The Frame 9E combustion liner provides the inner combustion passage within the MS9001E gas turbine combustion system. Its perforated wall, head-end arrangement and outlet features work together to establish the flame-containing space and admit air at defined locations. OBT supports custom manufacturing projects for this component family, with the exact configuration established through technical review.
For MS9001E liner work, OBT reviews the head-end plate, central opening, circumferential hole patterns and end connections. The specified part revision establishes the required geometry, material and surface-treatment requirements for the required component revision.
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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