公开(公告)号：US06444947B1

公开(公告)日：2002-09-03

申请号：US09463737

申请日：2000-02-16

申请人： Steffen Bonss ,  Jens Standfuss ,  Eckhard Beyer

发明人： Steffen Bonss ,  Jens Standfuss ,  Eckhard Beyer

IPC分类号： B23K2600

CPC分类号： B23K26/0613 ,  B23K26/0604 ,  B23K26/24

摘要： The invention relates to a method and a device for laser-beam welding, because the invention is especially suitable for deep welding a wide variety of materials. The object of the invention is to weld a wide variety of materials by means of laser radiation, especially by deep welding, with a reduced amount of work and at the same time good quality of the welded joint produced. The procedure adopted for this according to the invention is that the intensity of the laser radiation is set by beam-shaping in and on the surface of workpieces in such a way that a small area in the workpiece is irradiated with a great intensity, to form a steam capillary there, and a further, larger adjacent area on the workpiece surface is irradiated with a lesser intensity, and as a result a bell-shaped opening of the steam capillary is formed on the workpiece surface and the cooling rate of the melted material is reduced.

摘要翻译： 本发明涉及一种用于激光束焊接的方法和装置，因为本发明特别适用于深层焊接各种材料。 本发明的目的是通过激光辐射，特别是通过深度焊接，以减少的工作量同时焊接接头的良好质量来焊接多种材料。 根据本发明的方法是通过在工件表面上和表面上的波束整形来设定激光辐射的强度，使得工件中的小面积以大的强度被照射，以形成 蒸汽毛细管，工件表面上的另外较大的相邻区域以较小的强度照射，结果在工件表面上形成蒸汽毛细管的钟形开口，熔融材料的冷却速度 降低了。

公开(公告)号：US09187794B2

公开(公告)日：2015-11-17

申请号：US12312115

申请日：2007-10-10

申请人： Berndt Brenner ,  Steffen Bonss ,  Frank Tietz ,  Marko Seifert ,  Jan Hannweber ,  Stefan Kuehn ,  Udo Karsunke

发明人： Berndt Brenner ,  Steffen Bonss ,  Frank Tietz ,  Marko Seifert ,  Jan Hannweber ,  Stefan Kuehn ,  Udo Karsunke

IPC分类号： C21D1/42 ,  C21D1/09 ,  C21D10/00 ,  C21D11/00 ,  C21D1/34 ,  C21D9/00

CPC分类号： C21D1/09 ,  C21D10/00 ,  C21D10/005 ,  C21D11/00

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.

摘要翻译： 本发明涉及机器，设备和设备的部件表面层的硬化以及工具。 应用可能和有利的对象是遭受严重疲劳或磨损应力的部件，并且由可硬化钢组成并且具有复杂的形状并且其表面必须在功能表面上选择性地硬化，或者其功能表面具有多维度 形状。 用于硬化具有复杂形状的部件的表面层的工艺通过多个能量输入区域进行。 根据本发明，其特征在于，能量输入区域在空间和时间上分别在不同的弯曲部件上进行，并且通过协同工作的输送系统，使得各个温度场的叠加形成均匀的温度场，其完全覆盖 组分的功能表面，并且其中组分的后期硬化区的每个表面元素至少达到所选奥氏体形成温度间隔＆Dgr; Ta，并且各个温度场的最高温度Tmaxn之间的时间间隔＆Dgr; t 从3.1到3.n小于在冷却阶段要求低于马氏体起始温度MS的时间＆Dgr; tmS。 根据本发明，可以实现本发明的方法的装置是，其特征在于，能量构成单元连接到一个或多个用于光学或电磁辐射的能量源，并且各自固定为分离但协作地 操作运输系统。

