Siemens Aktiengesellschaft

Lanxess Deutschland Gmbh

Siemens Energy Global Gmbh & Co. Kg

Thyssenkrupp Steel Europe Ag

Thyssenkrupp Electrical Steel Gmbh

Andreas Böttcher

Tobias Krieger

Patrick Lapp

Andre Kluge

Jens Kleinfeld

Ulrich Wörz

Timothy A Fox

Stephen A Ramier

Bernd Koop

Claus Krusch

Peter Spetmann

Daniel Vogtmann

Peter Schröder

Vyacheslav Veitsman

Martin Kugler

Thomas Beck

Hermann Uhr

Thomas Jaetsch

William Richard Ryan

Bernd Prade

Thomas Grieb

Olga Deiss

Christian Beck

Thomas-Dieter Tenrahm

Elmar Pfeiffer

Johannes Kaulen

Marc Tertilt

Erasmus Vogl

Eckart Schumann

Mirko Milazar

Tobias Buchal

Oliver Schneider

Werner Krebs

Richard L Thackway

Berthold Köstlin

Francois Benkler

Dieter Minninger

Matthias Hase

David M Ritland

Winfried Esser

Daniel W Garan

Christian Scholz

Giuseppe Gaio

Jaap Van Kampen

Daniel Grundei

Uwe Kahlstorf

Rudolf Küperkoch

Gerd-Friedrich Renner

Birgit Grüger

Marco Link

Eberhard Sowka

Torsten Jokisch

Sabine Tüschen

Hartwig Dümler

Jürgen Meisl

Thomas Hauser

Werner Hesse

Peter Kaufmann

Rostislav Teteruk

Sascha Staring

Simon Purschke

Patrick Ronald Flohr

Christian Amann

Gerhard Simon

Holger Streb

Martin Hartmann

Stefan Reich

Shilun Sheng

Christopher Grandt

Günther Walz

Udo Schmitz

Torsten Matthias

Ludger Lahn

Steffen Donath

Joachim-Rene Nuding

Björn Beckmann

Uwe Lohse

Kai-Uwe Schildmacher

Boris Ferdinand Kock

Falk Seidel

Mark F Rubio

Gerd Weber

Michael Neubauer

Sabine Grendel

Wilhelm Scheidtmann

Matthias Chlebowski

Fabian Sander

Marcus Zurhorst

Jürgen Buchheim

Lars Otte

Christin Schlensog

Mariano Cano Wolff

Philipp Stapper

Thomas Kunadt

Julia Mühl

Christoph Buse

Patricia Hülsmeier

Ekkehard Maldfeld

Manfred Hartmann

Achim Schirrmacher

A heat shield assembly of a combustion chamber has a supporting structure and heat shield elements arranged on the supporting structure. For fastening, the supporting structure has spring devices fastened therein, into each of which a fastening bolt can be screwed. In order to realize the pre-installation and the later removal of the spring elements contained in the spring device, at a holding sleeve, a contact plate is removably fastened in the holding sleeve on the side facing the heat shield element and a stationary securing plate is arranged on the opposite side.

Heat shield assembly of a combustion chamber having a disk spring set

A fuel nozzle body having a rearward end and a front end with an outer tube which extends from the rearward end to the front end and has radial openings for a first fuel in the region of the front end, and an inner tube which is arranged concentrically to the outer tube and which opens in the region of the front end into a nozzle head, which has additional openings for a second fuel, wherein, in the region of the front end, the inner tube is guided in the outer tube by two fits which are arranged axially between the radial openings and the additional openings, and wherein the first fit closest to the radial openings is configured as a circumferential web around the inner tube, and wherein the second fit is configured with at least one interruption on the perimeter.

Fuel nozzle body

A burner assembly with a combustion chamber, a plurality of mixing ducts leading into the combustion chamber, where combustion air and introduced fuel are mixed. The mixing ducts are formed by mixing tubes extending axially through an annular space between a tubular outer wall, a tubular inner wall arranged radially at a distance from the outer wall, a ring-shaped end plate arranged upstream and a ring-shaped end plate arranged downstream. The end plates have through-openings, which accommodate and/or extend the mixing tubes, and the end plates have, both radially inside and outside, a circumferential edge extending in the direction of the annular space, with axial bores in the edge of the ring-shaped end plate arranged downstream. The axial bores extend from the annual space into the end plate, and at least one opening is for removing cooling air, the opening branching from the axial bore.

Bruner assembly

A pipe connection for conducting a fluid that is under pressure is provided, having two tubular connection parts for a conical clamping connection, which are screwed together by a union nut while one is inserted in the other, wherein each connection part has a conical sealing surface that contacts the other in a sealing manner and wherein an annular groove is provided in one of the sealing surfaces. In order to enable the pipe connection also to conduct a fluid having cycling or varying temperature, the inner of the two connection parts has thermal insulation on the inside of the pipe at least in the axial segment of the sealing surface of the connection part, wherein the thermal insulation tube has a cam or a collar on the outer surface, which engages in a recess, which is axially bounded by the two connection parts.

