Abstract:
The work shows selected mechanical properties (HB; \mathbf{R}_{\mathbf{m}};\ \ \mathbf{R}_{\mathbf{P}}; A) alloy AlSi10MnMg with different Mn content (0.4 and 0.6% mas)...Show MoreMetadata
Abstract:
The work shows selected mechanical properties (HB; \mathbf{R}_{\mathbf{m}};\ \ \mathbf{R}_{\mathbf{P}}; 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\div 118 HB after T6 machining, \mathbf{R}_{\mathbf{m}} approx. 320\div 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 \mathbf{R}_{\mathbf{P}} 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 \mathbf{R}_{\mathbf{P}} 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.
Published in: 2019 New Trends in Aviation Development (NTAD)
Date of Conference: 26-27 September 2019
Date Added to IEEE Xplore: 21 October 2019
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