YL GLOBALYL Global Industrial Trading Pte. Ltd.
Manufacturing Record
Large aluminum-alloy bar forged on an 8000 t press, then heat treated and machined to a bright surface condition.
Engineering case
Component application, material and performance requirements are translated into defined manufacturing controls and documented verification.
Spacecraft components and precision machinery
6061-T6 / 7075-T6 / 7175
For Spacecraft components and precision machinery, the Aluminum-Alloy Forged Bar must use 6061-T6 / 7075-T6 / 7175 at 1-3 t; diameter 300-800 mm; length 1-5 m scale while meeting Forged on an 8000 t press; Heat treated and bright machined. 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. Forged on an 8000 t press; Heat treated and bright machined 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.