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Michael Hanke

German Aerospace Center

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Publication

Featured researches published by Michael Hanke.

Archive | 2004

Surface heating for deicing composite aerodynamic structure uses electrically conducting reinforcing fibers to also act as resistance heating element

Holger Franken; Michael Hanke; Lars Herbeck

Archive | 2004

Heated composite molding tool for manufacture of fiber reinforced components is constructed in fiber reinforced plastic with embedded conductive electrical resistance heating element

Holger Franken; Michael Hanke; Lars Herbeck

Archive | 2003

Removing matrix resins from fiber-reinforced plastic components, preparatory to repair or joining, subjects defined region to microwave radiation

Michael Hanke; Markus Kleineberg; Matthias Meyer; Ulrich Riedel

Archive | 2009

Apparatus for preforming semifinished textile product, for use in fiber-resin composites, comprises continuous, automatic supplying and shearing devices to change fiber orientation

Michael Hanke; Dirk Holzhüter; Robert Kaps; Markus Kleineberg; Steffen Niemann; Tobias Ströhlein

Archive | 2009

Method for producing e.g. preform, from fiber-reinforced composite in molding tool, involves pressing vacuum foil against fiber scrim by pressure distribution applied by support structure, during evacuation of mold cavity

Michael Hanke; Andreas Metzler; Lars Herbeck

Archive | 2009

Verfahren zum Reparieren einer Flugzeugkomponente

Dirk Holzhüter; Michael Hanke; Babett Kujak

Archive | 2007

Molded part for aircraft, has radio frequency identification transponder directly arranged on barrier layer, covered by top layer and integrated between main structure and top layer, which is integrally connected to fiber connection

Michael Hanke; Lars Herbeck; Tim Berger

Archive | 2009

METHOD FOR REPAIRING A FLIGHT COMPONENT AND PATCH THEREFOR

Dirk Holzhüter; Michael Hanke; Babett Kujak

Archive | 2008

Semimonocoque-structured panel for use in e.g. airbus A-320, has stringer with hat profile exhibiting surface curved in direction of axis and transverse direction, where width of profile in transverse direction is set between frames

Axel Fink; Michael Hanke; Lars Herbeck; Christian Hühne; Markus Kleineberg; Boris Kolesnikov; Thomas Dipl.-Ing. Kruse

Archive | 2015

Design process and manufacturing of an unmanned blended wing-body aircraft

Benjamin Gramüller; Felix Stroscher; Jochen Schmidt; Tanut Ungwattanapanit; Thomas Löbel; Michael Hanke

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Collaboration

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Markus Kleineberg

German Aerospace Center

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Dirk Holzhüter

German Aerospace Center

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Lars Herbeck

German Aerospace Center

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Tobias Ströhlein

German Aerospace Center

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Jochen Schmidt

German Aerospace Center

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Robert Kaps

German Aerospace Center

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Andreas Metzler

German Aerospace Center

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Herbeck Lars

German Aerospace Center

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Holger Franken

German Aerospace Center

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Steffen Niemann

German Aerospace Center

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