YL GLOBALYL Global Industrial Trading Pte. Ltd.
Manufacturing Record
A one-ton 7075-T6 shaped forging produced by open-die forging on an 8000 t press.
Engineering case
Component application, material and performance requirements are translated into defined manufacturing controls and documented verification.
Aircraft wing structures
7075-T6 aluminum alloy
For Aircraft wing structures, the Large Shaped Aluminum-Alloy Forging must use 7075-T6 aluminum alloy at 1 t scale while meeting Open-die forged on an 8000 t press; Large asymmetric aerospace geometry. The engineering challenge is coordinated control of the forming-temperature window, heat-treatment response and machining distortion.
The manufacturing strategy controls the aluminum-alloy temperature window, heat-treatment response and machining distortion. Billet condition, heating and deformation parameters, solution ageing and finish-machining allowance are coordinated with material, property, dimensional and surface verification.
Delivery basis: Machined condition. Open-die forged on an 8000 t press; Large asymmetric aerospace geometry are incorporated into the project inspection plan, with final inspection records and the quality dossier supporting acceptance and release.
Material grade and batch traceability
Mechanical-property and heat-treatment verification to the approved specification
UT / PT, dimensional and surface inspection as technically required
Material certificate and heat/lot traceability
Heat-treatment and inspection records
Final dimensional report and release dossier
Related products
Engineering review
Share drawings, material requirements or a development brief for an initial manufacturing-route and verification review.