Accession Number : AD0261753
Title : RADIAL EXTRUSION OF TURBOJET DISCS
Corporate Author : CURTISS-WRIGHT CORP WOOD-RIDGE N J WRIGHT AERONAUTICAL DIV
Personal Author(s) : KROHN,ROBERT W.
Report Date : 30 JUN 1961
Pagination or Media Count : 1
Abstract : Procedures for the machining of full-scale steel and Ti alloy disks for turbojet engines are detailed. Six steel disks were produced to specification, and mechanical property data are presented. Difficulties were encountered in the production of Ti alloy disks. Distortion and excessive shrinkage of the disk occurred when cooled from the forging temperature. Distortion was partially corrected by the use of fixtures during annealing but was encountered again during rough machining. Excessive grinding burns and burrs were corrected by the use of coolants. Broaching of the fir tree slots was accomplished at speeds of 30 to 35 fpm by the use of a 2:1 mineral seal oil-fatty chlorinated hydrocarbons and sulphurized polymerized terpenes solution as a coolant.
Descriptors : *GAS TURBINE ROTORS, *TURBOJET ENGINES, CADMIUM, COOLANTS, CUTTING FLUIDS, DEFORMATION, DIES, EXTRUSION, FORGING, GRINDERS, HARDNESS, HEAT TREATMENT, HYDRAULIC PRESSES, MACHINING, MANUFACTURING, MECHANICAL PROPERTIES, PLATING, PRECISION FINISHING, PROCESSING, PRODUCTION, SMALL TOOLS, STEEL, TITANIUM ALLOYS, TORPEDO COMPONENTS
Distribution Statement : APPROVED FOR PUBLIC RELEASE