The MS6001 DLN Combustion Liner is a high-performance hot-section component designed for dry low NOx (DLN) gas turbine engines, such as the GE MS6001 series. It forms the internal wall of the combustion chamber, where compressed air mixes with fuel and ignites to produce high-temperature gases that drive the turbine. DLN technology focuses on reducing nitrogen oxide emissions while maintaining combustion stability, making the liner critical for both performance and environmental compliance.
Precision manufacturers like HGTP produce MS6001 DLN combustion liners using advanced machining, high-temperature alloys, and strict quality controls to ensure durability under extreme thermal and mechanical stress.
The combustion liner plays multiple critical roles in the gas turbine:
Maintains a stable flame in the combustion zone while preventing flashback into upstream components.
The internal geometry ensures optimal mixing of compressed air and fuel, enabling efficient combustion with low NOx emissions.
Cooling holes and film cooling channels help manage liner surface temperatures, protecting the material from thermal degradation.
Provides mounting interfaces for fuel nozzles and other internal combustion chamber components.
DLN combustion liners are exposed to extremely high temperatures (up to 1100°C) and thermal cycling. Materials are selected for heat resistance, strength, and oxidation resistance.
Inconel 625
Inconel 718
Hastelloy X
These materials offer:
High-temperature strength
Oxidation and corrosion resistance
Excellent thermal fatigue resistance
AISI 321
AISI 347
Used for lower-stress sections or supporting structures, providing weldability and dimensional stability.
Producing an MS6001 DLN combustion liner involves advanced aerospace and turbine manufacturing techniques:
Precision rolling, hydroforming, or deep drawing creates the cylindrical or segmented geometry.
TIG, laser, or electron beam welding joins multiple liner segments with minimal distortion.
Critical surfaces, mounting flanges, and alignment features are machined to tight tolerances (±0.02 – ±0.05 mm).
Hundreds of precision holes (0.5 – 2 mm diameter) are drilled for film cooling.
Methods include laser drilling, EDM, or high-precision mechanical drilling.
| Parameter | Value |
|---|---|
| Outer Diameter | 300 – 600 mm |
| Wall Thickness | 2 – 4 mm |
| Operating Temperature | 900°C – 1100°C |
| Cooling Hole Diameter | 0.5 – 2 mm |
| Critical Tolerance | ±0.02 – ±0.05 mm |
| Surface Finish | Ra 0.8 – 1.6 μm |
Strict quality assurance is essential for combustion liners in DLN turbines.
CMM ensures precise alignment and concentricity.
Dye penetrant, radiography, and ultrasonic inspections detect cracks, porosity, or weld defects.
Chemical composition, hardness testing, and metallography confirm compliance with turbine specifications.
The MS6001 DLN combustion liner is used in:
GE MS6001 series industrial gas turbines
Power generation plants utilizing DLN technology
Turbine MRO (maintenance, repair, overhaul) operations
Industrial turbine parts manufacturing
Its design ensures high combustion efficiency, long service life, and compliance with strict environmental standards.
Companies like HGTP specialize in producing high-quality turbine hot-section components including:
CNC machining of high-temperature superalloys
DLN combustion liner fabrication
Precision cooling hole drilling and film cooling optimization
Aerospace-grade welding and assembly
These capabilities support both original equipment manufacturing (OEM) and aftermarket turbine MRO requirements, ensuring reliability and efficiency in critical power generation application
Contact: Hangzhou Gas Turbine Parts Co.Ltd
Phone: 15869109368
Tel: 86-571-89967020
E-mail: saels@gas-turbine-parts.com
Add: No151,ZiDingXiang Road Hangzhou City ZheJiang China 310021