Markus J. Weber

FUSELAGE CELL STRUCTURE FOR AN AIRCRAFT IN HYBRID DESIGN

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

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

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

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

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

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

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

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

Stiffening structure and method for manufacturing such a structure