Patents by Inventor Hans-Peter Bossmann

Hans-Peter Bossmann has filed for patents to protect the following inventions. This listing includes patent applications that are pending as well as patents that have already been granted by the United States Patent and Trademark Office (USPTO).

  • Publication number: 20150083305
    Abstract: The invention refers to a method for applying heat resistant protection components onto the surface of a heat exposed component. The method including providing at least two separate heat protection components, and joining the at least two separate heat protection components onto their top surface and/or bottom surface and/or at least one side surface by flexible means for obtaining an integrally handable entity. The method further includes fixing the integrally handable entity by applying and brazing the surface of each heat protection component on the surface of the heat exposed component. The materials of the flexible means and for joining the flexible means on the separate heat protection components are selected such that the materials withstand brazing being performed under protective atmosphere, i.e. an atmosphere without or with reduced amount of oxygen, at process temperatures between 700° C. and 1200° C., and that the materials are burned out after brazing during a following oxidizing thermal step.
    Type: Application
    Filed: September 17, 2014
    Publication date: March 26, 2015
    Inventors: Hans-Peter Bossmann, Michael Stuer, Daniel Renusch
  • Publication number: 20150084245
    Abstract: The invention refers to a method for producing means with thermal resist for applying at a surface of a heat exposed component. The method includes providing at least one mixture of at least two different inorganic powder materials: with different chemical composition and thermal expansion coefficient, where at least one of the powder materials experiences volume changes due to crystallographic phase change at a given temperature, and/or\where at least one of the two powder materials experiences volume changes due to chemical composition change, forming the at least one mixture into a green body shape, sintering the green body to obtain a ceramic body and cooling the ceramic body and causing micro-cracking during heating and or/sintering and/or cooling to obtain the means with thermal resist. The forming is performed such that a first mixture forming a first layer onto which a second mixture is applied forming a second layer differs in porosity from that first layer to obtain a layered green body.
    Type: Application
    Filed: September 17, 2014
    Publication date: March 26, 2015
    Inventors: Michael STUER, Hans-Peter BOSSMANN
  • Patent number: 8951015
    Abstract: A rotor blade arrangement (20), especially for a gas turbine, which can be fastened on a blade carrier (19) and includes in each case a blade aerofoil element (10) and a platform element (14), wherein the platform elements (14) of a blade row form a continuous inner shroud. With such a blade arrangement, a mechanical decoupling, which extends the service life, is achieved by the blade aerofoil element (10) and the platform element (14) being formed as separate elements and by being able to be fastened in each case separately on the blade carrier (19).
    Type: Grant
    Filed: November 13, 2009
    Date of Patent: February 10, 2015
    Assignee: Alstom Technology Ltd.
    Inventors: Herbert Brandl, Hans-Peter Bossmann, Philipp Indlekofer
  • Patent number: 8911213
    Abstract: A rotor blade (10) for a gas turbine includes a blade airfoil (11), a blade tip (15), a blade root (14), and a platform (12) which is formed between the blade tip (15) and the blade root (14), and is assembled from a plurality of individual sections (16, 17, 18), the material of which is adapted in each case to the intended purpose of the individual section concerned. With such a rotor blade, a simplified production is achieved as a result of each of the individual sections (16, 17, 18) from the dimensions being significantly smaller than the assembled rotor blade (10).
    Type: Grant
    Filed: December 14, 2009
    Date of Patent: December 16, 2014
    Assignee: Alstom Technology Ltd
    Inventors: Herbert Brandl, Sven Schofer, Claus Paul Gerdes, Hans-Peter Bossmann
  • Publication number: 20140328672
    Abstract: A stator component of a turbomachine is composed substantially of at least one axially extending outer ring (10) which serves as a frame of an inner ring composed of partial segments (20). The partial segments are arranged on one another such that, on the rotor side, they form a coherent circular circumferential surface in relation to the rotational movement of rotor blades (30). The individual partial segment (20) is composed of a material of uniform construction or, at least in a radial direction, of multiple partial bodies constructed from different materials, such as for example ceramic, wherein a partial segment thus formed exhibits predetermined stress and/or expansion behaviour as a function of the load ranges of the turbomachine.
    Type: Application
    Filed: July 18, 2014
    Publication date: November 6, 2014
    Inventors: Herbert BRANDL, Hans-Peter BOSSMANN
  • Publication number: 20140308539
    Abstract: A configuration for joining a ceramic layer has a thermal insulating material to a metallic layer. The configuration includes an interface layer made of metallic material located between the ceramic layer and the metallic layer, which includes a plurality of interlocking elements on one of its sides, facing the ceramic layer, the ceramic layer comprising a plurality of cavities aimed at connecting with the corresponding interlocking elements of the interface layer. The configuration also includes a brazing layer by means of which the interface layer is joint to the metallic layer. The invention also refers to a method for obtaining such a configuration.
