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Markus J. Weber

Airbus

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Publication

Featured researches published by Markus J. Weber.

Archive | 2010

FUSELAGE CELL STRUCTURE FOR AN AIRCRAFT IN HYBRID DESIGN

Wolf-Dietrich Dolzinski; Norbert Heltsch; Arne Hartwig; Markus Mueller; Markus J. Weber; Jens-Ulrich Prowe; Paul Joern

Archive | 2009

Aircraft fuselage structure has skin field, where diagonal stiffening elements are formed by skin-field polygons, and stiffening frames are designed for limiting fuselage section

Paul Jörn; Wolfgang Machunze; Jens Prowe; Markus J. Weber

Archive | 2009

Reinforcement structure for sheet material for skin field of fuselage of aircraft, has stringers merged in intersection regions and defining closed meshes with different sizes, and ribs led above stringers and intersection regions

Paul Jörn; Ralf Lonthoff; Wolfgang Machunze; Lars Meyer; Jens Prowe; Markus J. Weber

Archive | 2009

Grid-like reinforcement structure for reinforcing skin field of fuselage of aircraft, has rigid parts merged in intersection regions, and load transfer element arranged in intersection region and in active connection with parts

Paul Jörn; Markus J. Weber; Jens Prowe; Wolfgang Machunze; Gastao De Freitas

Archive | 2009

Butt joint for longitudinal welding and/or mating of two fuselage sections of aircraft, has butt strap including elevations within region of stiffeners, where elevations extend in longitudinal direction of stiffeners

Paul Jörn; Wolfgang Machunze; Jens Prowe; Markus J. Weber

Archive | 2010

WINDOW ELEMENT FOR A DOUBLE-SHELL SKIN FIELD OF AN AIRCRAFT FUSELAGE CELL

Wolf-Dietrich Dolzinski; Norbert Heltsch; Arne Hartwig; Markus Mueller; Markus J. Weber; Jens-Ulrich Prowe; Paul Joern

Archive | 2009

Shell-like component i.e. fiber composite shell, manufacturing device for commercial aircraft body, has cores comprising inclined surface for defining wedge-shaped intermediate area, and retaining element inserted into intermediate area

Boris Ehrhardt; Paul Jörn; Lars Meyer; Markus J. Weber

Archive | 2009

Stiffening structure, particularly for aircraft fuselage, has three-dimensional struts arranged on skin field, where struts are made of fiber-reinforced composite material

Paul Jörn; Wolfgang Machunze; Jens Prowe; Markus J. Weber

Archive | 2009

Longitudinal welded joint for two fuselage sections, particularly for airplane, comprises overlapping joint formed by two fuselage sections, where opposite braces are connected with each other

Paul Jörn; Wolfgang Machunze; Jens Prove; Markus J. Weber

Archive | 2009

Stiffening structure and method for manufacturing such a structure

Paul Jörn; Markus J. Weber; Jens Prowe; Wolfgang Machunze

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Collaboration

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Wolfgang Machunze

Airbus Defence and Space

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Jens Prowe

Airbus

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Jens-Ulrich Prowe

Airbus

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Lars Meyer

Airbus

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Arne Hartwig

Airbus

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Markus Mueller

Airbus

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Norbert Heltsch

Airbus

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Paul Joern

Airbus

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Wolf-Dietrich Dolzinski

Airbus

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