Process and apparatus for hardening the surface layer of components having a complicated shape

摘要

The invention relates to the hardening of the surface layer of parts of machines, plants and apparatuses and also tools. Objects for which the application is possible and advantageous are components which are subjected to severe fatigue or wear stresses and are composed of hardenable steels and have a complicated shape and whose surface has to be hardened selectively on the functional surfaces or whose functional surface has a multidimensional shape. The process for hardening the surface layer of components having a complicated shape is carried out by means of a plurality of energy input zones. According to the invention, it is characterized in that the energy input zones are conducted on different curved parts separately in space and time and by means of cooperatively working transport systems so that superposition of the individual temperature fields forms a uniform temperature field which completely covers the functional surface of the component and within which each surface element of the later hardening zone of the component attains the selected austenite formation temperature interval ΔTa at least once and the time interval Δt between the maximum temperatures Tmaxn of the individual temperature fields is from 3.1 to 3.n smaller than the time ΔtmS which is required to go below the martensite start temperature MS during the cooling phase. The apparatus by means of which the process of the invention can be carried out is, according to the invention, characterized in that the energy configuring units are connected to one or more energy sources for optical or electromagnetic radiation and are each fixed to separate but cooperatively operating transport systems.

主权项

1. Method for boundary hardening of components having complicated shapes, wherein the components have two adjacent functional surfaces defining an abutting edge therebetween that extends in a three-dimensional path and/or the angle between the adjacent functional surfaces changes along the abutting edge path, comprising creating plural energy effect zones on different path curves separated in space and time through the use of cooperating movement systems that are moved and guided with respect to the functional surfaces of the components, wherein a uniform temperature field fully enclosing the functional surfaces of the component is formed by overlapping individual temperature fields along the abutting edge of the functional surfaces within which at each surface element of the later hardening zone of the component, a chosen austenitization temperature interval ΔTa is reached at least once and a time interval Δt between reaching the austenitization temperatures of the individual temperature fields is smaller than a time Δtms required to drop from the austenitization temperature to the martensite start temperature MS during its cooling phase.