G.E. 2116M75P01 Stage 1 High Pressure Turbine Disk Assembly
GE Engines CJ610 CF700
Part # 2116M75P01=CK
8130-3 Eligible
8130-3 Eligible
This precision-engineered turbine disk assembly is designed for the GE CJ610 turbojet and CF700 turbofan engines. Made from super alloys, it supports the blades and withstands high mechanical stresses and temperatures, ensuring reliable operation in demanding conditions. The part number for this assembly is 2116M75P01.This precision-engineered turbine disk assembly is designed
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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
Stage 1 turbine disk assembly are positioned around the circumference of the disk, which serves as a platform to provide the support required for the blades. The disk assembly is precision engineered from super alloys to withstand the mechanical stresses generated during the operation of the turbine. The stage 1 turbine disk for the GE CJ610 turbojet and CF700 turbofan engines is capable of handling more severe conditions than the subsequent stages since it is engineered specifically to handle the stresses and conditions prevalent at this stage. Part number 2116M75P01 disk assembly also helps distribute the loads that are generated in the process, thus ensuring reliable operation. The high mechanical strength of the material 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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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.