The Frame 6FA combustion liner forms the inner wall of the combustion passage within the relevant F-class gas turbine arrangement. Its cylindrical body, formed wall sections and local openings establish the combustion space and the interfaces with adjoining hardware. OBT supports custom manufacturing projects for this component family, with the exact configuration established through technical review.
For a 6FA-series liner project, formed wall sections, corrugations, side openings and end connections are reviewed together. The exact engine and combustion revision are identified during engineering review so that family-level appearance is translated into a defined manufacturing requirement.
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.
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.
EN
AR
BG
HR
CS
DA
NL
FI
FR
DE
EL
HI
IT
JA
KO
NO
PL
PT
RO
RU
ES
SV
TL
IW
LV
LT
SR
SK
SL
UK
VI
ET
HU
TH
TR
AF
MS
GA
IS
LA
