scholarly journals Fast solution heat treatment of high strength aluminum alloy sheets in radiant heating furnace during hot stamping

Author(s):  
Yong Liu ◽  
Bin Zhu ◽  
Yilin Wang ◽  
Shiqi Li ◽  
Yisheng Zhang
Author(s):  
Liliang Wang ◽  
Jun Liu ◽  
Jianguo Lin

Aluminum alloy components are important contribution to lightweight transportations for improving energy efficiency. However, formability of aluminum alloys at room temperature often hinders their further applications in the automotive, rail, or aerospace industries. The solution heat treatment, forming, and in-die quenching (HFQ®) process is an advanced forming technology that performs both forming and heat treatment simultaneously in a single operation. Since its inception, a significant amount of research has been made on the process to develop it further and to assess the feasibility of using it to form components with increasingly complicated geometries, from a growing variety of alloys. This entry summarizes the HFQ® research work, with the emphasis on the development, modeling, and applications of the technology for stamping complex-shaped high-strength aluminum panel components.


Author(s):  
S Wiesenmayer ◽  
M Merklein

Shear-clinching has proven to be a suitable technology for joining of high-strength materials. However, the mechanical properties of the upper joining partner are limited due to the high strains, which occur during the process. Therefore, shear-clinching of the high-strength aluminum alloy AA7075 in the T6 temper is not possible. Yet, the mechanical properties of hardenable alloys of the 7000 series can be influenced by a heat treatment. Thus, within the scope of this work, the joinability of the high-strength alloy AA7075 in shear-clinching processes in dependance of its temper is investigated. The as fabricated state F, the artificially aged T6 temper, a paint baked state and the naturally aged T4 temper are compared to the fully solution annealed W temper as well as to a retrogression heat-treated state. For retrogression heat treatment, a laser is used as heat source, heating up the alloy for a short term in order to only partially dissolve precipitations. The resulting mechanical properties are determined with uniaxial tensile tests. Moreover, the influence of the mechanical properties of AA7075 on the shear-clinching process, the joint formation and the resulting joint strength is analyzed.


Alloy Digest ◽  
1986 ◽  
Vol 35 (7) ◽  

Abstract UNS No. A97075 is a wrought precipitation-hardenable aluminum alloy. It has excellent mechanical properties, workability and response to heat treatment and refrigeration. Its typical uses comprise aircraft structural parts and other highly stressed structural applications where very high strength and good resistance to corrosion are required. This datasheet provides information on composition, physical properties, hardness, elasticity, tensile properties, and shear strength as well as fatigue. It also includes information on low temperature performance as well as forming, heat treating, and machining. Filing Code: Al-269. Producer or source: Various aluminum companies.


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