The Frame 6B DLN combustion system combines fuel-entry hardware, the combustion liner and downstream gas-path connections in a configuration intended for dry low NOx operation. The designation describes the combustion arrangement; individual component selection depends on the installed version and its interface details. OBT supports custom development and manufacturing of selected components for the specified combustion arrangement.
System-related work starts by separating the liner, cap, fuel-entry and transition-interface requirements. OBT then reviews the requested part scope against the identified DLN configuration, establishing which components and mating dimensions need to be included in the production definition.
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.
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