Oerlikon Surface Solutions Ag, Pfaffikon

Oerlikon Trading Ag, Trubbach

Oerlikon Trading Ag, Truebbach

Siemens Aktiengesellschaft

Siemens Energy Global Gmbh & Co. Kg

Unaxis-balzers Aktiengesellschaft

Oerlikon Surface Solutions Ag, Trubbach

Plansee Composite Materials Gmbh

Jürgen Ramm

Beno Widrig

Werner Stamm

Denis Kurapov

Christian Wohlrab

Florian Seibert

Peter Polcik

Daniel Lendi

Matthias Lukas Sobiech

Mirjam Arndt

Paul Heinz Mayrhofer

Helmut Rudigier

Volker Derflinger

Orlaw Massler

Hamid Bolvardi

Malko Gindrat

Oliver Hunold

Dennis T Quinto

Michael Ante

Arturo Flores Renteria

Peter Ernst

Jochen Barnikel

Oliver Gstoehl

Andreas Reiter

Wolfgang Kalss

Richard Rachbauer

Johann Karner

Torsten Neddemeyer

Eugen Beck

Christian Martin Koller

Stephan Kasemann

Doris Fopp-Spori

Andrei Ghicov

Ali Khatibi

Kurt Ruhm

Michael Annen

Gerhard Tuymer

Robert Raab

Bernhard Kohlhauser

Joerg Paulitsch

Beno Wídrìg

Helmut Rudígìer

Marcelo Dornelles Pimenta

Sascha Hessel

Barbara Hanselmann

Heinrich Zimmermann

Florian Neff

Edgar Balter

Thomas Glechner

Helmut Riedl-tragenreif

Hans-Georg Oemer

Troy Vom Braucke

Kerstin Glantz

Matthias Lukas Soebiech

Reinhard Dr Rose

Monika Dr Lehnert

Kerstin GLÄNTZ

Benno Widrig

Benno Widrg

A coated article includes a coated surface which consists of a substrate and a coating system. The coating system has at least one protective layer consisting of one or more transition metal borides and one dopant element, wherein: 13 the protective layer having chemical element composition defined by the formula TMBSi, where TM is one or more of the transition metal elements Chromium and Hafnium; Si is Silicon present in the protective layer as the dopant element; B is Boron; x is the concentration in atomic percent of TM; y is the concentration in atomic percent of B; and q is the concentration in atomic percent of Si, where x+y+q=1, 0.15≤x≤0.33, 0.40≤y≤0.67, and 0.1≤q≤0.40, and—the atomic concentration ratio of boron to the transition metals in the protective layer is higher or equal to 2, i.e. y/x≥2, and—the protective layer exhibits an AlBcrystal structure.

Coated article with enhanced oxidation resistance properties

A method for coating a substrate surrounding a gas turbine blade, including the following steps: in a first step, a MCrAlY matrix is applied by means of a PVD method; in a further step, an oxide layer is applied by means of a PVD method.

Coating for thermally and abrasively loaded turbine blades

An improved coating used in plastic processing applications including a first layer system that includes at least one corrosion resistant material layer; a second layer system that includes at least one abrasion resistant material layers; and a transition layer provided between the first layer and the second layer. The coating is resistant to both abrasion and corrosion, while maintaining ductility and impact resistance.

Coating for enhanced performance and lifetime in plastic processing applications

Coated tool comprising a coated surface, the coated surface comprising a substrate having a surface on which a coating is deposited, wherein the substrate is made of a material comprising cobalt, and wherein the coating comprises at least one boron-comprising layer, wherein the at least one boron-comprising layer comprises Al and the boron comprised in this layer is present as boride, thereby the boron-comprising layer is able to form further layers for providing a diffusion barrier layer effect, in particular for stopping diffusion of cobalt from the substrate surface to the coating, when the coated tool or the coated surface is exposed to temperatures in a range between approximately 600 and 1200° C.

Coated tool with coating comprising boride-containing diffusion barrier layer

A superalloy target wherein the superalloy target has a polycrystalline structure of random grain orientation, the average grain size in the structure is smaller than 20 μm, and the porosity in the structure is smaller than 10%. Furthermore, the invention includes a method of producing a superalloy target by powder metallurgical production, wherein the powder-metallurgical production starts from alloyed powder(s) of a superalloy and includes the step of spark plasma sintering (SPS) of the alloyed powder(s).

Superalloy target

A superalloy workpiece includes a superalloy substrate and an interface layer (IF-1) of essentially the same superalloy composition directly on a surface of the superalloy substrate. A transition layer (TL) of essentially the same superalloy and superalloy oxides or a different metal composition and different metal oxides is on the interface layer (IF-1). The oxygen content of the transition layer increases from the interface layer (IF-1) towards a barrier layer (IF-2) of super alloy oxides or of different metal oxides.

PVD bond coat

A layered stack that can be used as an oxidation and chemical barrier with superalloy substrates, including Ni, Ni&#x2014;Co, Co, and Ni-aluminide based substrates, and methods of preparing the layered stack. The layer system can be applied to a substrate in a single physical vapor deposition process with no interruption of vacuum conditions.