    Type: Application
    Filed: April 11, 2014
    Publication date: October 16, 2014
    Inventors: Gregoire Etienne WITZ, Matthias HOEBEL, Hans-Peter BOSSMANN
  • Publication number: 20140308116
    Abstract: Shroud device thermally protecting a gas turbine blade, having a ceramic layer and a metallic layer, the metallic layer being thermally protected by the ceramic layer, the ceramic layer being mechanically joined to the metallic layer by a fixation device having a plurality of protrusions located in the metallic layer designed so as to engage with a plurality of cavities located in the ceramic layer, such that there exists a gap between the cavities and the protrusions at ambient temperature, the gap disappearing at high temperature operation of the gas turbine, the protrusions being then locked into the cavities.
    Type: Application
    Filed: April 10, 2014
    Publication date: October 16, 2014
    Applicant: ALSTOM Technology Ltd
    Inventors: Gregoire Etienne WITZ, Mathieu Esquerre, Michael Stuer, Daniel Renusch, Hans-Peter Bossmann
  • Publication number: 20140242411
    Abstract: A high temperature thermal barrier coating which consists of a stabilized ZrO2 composition for the protection of thermally loaded components (10, 10?) of a thermal machine, especially a gas turbine, is disclosed. The thermal barrier coating is stabilized with at least 15 mol % Y1+v Ta1?vO4?v, the ZrO2 is partially substituted by at least 10 mol % HfO2 and the composition is established according to the formula (Y1+vTa1?vO4?v)z(Zr1?xHfxO2)1?z, with x ranging from 0.1 to 0.5, v ranging from ?0.1 to 0.2 and z ranging from 0.15 to 0.25.
    Type: Application
    Filed: May 8, 2014
    Publication date: August 28, 2014
    Inventors: Gregoire Etienne WITZ, Hans-Peter BOSSMANN, Anup BHATTACHARYA, Valery SHKLOVER
  • Publication number: 20140242408
    Abstract: The invention relates to a method for manufacturing a metal-ceramic composite structure intended to be exposed to high temperatures. The composite structure includes a base metal structure or component, which is on at least one side covered and permanently joined with one or more ceramic tiles.
    Type: Application
    Filed: February 25, 2014
    Publication date: August 28, 2014
    Inventors: Herbert BRANDL, Hans-Peter BOSSMANN
  • Patent number: 8801381
    Abstract: A turbine blade is provided having an airfoil and a platform manufactured in two separate pieces, which are joined together. The blade includes a seal, which is a mechanically decoupled seal, interposed between the airfoil and platform in a position closer to a hot gases path than a joint.
    Type: Grant
    Filed: September 8, 2010
    Date of Patent: August 12, 2014
    Assignee: Alstom Technology Ltd.
    Inventors: Carlos Simon-Delgado, Hans-Peter Bossmann, Herbert Brandl
  • Patent number: 8638432
    Abstract: In a method of spatially detecting the chemical composition of nonmetallic components on a surface which is subsequently to be coated with a metallic and/or ceramic and/or organic layer, a laser optical device is provided. The turbine part is irradiated with monochromatic irradiation at a first wavelength (?in) with the laser optical device. Radiation is detected which is emitted by the surface at a second wavelength (?out) which is longer than the first wavelength (?in).
    Type: Grant
    Filed: March 7, 2012
    Date of Patent: January 28, 2014
    Assignee: Alstom Technology Ltd.
    Inventors: Gregoire Witz, Hans-Peter Bossmann
  • Patent number: 8563142
    Abstract: A dual brazing alloy element for a materially integral connection of a ceramic surface to a metallic surface includes a first layer having a Ni-based brazing alloy with a Ni content of at least 50% by weight and having at least one component configured to lower a melting point of the Ni-based brazing alloy selected from the group consisting of Si, B, Mn, Sn and Ge. A second layer includes an active brazing alloy material having a total content of 1-15% by weight of at least one active element selected from the group consisting of Ti, Hf, Zr and V.
    Type: Grant
    Filed: September 29, 2011
    Date of Patent: October 22, 2013
    Assignee: Alstom Technology Ltd
    Inventors: Hans-Peter Bossmann, Alexander Schnell
  • Patent number: 8252601
    Abstract: A method for designating a component, coated with a heat insulation layer including zirconium dioxide (ZrO2) stabilized with yttrium oxide (Y2O3) [YSZ], and for determining its operating time or operating temperature is provided. The method includes doping the heat insulation layer and marking the doped heat insulation layer, with at least one metal oxide in at least one surface region of the component. The metal oxide is selected such that the doped region of YSZ is visible or can be made optically visible in order to designate the component. The method also includes comparing a slower or faster change in lattice parameters of the doped YSZ region, as compared with undoped YSZ, and determining the operating time of the component under temperature by comparing the lattice parameters with a known calibrating characteristic curve.
    Type: Grant
    Filed: August 25, 2008
    Date of Patent: August 28, 2012
    Assignee: ALSTOM Technology Ltd.
    Inventors: Hans-Peter Bossmann, Dietrich Eckardt
  • Publication number: 20120206717
    Abstract: In a method of spatially detecting the chemical composition of nonmetallic components on a surface which is subsequently to be coated with a metallic and/or ceramic and/or organic layer, a laser optical device is provided. The turbine part is irradiated with monochromatic irradiation at a first wavelength (?in) with the laser optical device. Radiation is detected which is emitted by the surface at a second wavelength (?out) which is longer than the first wavelength (?in).
