G.E.® Impeller Spacer 1539M12P02

The specific axial clearance between the impeller and other adjacent stationary components is maintained by spacers.  The ring-shaped piece prevents contact or rubbing between the impeller and stationary parts, preventing damage that happens due to friction and wear. The spacer allows for thermal expansion while also allowing adequate space for the gas flow.
Part number 1539M12P02 impeller spacer for GE engine – CJ610 turbojet engine – CF700 Turbofan engine are precisely machined from high-strength alloys to withstand high temperatures and mechanical stresses, actively contributing to the performance and longevity of the turbine while ensuring maximum reliability and durability. The spacer meets the precise design specifications for optimal performance.