The Frame 9F combustion system introduces fuel, establishes the combustion zone and directs the resulting hot-gas flow toward the turbine. Its arrangement includes configuration-specific head-end hardware, a combustion passage and downstream connections. OBT supports custom development and manufacturing of selected components for the specified combustion arrangement.
For a 9F system-related requirement, OBT separates the requested liner, sleeve or support hardware, fuel-entry components and transition interfaces. The exact engine and combustion variant determine the component geometry and the assembly relationships covered by the project.
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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