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PL
Praca dotyczy badań zmęczenia wysokocyklowego przerabianych plastycznie stopów metali lekkich, mających zastosowanie między innymi w technice lotniczej. Przydatność stopów metali lekkich na elementy konstrukcyjne urządzeń determinowana jest, oprócz ich niskiej gęstości, także szeregiem korzystnych właściwości mechanicznych, a w przypadku zastosowań na elementy środków transportu dodatkowo dobrą wytrzymałością zmęczeniową. Materiał do badań stanowiły pręty po przeróbce plastycznej na gorąco ze stopów magnezu AZ31 i AZ61, dwufazowego stopu tytanu Ti-6Al-4V oraz stopu aluminium 2017A (T451). Do badań zmęczenia wysokocyklowego w warunkach zginania obrotowego przy współczynniku asymetrii cyklu R= −1 wykonano próbki walcowe o średnicy d0=8 mm. Przeprowadzono próby w zakresie ograniczonej wytrzymałości zmęczeniowej. Na podstawie uzyskanych wyników opracowano charakterystyki trwałości zmęczeniowej badanych materiałów. W badaniach zmęczenia wysokocyklowego największą trwałość wykazał stopu tytanu Ti-6Al-4V.
EN
The paper refers to the research on high-cycle fatigue of wrought light metal alloys, applied, inter alia, in the aviation technology. Usefulness of the light metal alloys for various structural components is determined, apart from their low density, by a number of favourable mechanical properties and in the case of their use for components of transport means - additionally by good fatigue strength. The material for the research consisted of hot-worked rods made of AZ31 and AZ61 magnesium alloys, Ti-6Al-4V two-phase titanium alloy and 2017A (T451) aluminium alloy. Cylindrical specimens with a diameter of d0 = 8 mm were made for the fatigue test under high-cycle rotary bending conditions with the cycle asymmetry coefficient R = −1. The tests were carried out for a limited fatigue strength range. Based on the obtained results, fatigue life characteristics of the tested materials were drawn up. It was found that the Ti-6Al-4V alloy has the longest fatigue life.
2
Content available remote Microstructure and properties of FSW joints of 2017A/6013 aluminium alloys sheets
EN
Purpose: The aim of the studies was to analyse the structure and mechanical properties of FSW joints. Experiment were perform in order to study possibilities to join different aluminium alloys 2017A and 6013. The alloys differ one from the other with respect to chemical composition and mechanical properties especially, therefore the ability to perform the correct joints may be useful for special constructions. Design/methodology/approach: The joints were produced applying different parameters and temperatures. The microstructure was studied using optical, scanning electron and transmission electron microscopes. The mechanical properties are discussed with regard to microhardness profiles on the cross-sections of the joints. Findings: No cracks were found in the joints. Weld nuggets were formed in the 2017A alloy which was located on the advancing side during welding. Mixing process of the materials within the joints was observed as a formation of separate regions of the materials being joined. The hardness profiles showed sudden changes of hardness what correlates with structure observations. In the vicinity of the weld nugget higher dislocation density was observed. Lowering the temperature of sheets and welding with intensive cooling caused a decrease in size of the weld nugget. Research limitations/implications: In the further studies, tensile and bending tests are planned. Moreover, an attempt of explaining the influence of precipitates at the regions boundaries on the fracture process. Practical implications: Good quality of the joints can be stated on the basis of structure analysis. The chosen parameters of welding can be considered as proper ones. Originality/value: Comparison of the welding of the alloys2017A and 6013 are not common. The results of studies and conclusions presented in the paper are consecutive data complementing knowledge on FSW of the aluminium alloys. The applied welding parameters ensure good quality of joints with respect to the technology.
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