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.
Pro opus liner MS6001B ad mensuram, recensio technica amplectitur parietem perforatum, sectiones corporis formatas, aperturam centralem, loca portarum laterales et proprietates extremorum fissurarum. Geometria parietis et dimensiones connexionum constituuntur ex configuratione specificata antequam planificatio processus incipiat.
OBT combinat fabricacionem metalli laminaris ex legaturis alti-temperaturae cum formando, incisione laser, soldatura et tractamento calorico. Machinatio CNC potest integrari pro interfacibus designatis, et mensuratio coordinata ac inspectio materialis utuntur ad verificandum requisita productionis consensu approbata. Via fabricandi eligitur ut conveniat designo linerei approbato.
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.
Noster peritus turma venditionis ad consultationem tuam exspectat.
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