Trends in Aviation Development 2019 - 14th International Scientific Conference, Proceedings
A2 - Andoga, Rudolf
PB - Institute of Electrical and Electronics Engineers Inc.
T2 - 14th International Scientific Conference on New Trends in Aviation Development, NTinAD 2019
Y2 - 26 September 2019 through 27 September 2019
ER -