G.E.® 1968M38P02 Splash Plate is a critical component of the combustor dome assembly in widebody aircraft engines, designed to protect the engine structure from extreme heat while managing airflow for efficient combustion and cooling.
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Overview
1968M38P02 Splash Plate serves as a thermal barrier and airflow management device within General Electric (GE) aircraft turbine engines. Positioned to shield the main combustor dome from the intense heat of the combustion flame, it also strategically directs compressed air to ensure efficient cooling and optimal fuel-air mixing. This design is essential for maintaining engine integrity and performance under demanding operational conditions.
Features & Benefits
Protects the engine structure from extreme heat during combustion.
Acts as a thermal barrier to enhance engine durability.
Manages airflow for efficient combustion and cooling.
Designed for use in widebody aircraft engines for reliability.
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