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Dipl.-Ing. Heß Thomas

MTU Aero Engines

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Publication

Featured researches published by Dipl.-Ing. Heß Thomas.

Archive | 2010

Component, preferably aircraft component, which is formed of powder to be solidified by energy radiation source, comprises cavity with solidified powder, which is not solidified by energy radiation source and for forming damping element

Dipl.-Ing. Heß Thomas; Steffen Schlothauer

Archive | 2010

Manufacturing component, preferably e.g. guide vane of a turbomachine, comprises selective laser melting raw material powder using process gas, hot isostatic pressing resulting component, and precipitation hardening resulting component

Bayer Erwin; Dipl.-Ing. Heß Thomas; Andreas Jakimov; Kopperger Bertram

Archive | 2012

Method for producing honeycomb seal arranged between stator and rotor components of turbomachine in aircraft engine, involves forming seal portion of seal by fixation of material layers or formless material with high energy beam

Dipl.-Ing. Heß Thomas; Hessert Roland; Wilhelm Satzger

Archive | 2012

Producing three-dimensional metallic component such as component of aircraft engine, comprises applying of droplets that contain organometallic compound; and removing organic part of the organometallic compound in applied droplets

Bayer Erwin; Dipl.-Ing. Heß Thomas

Archive | 2011

Producing or repairing component, preferably components of turbomachine, comprises applying first material layer on base and solidifying, producing first component portion, and applying second material layer on produced component portion

Dusel Karl-Heinz; Dipl.-Ing. Heß Thomas; Andreas Jakimov; Klaus-Dieter Tartsch

Archive | 2010

Generatively producing component, preferably turbomachine, comprises solidifying powder bed in section-wise manner by energy input, to form local melt bath in powder bed, and vibrating powder bed for releasing gas components

Bayer Erwin; Dusel Karl-Heinz; Dipl.-Ing. Heß Thomas; Hans-Christian Melzer; Wilhelm Satzger; Dipl.-Ing. Sikorski Siegfried

Archive | 2012

Component, particularly guide vane for turbomachine, particularly gas turbine, comprises structural weakening in contact section for simplified removing, where component is formed as guide vane

Dusel Karl-Heinz; Dipl.-Ing. Heß Thomas; Dipl.-Ing. Humhauser Werner; Werner André

Archive | 2011

Verfahren zum schichtweisen Herstellen eines Bauteils sowie Vorrichtung Method for layered manufacturing a component and device

Bayer Erwin; Dipl.-Ing. Heß Thomas

Archive | 2010

Method for manufacturing or repairing e.g. housing of gas turbine, involves selectively adhering material layer in chemical film when connecting material layer with substrate, where material layer is adhered in form of component

Bayer Erwin; Broichhausen Klaus; Dusel Karl-Heinz; Dr.-Ing. Eisen Markus; Dipl.-Ing. Heß Thomas; Andreas Jakimov; Kopperger Bertram; Wilhelm Meir; Hans-Christian Melzer; Wilhelm Satzger; Dipl.-Ing. Sikorski Siegfried; Josef Wärmann

Archive | 2010

Verfahren zum Herstellen eines Bauteils und derartiges Bauteil

Bayer Erwin; Dipl.-Ing. Heß Thomas; Andreas Jakimov; Kopperger Bertram

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Bayer Erwin

MTU Aero Engines

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Andreas Jakimov

MTU Aero Engines

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Dusel Karl-Heinz

MTU Aero Engines

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Kopperger Bertram

MTU Aero Engines

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Wilhelm Satzger

MTU Aero Engines

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Broichhausen Klaus

MTU Aero Engines

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Dipl.-Ing. Sikorski Siegfried

MTU Aero Engines

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Dr.-Ing. Eisen Markus

MTU Aero Engines

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Hans-Christian Melzer

MTU Aero Engines

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Josef Wärmann

MTU Aero Engines

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