This low-pressure turbine disk serves as a robust mounting platform for blade roots and safety mechanisms. Constructed from super alloys, it withstands high temperatures and stresses while minimizing vibrations. It features internal cooling passages for heat dissipation and is designed for easy replacement, meeting specific design requirements.
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Overview
Stage 1 low-pressure turbine disk is a sturdy structure that serve as mounting platform to accommodate the blade roots and safety locking mechanisms. The turbine disk is made of super alloys to withstand high-temperatures, mechanical and thermal stresses that ensure structural integrity. The turbine disk rotor is also designed to minimize the vibrations and imbalances that occur as a result of heavy centrifugal forces acting upon the disk. The turbine disk also has internal cooling passages to dissipate the excess heat in the turbine. Part number 301-331-126-0 meets the specific design requirement for easy replacements, and their robustness assists the turbine in achieving overall efficiency.
Technical Information
ATA Number
72
ATA Chapter
Engine Turbine / Turbo Prop Ducted Fan / Unducted Fan
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