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Raimund Lackermeier

MTU Aero Engines

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Publication

Featured researches published by Raimund Lackermeier.

Archive | 2004

Method for the production of components

Gerhard Andrees; Josef Kranzeder; Max Kraus; Raimund Lackermeier

Archive | 1987

Variable cooling device for turbo engine wall parts

Lothar Peichl; Horst Pillhoefer; Heinrich Walter; Raimund Lackermeier; Max Kraus

Archive | 2004

Rotor for a turbomachine, and method for the production of such a rotor

Gerhard Andrees; Manfred Berthan; Bertram Kopperger; Josef Kranzeder; Raimund Lackermeier; Axel Rossmann

Archive | 2005

Rotor für eine Turbomaschine und Verfahren zur Herstellung eines solchen Rotors

Gerhard Andrees; Bertram Kopperger; Manfred Berthan; Josef Kranzeder; Raimund Lackermeier; Axel Rossmann

Archive | 2005

Guide vane grid is blade rim or rim segment forming part of gas turbine with several fixed blades with ends fixed into and soldered in inner, outer ring segments; guide vanes are manufactured by powder metallurgical injection molding

Gerhard Andrees; Josef Kranzeder; Raimund Lackermeier; Axel Rossman

Archive | 2005

Production of aircraft gas turbine engine parts comprises injection molding mixture of metal powder and binder, molding then being sintered in at least two stages under different conditions to produce desired part

Gerhard Andrees; Max Kraus; Josef Kranzeder; Raimund Lackermeier

Archive | 2004

Rotor For A Turbo Machine And Method For The Manufacture Of Such A Rotor

Gerhard Andrees; Manfred Berthan; Bertram Kopperger; Josef Kranzeder; Raimund Lackermeier; Axel Rossmann

Archive | 2007

METHOD FOR THE PRODUCTION OF COMPONENTS OF A GAS TURBINE

Gerhard Andrees; Josef Kranzeder; Max Kraus; Raimund Lackermeier

Archive | 2007

Bonding of metallic components used in gas turbine construction, by hot isostatic pressing, first employs inductive press-welding to soften bonded surfaces and eliminate surface irregularities

Raimund Lackermeier; Reinhold Meier

Archive | 2005

Ring-shaped HIP-capsule for hot isostatic pressing (HIP) of ring-shaped metal matrix composite workpiece used for engine sealing rings has concentric bevels on its two axial sides

Gerhard Andrees; Manfred Berthan; Josef Kranzeder; Raimund Lackermeier; Bernhard Dr. Wöhrl

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Collaboration

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Gerhard Andrees

MTU Aero Engines

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Josef Kranzeder

MTU Aero Engines

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Max Kraus

MTU Aero Engines

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Manfred Berthan

MTU Aero Engines

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Axel Rossmann

MTU Aero Engines

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Bertram Kopperger

MTU Aero Engines

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Heinrich Walter

MTU Aero Engines

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Horst Pillhoefer

MTU Aero Engines

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Lothar Peichl

MTU Aero Engines

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Axel Rossman

MTU Aero Engines

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