公开(公告)号：US06231956B1

公开(公告)日：2001-05-15

申请号：US09147810

申请日：1999-06-14

申请人： Berndt Brenner ,  Steffen Bonss ,  Hans-Joachim Scheibe ,  Holger Ziegele

发明人： Berndt Brenner ,  Steffen Bonss ,  Hans-Joachim Scheibe ,  Holger Ziegele

IPC分类号： B32B900

CPC分类号： C23C28/321 ,  A61F2310/00023 ,  A61F2310/00161 ,  A61L27/06 ,  A61L27/08 ,  B23K26/32 ,  B23K26/34 ,  B23K2103/14 ,  C22F1/183 ,  C22F3/00 ,  C23C28/322 ,  C23C28/324 ,  C23C28/343 ,  C23C28/347 ,  Y10T428/24942 ,  Y10T428/24975 ,  Y10T428/265 ,  Y10T428/30 ,  Y10T428/31678

摘要： Wear-resistant edge layer for titanium and its alloys which can be subjected to high loads and has a low coefficient of friction. The wear-resistant edge layer includes a hard amorphous carbon layer, an intermediate layer, and a laser gas alloyed layer. The wear-resistant edge layer may include a 200 to 400 nm thick hard amorphous carbon layer, a 50 to 200 nm thick intermediate layer, and a 0.3 to 2.0 mm thick laser gas alloyed layer. The laser gas alloyed layer may include precipitated titanium nitride needles and have a hardness between 600 HV0.1 and 1400 HV0.1. Process for producing a wear resistant edge layer on a substrate. The process includes forming a laser gas alloyed layer by melting a surface of a substrate, applying an intermediate layer by Laser-Arc, and depositing a hard amorphous carbon layer on the intermediate layer by Laser-Arc.

摘要翻译： 用于钛及其合金的耐磨边缘层可承受高负载且摩擦系数低。 耐磨边缘层包括硬的无定形碳层，中间层和激光气体合金层。 耐磨边缘层可以包括200-400nm厚的硬非晶碳层，50-200nm厚的中间层和0.3-2.0mm厚的激光气体合金层。 激光气体合金层可以包括沉淀的氮化钛针，并且具有在600HV0.1和1400HV0.1之间的硬度。 在基板上制造耐磨边缘层的工艺。 该方法包括通过熔化基板的表面，通过激光弧施加中间层并通过激光弧在中间层上沉积硬的非晶碳层来形成激光气体合金层。

公开(公告)号：US20100126642A1

公开(公告)日：2010-05-27

申请号：US12312115

申请日：2007-10-10

申请人： Berndt Brenner ,  Steffen Bonss ,  Frank Tietz ,  Marko Seifert ,  Jan Hannweber ,  Stefan Kuehn ,  Udo Karsunke

发明人： Berndt Brenner ,  Steffen Bonss ,  Frank Tietz ,  Marko Seifert ,  Jan Hannweber ,  Stefan Kuehn ,  Udo Karsunke

IPC分类号： C21D1/42 ,  C21D1/34 ,  C21D9/00 ,  B23K26/00 ,  C21D11/00 ,  H05B6/04

CPC分类号： C21D1/09 ,  C21D10/00 ,  C21D10/005 ,  C21D11/00

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.

摘要翻译： 本发明涉及机器，设备和设备的部件表面层的硬化以及工具。 应用可能和有利的对象是遭受严重疲劳或磨损应力的部件，并且由可硬化钢组成并且具有复杂的形状并且其表面必须在功能表面上选择性地硬化，或者其功能表面具有多维度 形状。 用于硬化具有复杂形状的部件的表面层的工艺通过多个能量输入区域进行。 根据本发明，其特征在于，能量输入区域在空间和时间上分别在不同的弯曲部件上进行，并且通过协同工作的输送系统，使得各个温度场的叠加形成均匀的温度场，其完全覆盖 组分的功能表面，并且其中组分的后期硬化区的每个表面元素至少达到所选奥氏体形成温度间隔＆Dgr; Ta，并且各个温度场的最高温度Tmaxn之间的时间间隔＆Dgr; t 从3.1到3.n小于在冷却阶段要求低于马氏体起始温度MS的时间＆Dgr; tmS。 根据本发明，可以实现本发明的方法的装置是，其特征在于，能量构成单元连接到一个或多个用于光学或电磁辐射的能量源，并且各自固定为分离但协作地 操作运输系统。

公开(公告)号：US20080011391A1

公开(公告)日：2008-01-17

申请号：US11571818

申请日：2005-07-08

申请人： Berndt Brenner ,  Steffen Bonss ,  Frank Tietz ,  Joerg Kaspar ,  David Walter

