The Frame 6FA.03 transition piece links the combustor outlet to the downstream turbine gas path. Its curved passage modifies the flow-section shape and orientation between the combustion hardware and the turbine inlet interface. OBT supports custom manufacturing projects for this component family, with the precise configuration determined via technical review.
The inlet and outlet profiles, curved passage, perforated wall zones, supports, and flange geometry are assessed collectively as a single gas-path component. OBT defines the manufacturing specifications based on the required liner connection and downstream interface, including mutually agreed sealing and locating features.
OBT offert processus pro alliatis ad altas temperaturas, fabricatio, soldatio et machinatio praecisa pro componentibus turbinum ad mensuram. Via ad partem transitionis elaboratur circa formam ductus et geometriam connexionis, utendo sectionibus fabricatis vel subcomponentibus fusis ubi idoneum est. Mensurae dimensionales, verificatio materiae et requisita inspectio nondestructiva convenita in planum qualitatis proiecti includuntur.
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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