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Combustion Liner

Updated: 2026-08-05

Overview

The combustion chamber liner is a cylindrical or annular component that forms the inner wall of a gas turbine or jet engine's combustion section. It directly encounters flame temperatures exceeding 1,500°C while maintaining structural stability. Modern liners utilize advanced cooling techniques like film cooling and thermal barrier coatings to extend service life. In aerospace applications, these liners are precision-engineered to minimize weight while maximizing heat resistance. Industrial versions for power generation turbines often prioritize durability over weight savings, with thicker walls and reinforced designs.

Structure and Working Principle

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Typical liners feature a double-wall construction with intricate cooling channels between layers. The inner wall faces combustion gases, while the outer wall interfaces with the compressor discharge air. This design creates a protective film of cooler air along the hot surfaces. Perforations (dilution holes) are strategically placed to control airflow distribution, ensuring complete fuel combustion while preventing flame attachment. Some advanced models incorporate transpiration cooling systems where air permeates through porous metal walls.

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Key Features

Modern combustion liners exhibit three critical characteristics: thermal fatigue resistance to handle repeated heating/cooling cycles, oxidation resistance against hot corrosion from combustion byproducts, and creep resistance to prevent deformation under sustained loads. Ceramic matrix composite (CMC) liners are gaining adoption for their ability to operate at temperatures 200-300°C higher than metal alloys. These typically combine silicon carbide fibers with a ceramic matrix, offering both strength and thermal protection.

Application Areas

Primary applications include aircraft engines (both commercial and military), land-based power turbines, and marine propulsion systems. In industrial settings, they're found in refinery heaters and large-scale process heaters. The aerospace sector accounts for approximately 60% of high-performance liner demand, driven by stringent efficiency requirements. Industrial applications often use segmented liners for easier maintenance in large-diameter combustion systems.

Maintenance and Precautions

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Regular borescope inspections should check for: hot spots (discoloration), crack initiation near cooling holes, and coating spallation. Thermal cycling is the primary failure mode, making startup/shutdown procedures critical for longevity. Storage recommendations include climate-controlled environments to prevent moisture absorption (for CMC liners) and protective caps for open ends. During handling, avoid impacts that could compromise cooling channel integrity or coating adhesion.

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B2B Procurement Guide

When sourcing combustion liners, verify the manufacturer's certification for aerospace (AS9100) or industrial (ISO 9001) standards as applicable. Lead times for custom designs typically range 8-16 weeks due to complex fabrication processes. Key procurement considerations should include: compatibility with existing fuel injectors, cooling airflow requirements, and expected maintenance intervals. For retrofit projects, ensure dimensional conformity with legacy combustion hardware to avoid costly modifications.

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