G.E.® 2116M75P01 Stage 1 High Pressure Turbine Disk Assembly
GE Engines CJ610 CF700
Part # 2116M75P01=CK
8130-3 Eligible
8130-3 Eligible
2116M75P01 Stage 1 High Pressure Turbine Disk Assembly is designed to provide essential support for the turbine blades, ensuring optimal performance in high-pressure turbine applications.
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Allocation Control: Allocation control is a process used to ensure fair allocation of assets. It is applied to parts with limited availability and high customer demand. Due to the nature of allocation control items, there is the possibility that stock shown as available may already be allocated based on previously received customer order(s). Specific questions related to allocation control, please contact Boeing Customer Support.
Overview
2116M75P01 Disk Assembly is positioned around the circumference of the disk, serving as a platform for the blades. Precision engineered from high-strength super alloys, it is built to withstand the mechanical stresses generated during turbine operation. The Stage 1 turbine disk for the GE CJ610 turbojet and CF700 turbofan engines is specifically designed to handle more severe conditions than subsequent stages, effectively managing the stresses and conditions prevalent at this stage. It also plays a crucial role in distributing the loads generated during operation, ensuring reliable performance. Its high mechanical strength allows the part to operate efficiently at elevated temperatures, contributing to the overall efficiency of the turbine.
Features & Benefits
Precision engineered from super alloys for enhanced durability
Designed to withstand high mechanical stresses during operation
Effectively distributes loads for reliable turbine performance
Capable of handling severe conditions prevalent in Stage 1
High mechanical strength ensures efficient operation at elevated temperatures
Technical Information
ATA Number
72
ATA Chapter
Engine Turbine / Turbo Prop Ducted Fan / Unducted Fan
ATA Group
Power Plant
ATA Section
HIGH PRESSURE TURBINE SHROUD AND 1ST-STAGE LOW PRESSURE TURBINE NOZZLE
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Product information provided "as is", and Boeing may add, change, discontinue or remove product information at any time. Product photos may not be exact match to product delivered. Seeterms & conditions.
Allocation Control: Allocation control is a process used to ensure fair allocation of assets. It is applied to parts with limited availability and high customer demand. Due to the nature of allocation control items, there is the possibility that stock shown as available may already be allocated based on previously received customer order(s). Specific questions related to allocation control, please contact Boeing Customer Support.