![]() The presence and nature of serrations in the stress–strain curves are assessed. The mechanical properties of the material are determined between ☌. In this work, a hot forming procedure of a double-curved component in alloy 718 is studied. The manufacturing process of aero-engine parts in superalloys at temperatures close to 950 ☌ produces reduced stamping force, residual stresses, and springback compared to traditional forming procedures occurring at room temperature. Furthermore, the competitiveness of the aero-engine industry can benefit from reduced production costs and shorter development times while minimizing costly try-outs and increasing the efficiency of engines. The use of lightweight components in load-carrying aero-engine structures has the potential to significantly reduce fuel consumption and greenhouse gas emissions. The demands associated with the production of advanced parts made of nickel-base superalloys are continuously increasing to meet the requirements of current environmental laws.
0 Comments
Leave a Reply. |
Details
AuthorWrite something about yourself. No need to be fancy, just an overview. ArchivesCategories |