G.E.® 4124T20G04 Swirler Assembly - Gas Turbine Combustor
GE Engine Services Dist LLC
Part # 4124T20G04=CZ
8130-3 Eligible
8130-3 Eligible
4124T20G04 Swirler Assembly is a critical component located in the head end of a gas turbine combustor. It consists of a series of vanes or guides arranged in a circular pattern to induce a swirling motion in the combustion air.
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Overview
4124T20G04 Swirler Assembly creates a primary zone for igniting the fuel and sustaining the flame. By enhancing the combustion process, it improves the air-fuel mixture and stabilizes combustion, leading to improved overall efficiency. The swirler assembly converts the axial momentum of the incoming air flow into tangential (rotating) momentum, forming low-pressure recirculation zones within the combustion chamber. This swirling motion is essential for stabilizing the flame and ensuring thorough mixing of the fuel and air, which in turn leads to more complete and efficient combustion while suppressing soot formation.
Features & Benefits
Induces swirling motion in combustion air for improved combustion efficiency.
Enhances air-fuel mixture stability for better flame retention.
Forms low-pressure recirculation zones to stabilize the flame.
Helps suppress soot formation, contributing to cleaner operation.
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