PVD barrier coating for superalloy substrates

The present invention relates to coated sliding parts having coating systems which allow better sliding performance under dry and/or under lubricated conditions. The coating systems according to the present invention being characterized by having an outermost layer which&#x2014;is a smooth oxide-containing layer in case of sliding applications under lubricated conditions, or&#x2014;is a self-lubricated layer comprising molybdenum nitride, in case of sliding applications under dry or lubricated conditions, is a self lubricated layer with a structured surface comprising a multitude of essentially circular recesses with diameters of several micrometers or below, the recesses randomly distributed over the surface.

Coating with enhanced sliding properties

Provided is a method for arranging a protective coating for a thermally stressed structure, having at least one layer of alpha-aluminium oxide or of element-modified alpha-aluminium oxide, and wherein the protective coating is applied by reactive cathodic arc vaporization. A protective coating produced by the method and a component having a protective coating is also provided.

Protective coating for a thermally stressed structure

The present invention relates to a method for producing a multilayer film comprising aluminum, chromium, oxygen and nitrogen, in a vacuum coating chamber, the multilayer film comprising layers of type A and layers of type B deposited alternate one of each other, wherein during deposition of the multilayer film at least one target comprising aluminum and chromium is operated as cathode by means of a PVD technique and used in this manner as material source for supplying aluminum and chromium, and an oxygen gas flow and a nitrogen gas flow are introduced as reactive gases in the vacuum chamber for reacting with aluminum and chromium, thereby supplying oxygen and nitrogen for forming the multilayer film, characterized in that: &#x2014;The A layers are deposited as oxynitride layers of Al&#x2014;Cr&#x2014;O&#x2014;N by using nitrogen and oxygen as reactive gas at the same time, &#x2014;The B layers are deposited as nitride layers of Al&#x2014;Cr&#x2014;N by reducing the oxygen gas flow and by increasing the nitrogen gas flow in order to use only nitrogen as reactive gas for the formation of the Al&#x2014;Cr&#x2014;N layer, and wherein the relation between oxygen content and nitrogen content in the multilayer film correspond to a ratio in atomic percentage having a value between and including 1.8 and 4.

Al&#x2014;Cr-based ceramic coatings with increased thermal stability

A sealable volume has a wall forming at least a portion of a boundary limiting the volume. The wall includes a hydrogen permeation barrier including a layer system (LS) having at least one layer. The layer system includes at least one hydrogen barrier layer (HPBL) of an at least ternary oxide. Preferably, the oxide is substantially composed of Al, Cr and O and the hydrogen barrier layer (HPBL) is deposited using physical vapor deposition, in particular cathodic arc evaporation. Preferably, the layer system includes at least one of: an adhesion layer (AdhL), a hydrogen storage layer (HStL), a protective layer (ProtL), in particular a thermal barrier layer (ThBL), a diffusion barrier layer (DBL), an oxidation barrier layer (OxBL), a chemical barrier layer (ChBL), a wear resistance layer (WRL). Excellent hydrogen permeation barrier properties can be achieved, and the layer system can be tailored as required by an envisaged application.

Permeation barrier layer

In these investigations, an attempt has been made to correlate the deposition parameters of the reactive cathodic arc evaporation with processes at the surface of the composite Al&#x2014;Cr targets and the nucleation and phase formation of the synthesized Al&#x2014;Cr&#x2014;O layers. The oxygen partial pressure and the pulsed operation of the arc current influence the formation of intermetallic phases and solid solutions at the target surface. The nucleation of the ternary oxides at the substrate site appears to be, to some extent, controllable by the intermetallics or solid solutions formed at the target surface. A specific nucleation process at substrate site can therefore be induced by the free choice of target composition in combination with the partial pressure of the oxygen reactive gas. It also allows the control over the oxide island growth at the target surface which occurs occasionally at higher oxygen partial pressure. This hypothesis is supported by the X-ray diffraction analysis of the layers as well as of the target surface.

Synthesis of metal oxides by reactive cathodic arc evaporation

Provided is a coating system for a substrate, the system including a first, second and third layer. In the system, the first layer is designed as an adhesion promoter layer, the second layer is a ductile metal layer with a columnar structure and the uppermost, third layer is a ceramic oxide layer with a high hardness value. The substrate is ideally an element of a compressor component of a stationary gas turbine. Also disclosed is a method for producing the coating system.

Contour-following protective layer for compressor components of gas turbines

The present invention relates to a tribological system () comprising a first body () and a second body (), which each form a component of an internal combustion engine (), in particular a piston (), a piston ring () or a cylinder (), and the surfaces () of which have a first and a second material area () which come into contact with each other at least in some regions during operation and form a tribological contact, wherein the first and/or the second material area () is formed as a layer on the basis of chromium oxide or aluminum chromium oxide. The invention also relates to an internal combustion engine () having such a system ().

Tribological system of an internal combustion engine with a coating

A method for producing an oxidation barrier layer on a workpiece substrate in which the oxidation barrier layer is produced by means of physical deposition from the gas phase (PVD) and is an oxide that is materially related to the uncoated surface of the workpiece.

Oxidation barrier layer

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Maienfeld, Switzerland

Jürgen Ramm