The Frame 6F LEC III combustion system integrates fuel-entry hardware, a defined combustion passage and the surrounding assembly features within the relevant F-class arrangement. Its system configuration governs how the individual parts connect and how the hot-gas passage is established. OBT supports custom development and manufacturing of selected components for the specified combustion arrangement.
For a 6F LEC III scope, the head-end interfaces, liner body, supports and downstream connection are reviewed as an assembly relationship. The manufacturing definition identifies the selected components and their mating geometry for the specified 6F configuration.
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.
Please provide 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.
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