The Frame 6B combustion liner forms the inner combustion chamber of the MS6001B gas turbine combustion system. The perforated cylindrical wall admits air at defined locations, and the head-end and outlet features establish the liner's connection with adjacent combustion hardware. OBT supports custom manufacturing projects for this component family, with the exact configuration established through technical review.
For custom MS6001B liner work, the engineering review covers the perforated wall, formed body sections, central opening, side-port locations and slotted end features. Wall geometry and connection dimensions are established from the specified configuration before process planning.
OBT combines high-temperature-alloy sheet-metal fabrication with forming, laser cutting, welding and heat-treatment resources. CNC machining can be integrated for designated interfaces, with coordinate measurement and material inspection used to verify the agreed production requirements. The fabrication route is selected to suit the approved liner design.
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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