Fuel Nozzle
Scheme
MT-280
Considering the strict requirements of the aero-engine on the mechanical properties and high temperature resistance of the material, Avimetal chooses MT-GH3536 with excellent performance, carries out powder composition optimization, aiming at the problems of alloy cracking in the deposition state and low elongation at high temperature, so as to achieve the elimination of powder micro-cracking.
Reasonable structure design & optimized component structure
Result
Reasonable structure design, multi-component integration and overall weight reduction of key engine parts
Efficiency of a certain type of aircraft engine improved