The Frame 5 combustion liner forms the flame-containing section of the MS5001 gas turbine combustor. Its cylindrical body provides a defined combustion space, while openings along the wall admit air into the hot-gas stream. The liner connects the head-end combustion hardware with the downstream gas path. OBT supports custom manufacturing projects for this component family, with the exact configuration established through technical review.
The production review covers the head-end plate, cooling and dilution openings, side ports, seams and outlet retention features. The required MS5001 configuration determines wall geometry, local interface dimensions and the acceptance criteria for the completed liner.
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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