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.
摘要:
The invention concerns a wear-resistant edge layer structure for titanium and its alloys which can be subjected to high loads and has a low coefficient of friction and can be used to particular advantage for protecting human implants. In the edge layer structure according to the invention the edge layer comprises a 200 to 400 nm-thick hard-amorphous carbon layer (4), a 50 to 200 nm-thick intermediate layer (3) and a 0.3 to 2.0 mm-thick gas-alloyed layer (2) whose hardness is between 600 and 1400 Vickers hardness0.1. In order to produce the edge layer structure according to the invention, the surface of the component to be protected is first melted, then gas-alloyed in an N2/Ar atmosphere and cleaned. Only then are the intermediate layer and then the hard-amorphous carbon layer deposited by means of the laser-controlled pulsed vacuum arc process (laser arc process).
摘要:
The invention relates to a wear-resistant, highly stressed and low-friction boundary coating construction for titanium or the alloys thereof which can be advantageously used in order to protect human implants. According to the inventive boundary coating construction, the boundary coating is comprised of a 200 to 400 nm thick DLC coating (4), a 5 to 50 nm thick intermediate coating (3) and a 0.3 to 2.0 mm thick gas alloyed coating (2), said gas alloyed coating having a hardness between 600 HV0,1 and 1,400 HV0,1. The inventive boundary coating construction is produced by firstly melting the surface of the member which is to be protected. The surface is then gas alloyed and cleaned in an N2/Ar atmosphere. Subsequently, the intermediate coating is first deposited followed by a depositing of the hard amorphous carbon coating by means of the laser-induced, pulsed vacuum arc (laser-arc) method.
摘要:
The invention concerns a wear-resistant camshaft and a method of producing the same. Objects to which the invention is advantageously applicable include all cast-iron parts which are subject to wear as a result of lubricated friction. The wear-resistant camshaft consists of cast-iron and comprises a surface layer consisting of a ledeburitic recast layer with a high cementite portion and, lying therebelow, a martensitic hardening zone. According to the invention, the recast layer consists of finely dispersed ledeburitic cementite with thicknesses of ≤ 0.1 νm and a metallic matrix comprising a phase mixture of martensite and/or bainite, residual austenite and less than 20 % finely laminated perlite with a distance of ≤ 0.1 νm between the laminations. The hardening layer is formed from a phase mixture of martensite and/or bainite, partially dissolved perlite and residual austenite. This wear-resistant camshaft according to the invention is produced by means of a high-energy surface recasting method.
摘要:
The invention relates to a method and a device for the crack-free welding, repair welding, or surface welding of metallic parts made of materials that are prone to forming hot cracks. Objects on which said method and device can be efficiently and advantageously used include all parts made of alloys that freeze in several phases and have a large freezing interval or alloys that contain alloying elements or impurity elements which form a low-melting eutectic mixture with one or more main alloying elements and are to be joined by means of a fusion welding process at high power density. In the method according to the invention, a temperature is locally applied in a following manner by two parallel or nearly parallel temperature fields which extend along the welding direction, are electromagnetically generated by means of a volume energy source inside the parts, both begin in front of the welding zone in the welding direction, and of which the maximum temperatures are reached outside the heat affected zone and behind the freezing zone in the welding direction. The depth of the temperature fields at the maximum temperature point is at least as low as the depth of the weld. The additional energy source in the device according to the invention is a volume energy source, is connected to the welding head, and follows the movement of the welding head.
摘要:
The invention concerns a method for beam welding of hardenable steels using a short-time heat treatment. The invention is specially useful in the automobile and engineering industries. At first a short-time heat treatment as single defined preheating is carried out. The beam welding starts at the latest after a defined cooling time.