    Type: Application
    Filed: March 7, 2012
    Publication date: August 16, 2012
    Inventors: Gregoire Witz, Hans-Peter BOSSMANN
  • Patent number: 8216689
    Abstract: Components (1) have a thermal barrier coating (2-6) on the surface thereof, wherein the thermal barrier coating includes at least one layer (3) having chemically stabilized zirconia, and wherein at least indirectly adjacent to the layer (3) with chemically stabilized zirconia and on its surface facing side, there is provided a protective layer (4) and/or a infiltration zone (5) which does not react with environmental contaminant compositions that contain oxides of calcium and which does not react with the material of the layer (3) having chemically stabilized zirconia. Methods for making such components as well as to uses of specific systems for coating thermal barrier coatings, can prevent CMAS.
    Type: Grant
    Filed: May 26, 2009
    Date of Patent: July 10, 2012
    Assignees: ALSTOM Technology Ltd., ETH Eidgenoessische Technische Hochschule Zuerich
    Inventors: Gregoire Etienne Witz, Hans-Peter Bossmann, Valery Shklover, Sharath Bachegowda
  • Publication number: 20120063911
    Abstract: A dual brazing alloy element for a materially integral connection of a ceramic surface to a metallic surface includes a first layer having a Ni-based brazing alloy with a Ni content of at least 50% by weight and having at least one component configured to lower a melting point of the Ni-based brazing alloy selected from the group consisting of Si, B, Mn, Sn and Ge. A second layer includes an active brazing alloy material having a total content of 1-15% by weight of at least one active element selected from the group consisting of Ti, Hf, Zr and V.
    Type: Application
    Filed: September 29, 2011
    Publication date: March 15, 2012
    Applicant: ALSTOM TECHNOLOGY LTD
    Inventors: Hans-Peter Bossmann, Alexander Schnell
  • Publication number: 20110300357
    Abstract: A thermal barrier coating system on a base material includes a bond coat layer with a lower face in direct contact with the base material and an upper face, a first ceramic layer in direct contact with the upper face of the bond coating layer and a second ceramic layer disposed on an outermost surface of the coating system and configured to be exposed to hot gas. The first ceramic layer includes a layer, combination, mixture, alloy, blend or multilayer structure of at least one of yttria-stabilized zirconia with a yttria content in a range of 6-8 wt-%, YTaO4 doped zirconia, and titania doped zirconia. The second ceramic layer includes a layer, combination, mixture, alloy, blend or multilayer structure of at least one of YTaO4 doped zirconia, titania doped zirconia, scandia stabilized zirconia, ceria containing perovskite material, yttrium aluminium garnet material, Monazite material, and spinel material. A material of the second ceramic layer is different from a material of the first ceramic layer.
    Type: Application
    Filed: June 15, 2011
    Publication date: December 8, 2011
    Applicant: ALSTOM TECHNOLOGY LTD
    Inventors: Gregoire Witz, Markus Schaudinn, Hans-Peter Bossmann, Matthieu Esquerre
  • Publication number: 20110058953
    Abstract: A turbine blade is provided having an airfoil and a platform manufactured in two separate pieces, which are joined together. The blade includes a seal, which is a mechanically decoupled seal, interposed between the airfoil and platform in a position closer to a hot gases path than a joint.
    Type: Application
    Filed: September 8, 2010
    Publication date: March 10, 2011
    Applicant: ALSTOM TECHNOLOGY LTD
    Inventors: Carlos Simon-Delgado, Hans-Peter Bossmann, Herbert Brandl
  • Publication number: 20100247953
    Abstract: A multilayer thermal protection system includes a metallic substrate; a first ceramic layer; a bond coat layer attaching the first ceramic layer to the metallic substrate, wherein the first ceramic layer is applied by plasma spraying; at least one second ceramic layer attached to the first ceramic layer, wherein the at least one second ceramic layer includes monolithic ceramic elements adhesively attached to the first ceramic layer; and a ceramic adhesive layer attaching the at least one second ceramic layer to the first ceramic layer.
    Type: Application
    Filed: March 12, 2010
    Publication date: September 30, 2010
    Applicant: ALSTOM TECHNOLOGY LTD
    Inventors: Hans-Peter Bossmann, Sharath Bachegowda, Matthieu Esquerre, Rico Iten
  • Publication number: 20100150727
    Abstract: A rotor blade (10) for a gas turbine includes a blade airfoil (11), a blade tip (15), a blade root (14), and a platform (12) which is formed between the blade tip (15) and the blade root (14), and is assembled from a plurality of individual sections (16, 17, 18), the material of which is adapted in each case to the intended purpose of the individual section concerned. With such a rotor blade, a simplified production is achieved as a result of each of the individual sections (16, 17, 18) from the dimensions being significantly smaller than the assembled rotor blade (10).
    Type: Application
    Filed: December 14, 2009
    Publication date: June 17, 2010
    Inventors: Herbert Brandl, Sven Schofer, Claus Paul Gerdes, Hans-Peter Bossmann