Temat: vickers hardness - Katalog OPAC zbiorów

Skocz do pozycji: 1.

Tytuł:: The Impact of Damage in Inconel 718 on Hardness Measured by the Vickers Method
Autorzy:: Malicki, M.
Madejski, B.
Powiązania:: https://bibliotekanauki.pl/articles/1203404.pdf
Data publikacji:: 2015
Wydawca:: Sieć Badawcza Łukasiewicz - Instytut Lotnictwa
Tematy:: damage parameter
Vickers hardness
Inconel 718
tensile test
Opis:: To prevent failure of machine components it is necessary to measure material damage generated in a component throughout its entire lifetime. Damage can be quantified by means of damage parameters. This paper considers the usefulness of hardness measurements to evaluate damage parameter in Inconel 718. Vickers hardness tests were performed on a specimen with a variable cross section area after tensile testing. The specimen’s geometry enabled the evaluation of damage parameter in respect of hardness measurements made on one individual specimen.
Źródło:: Fatigue of Aircraft Structures; 2015, 7; 69-79
2081-7738
2300-7591
Pojawia się w:: Fatigue of Aircraft Structures
Dostawca treści:: Biblioteka Nauki

Artykuł

Skocz do pozycji: 2.

Tytuł:: The Impact of Damage in Anneling Inconel 718 on Hardness Measured by the Vickers Method
Autorzy:: Malicki, M.
Gadalińska, E.
Chmiel, M.
Powiązania:: https://bibliotekanauki.pl/articles/98002.pdf
Data publikacji:: 2016
Wydawca:: Sieć Badawcza Łukasiewicz - Instytut Lotnictwa
Tematy:: damage parameter
Vickers hardness
Inconel 718
tensile test
heat treatment
Opis:: In the previous work [1] it was shown that strain hardening had considerable impact on the hardness of Inconel 718. In order to verify the weakening of the material associated with the damage mechanism in the tested material, the hardness tests were performed on the stretched specimen which was subsequently heat treated. The tests revealed that, after heat treatment, the measured hardness was reduced with an increasing degree of the plastic deformation present prior to heat treatment.
Źródło:: Fatigue of Aircraft Structures; 2016, 8; 92-96
2081-7738
2300-7591
Pojawia się w:: Fatigue of Aircraft Structures
Dostawca treści:: Biblioteka Nauki

Artykuł

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