Gas Turbine Transition Duct
Reliable High-Temperature Transition Solutions for Industrial Gas Turbines
Why
Our Transition Ducts Perform Better
Our transition ducts are designed to ensure a smooth and uniform transition of high-temperature combustion gases, minimizing pressure loss and flow distortion before the turbine stage. This helps protect turbine blades and improves overall system efficiency.
Optimized Gas Flow Design
Smooth internal geometry reduces pressure loss and flow distortion, helping protect turbine blades and improve overall efficiency.
High-Temperature Alloy Reliability
Nickel-based superalloys are selected based on real operating conditions to ensure resistance to oxidation, thermal fatigue, and creep.
Designed for Thermal Cycling
Structural design accounts for thermal expansion and cyclic loading, reducing the risk of cracking during frequent start-stop operations.
Consistent Manufacturing Quality
Controlled forming, welding, and heat treatment ensure dimensional accuracy and stable long-term performance.
OEM-Compatible Fit
Manufactured to match OEM interface dimensions, allowing direct replacement without modification or installation issues.
Engineering Support You Can Rely On
From drawing review to material optimization, our engineering team supports your project beyond manufacturing.
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OEM-compatible solutions with engineering support and stable delivery
Gas Turbine Transition Duct Solutions
Engineered for high-temperature reliability, flow stability, and long-term service in industrial gas turbines

Combustor to Turbine Transition Duct
Designed to smoothly guide high-temperature combustion gases from the combustor to the turbine inlet, ensuring uniform flow distribution and reduced thermal stress on downstream components.

Integrated High-Temperature Transition Assembly
Manufactured from nickel-based superalloys to withstand extreme thermal and mechanical loads, providing stable performance and long service life in demanding operating conditions.

Combustor-to-Turbine Transition Duct
Engineered for stable guidance of high-temperature combustion gases from the combustor to the turbine inlet, this transition duct features a robust structure and precise interfaces to ensure reliable operation under continuous thermal and mechanical loading.

Aerodynamically Optimized Transition Duct
Developed through flow and thermal analysis, this transition duct design focuses on uniform gas distribution and reduced pressure loss, helping improve turbine efficiency and extend the service life of downstream hot-section components.