The patent badge is an abbreviated version of the USPTO patent document. The patent badge does contain a link to the full patent document.

The patent badge is an abbreviated version of the USPTO patent document. The patent badge covers the following: Patent number, Date patent was issued, Date patent was filed, Title of the patent, Applicant, Inventor, Assignee, Attorney firm, Primary examiner, Assistant examiner, CPCs, and Abstract. The patent badge does contain a link to the full patent document (in Adobe Acrobat format, aka pdf). To download or print any patent click here.

Date of Patent:
Jun. 04, 2013

Filed:

Oct. 18, 2010
Applicants:

Marc Bochinger, Elmshorn, DE;

Klaus Edelmann, Bremen, DE;

Thomas Lange, Delmenhorst, DE;

Tanja Frese, Horstedt, DE;

Sven Sperling, Schwanewede, DE;

Eugen Tschakrow, Voehl, DE;

Tobias Wirtz, Bremen, DE;

Inventors:

Marc Bochinger, Elmshorn, DE;

Klaus Edelmann, Bremen, DE;

Thomas Lange, Delmenhorst, DE;

Tanja Frese, Horstedt, DE;

Sven Sperling, Schwanewede, DE;

Eugen Tschakrow, Voehl, DE;

Tobias Wirtz, Bremen, DE;

Assignee:

Airbus Operations GmbH, Hamburg, DE;

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B27N 3/18 (2006.01);
U.S. Cl.
CPC ...
Abstract

The invention relates to a device for the production of an angle for connecting a fuselage cell skin to an annular former and/or a stringer inside a fuselage cell structure of an aircraft, the angle taking place by the one-step deformation of an initially planar blank along at least three fold lines in a uniaxial compression molding device. A mounting frame with hinges is arranged in the compression molding device, the blank to be deformed being accommodated along the edges preferably by means of a plurality of peripherally arranged springs. A deformation of the blank into an auto-stabilized angle is possible in one step while simultaneously ensuring interlaminar slide. Due to the constructively conditioned auto-stabilization of the angle, additional components which increase the weight and the assembly effort (so-called 'stabilos') in the connection region between fuselage cell skin, stringers and annular formers inside a fuselage structure of an aircraft are unnecessary.


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