Stabilization and landing braking during landing and takeoff,located on aircraft wings
the so-called flap and spoiler, composite, aluminum alloys,etc.
It is produced from materials.
Two different aircraft firms, precipitation hardening on the samealuminum alloy material
They wanted to produce these parts by applying (aging) heattreatment. Heat treatment
As a result of mechanical tests on applied parts, mechanical partsof a firm
strength was found to be lower than that of the other firm.made
In the examinations, in the aging heat treatment of this problem,some companies
since they take the size (s) of their parameters different fromeach other
It was determined that it originated due to (their choice).
a) The parts produced by the two companies have differentmechanical strength, aging thermal
What parameters might have affected the process? (10 points)
b) Materials science, which causes this difference in mechanicalproperties.
(Microstructure formations, etc.) in terms of evaluation andexplain. (20 points)
