G.E.® Stage 1 High Pressure Turbine Disk Assembly 2116M75P01

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.