The Frame 9E LEC III combustion system brings fuel-entry hardware, the combustion liner and downstream transition connections into a defined assembly. The system layout establishes the relationship between individual components and the gas path toward the turbine inlet. OBT supports custom development and manufacturing of selected components for the specified combustion arrangement.
Proiectul 9E LEC III începe cu lista componentelor necesare și interfețele de asamblare. OBT analizează locațiile de montare, secțiunile de căptușeală, conexiunile din capătul frontal și relațiile de tranziție pentru a defini materialul, traseul de producție și cerințele de acceptare pentru echipamentele selectate.
OBT supports turbine-component projects through alloy processing, casting, forming, welding, CNC machining and inspection resources. For a system-related scope, these capabilities are applied to the selected parts and mating interfaces identified in project review. Material verification, coordinate measurement and agreed weld or other inspections help define the production acceptance plan.
Pls providere engineering drawings or a representative physical sample for quotation and technical review. If drawings are unavailable, OBT can evaluate the sample for reverse engineering. The material, critical dimensions, quantity and inspection requirements are agreed with the customer before production.
Noster peritus turma venditionis ad consultationem tuam exspectat.
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