发明人： Berndt Brenner ,  Steffen Bonss ,  Frank Tietz ,  Joerg Kaspar ,  David Walter

IPC分类号： C21D1/09

CPC分类号： C23C8/06 ,  B23K26/32 ,  B23K26/34 ,  B23K31/025 ,  B23K35/325 ,  B23K2101/001 ,  B23K2103/14 ,  C23C8/24 ,  C23C24/08 ,  Y02T50/67 ,  Y02T50/6765

摘要： The invention relates to edge layer finishing of functional components, and thereby in particular to a method for producing wear-resistant and fatigue-resistant edge layers in titanium alloys, and components produced therewith. The method according to the invention for producing wear-resistant and fatigue-resistant edge layers in titanium alloys by means of laser gas alloying is essentially characterized in that the laser gas alloying is carried out with a reaction gas that contains or releases interstitially soluble elements in the titanium alloy used, whereby the partial pressure of the reaction gas is selected such that the partial pressure remains below the threshold value above which nitride, carbide, or boride titanium phases are produced. The features according to the invention of the wear-resistant and fatigue-resistant component made of a titanium alloy with a gas-alloyed edge layer essentially are that the wear-resistant edge layer is composed of a fine-grain mixture of α- and β-titanium grains with an interstitially dissolved reaction gas, has a surface hardness Hs, measured on the ground surface, of 360 HV0.5≦Hs≦500 HV0.5, or an edge layer microhardness HR, measured on a polished cross section at 0.1 mm below the surface, of 360 HV0.1≦HR≦560 HV0.1, extends over a depth tR of 0.1 mm≦tR

摘要翻译： 本发明涉及功能部件的边缘层整理，特别涉及一种在钛合金中生产耐磨和耐疲劳边缘层的方法，以及由其制造的部件。 根据本发明的用于通过激光气体合金化在钛合金中生产耐磨和耐疲劳边缘层的方法的基本特征在于，激光气体合金化是用含有或释放空间溶解元素的反应气体进行的 使用钛合金，由此选择反应气体的分压使得分压保持低于阈值以上，在该阈值以上产生氮化物，碳化物或硼化物钛相。 根据本发明的由具有气体合金边缘层的钛合金制成的耐磨和耐疲劳部件的特征基本上是耐磨边缘层由α和β的细晶粒混合物组成 具有间质溶解的反应气体的钛颗粒在地表上测量的表面硬度H S为360HV0.5≤H≤500HV0 或在表面下方0.1mm的抛光横截面上测量的边缘层显微硬度H为360 HV0.1 <= H

公开(公告)号：US06410125B1

公开(公告)日：2002-06-25

申请号：US09530963

申请日：2000-07-24

申请人： Berndt Brenner ,  Steffen Bonss ,  Hans-Joachim Scheibe ,  Holger Ziegele

发明人： Berndt Brenner ,  Steffen Bonss ,  Hans-Joachim Scheibe ,  Holger Ziegele

IPC分类号： B32B500

CPC分类号： C23C8/24 ,  C23C14/02 ,  C23C14/022 ,  C23C14/028 ,  C23C14/0605 ,  C23C14/325 ,  C23C26/02 ,  C23C28/322 ,  C23C28/324 ,  C23C28/343 ,  Y10T428/24942 ,  Y10T428/24975 ,  Y10T428/265 ,  Y10T428/30 ,  Y10T428/31678

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.

摘要翻译： 本发明涉及用于钛或其合金的耐磨，高应力和低摩擦边界涂层结构，其可有利地用于保护人类植入物。 根据本发明的边界涂层结构，边界涂层由200至400nm厚的DLC涂层（4），5至50nm厚的中间涂层（3）和0.3至2.0mm厚的气体合金涂层（2）组成， 所述气体合金涂层的硬度为600HV0.1至1400HV0.1。 本发明的边界涂层结构通过首先熔化待保护的构件的表面来制造。 然后将表面气体合金化并在N 2 / Ar气氛中进行清洁。 随后，首先沉积中间涂层，然后通过激光诱导的脉冲真空电弧（激光弧）法沉积硬质无定形碳涂层。