Pipe connection for conducting a fluid that is under pressure

A heat shield with support structure and a number of heat shield blocks secured thereto, having a cold side facing the support structure and a hot side opposite the cold side. At least one recess is arranged in at least one heat shield block circumferential face, connecting the cold to hot side. An opening connecting the recess to the cold side runs in the circumferential face perpendicularly to the cold side. A securing bolt inserted into the opening secures the heat shield block to the support structure. A bolt head protrudes at least partly into the recess. The securing bolt passes through an angled plate having first limb extending substantially parallel to the circumferential face and second limb extending into the recess. The angled plate has a reinforcing device extending beyond the pure angular shape to increase a resistance of the angled plate against bending due to the securing bolt.

Securing a heat shield block to a support structure, and heat shield

A pipe connection arrangement in a high-pressure fluid line system of a dual fuel engine, having first pipe element with outer sealing cone and conical shoulder adjoining the cone, having further pipe element with inner sealing cone and external thread, having a screw nut element with clamping sleeve region having inner clamping cone and threaded sleeve region having internal thread. The outer sealing cone of the first pipe element is arranged in the inner sealing cone of the further pipe element and the internal thread of the screw nut element is screwed on the external thread of the further pipe element. The inner clamping cone of the screw nut element is pulled against the conical shoulder of the first pipe element such that the outer and inner sealing cones are clamped with one another in a sealing manner, wherein the threaded sleeve region of the screw nut element is conical.

Pipe connection arrangement, high-pressure fluid line system of a dual fuel engine, dual fuel engine and use of a tension nut

A method for monitoring the operation of a gas turbine is provided, in which component vibrations are detected during the operation of the gas turbine by an acceleration sensor arranged on the component, a plurality of signal sections being determined by a plurality of frequency bands fb from the signal forwarded and processed by the acceleration sensor. To avoid an unnecessary shutdown of the gas turbine to perform an inspection which subsequently proves unnecessary, thereby increasing the availability of the gas turbine, a total vibration period is determined by adding together the vibration periods of signal sections during which the amplitudes of the signal sections concerned are greater than a frequency band-specific threshold.

Method for monitoring the operation of a gas turbine

A layer system including a substrate and a layer is provided. The layer system has a hole at least in the layer, and wherein at least one recess is present in a surface of the layer in a vicinity around the hole or directly adjoining a boundary line of the hole.

Modified interface around a hole

A pipe connection that includes two tubular connection pieces for a conical clamping connection, the connection pieces being screwed together by a union nut while one connection piece is plugged inside the other. Each connection piece has a conical sealing surface which sealingly rests against the other, and an annular groove is provided in one of the sealing surfaces. The union nut is slit on the collar side.

Pipe connection for conducting a pressurized fluid

Use of aziridines for stabilizing iodine-containing compounds, especially biocides.

Stabilization of compounds comprising iodine

An assembly for a gas turbine is presented. The assembly includes a gas supply pipe passing through a bore in a flange of the gas turbine for supplying gas to a combustion chamber of the gas turbine and a sleeve surrounding the gas supply pipe, having a first end and a second end, wherein the first end is sealingly coupled to the gas supply pipe, and wherein the sleeve is adapted to be sealingly coupled to the flange at the second end such that the sleeve extends along a thickness of the flange.

Gas turbine assembly and method therefor

The invention relates to nitrogen-containing inorganic carrier materials, more particularly to inorganic carrier materials containing organically bonded nitrogen, to their preparation and also to their use for stabilizing iodine-containing compounds, and also to binder formulations comprising them and to the use thereof for protecting industrial materials.

Nitrogen-containing inorganic carrier materials

A burner assembly is provided. The burner assembly includes a support housing with a supply manifold, the supply manifold includes a fuel passage system, and fuel nozzles extending from the supply manifold and being supplied with fuel through the fuel passage system of the supply manifold. The supply manifold is sandwiched using at least two subparts.

Burner assembly

A burner carrier flange and a burner with such a burner carrier flange are provided. A surface of the burner carrier flange potentially comes into contact with fuel. The burner carrier element includes a base material and a corrosion-resistant material and the surface that potentially comes into contact with fuel is made of the corrosion-resistant material.

Burning element and burner with a corrosion-resistant insert

A burner incorporating a pilot cone and a mounting insert is provided. The pilot cone is constructed as a pilot cone assembly which is decoupled from the mounting insert. Further, an operating method for increasing the service life of a burner which incorporates a pilot cone assembly and a mounting insert is provided. The pilot cone assembly has a cone side and incorporates at least one further side where the further side is arranged to be essentially parallel to one of the sides of the mounting insert and spaced apart from it, so that between the further side and the side of the mounting insert there is a defined gap. In an operation of the burner, the gap is significantly reduced by the thermal expansion in at least at one point of contact between the further side and the side of the mounting insert. Finally, an assembly method is provided.

Burner, operating method and assembly method

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Mettmann, Germany

Andreas Böttcher