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.
Patent No.:
Date of Patent:
Apr. 14, 2015
Filed:
Sep. 16, 2009
Marco Goettinger, Munich, DE;
Tamas Havar, Bruckmuehl, DE;
Xavier Hue, Bremen, DE;
Franz Stadler, Boehmfeld, DE;
Marco Goettinger, Munich, DE;
Tamas Havar, Bruckmuehl, DE;
Xavier Hue, Bremen, DE;
Franz Stadler, Boehmfeld, DE;
EADS Deutschland GmbH, Ottobrunn, DE;
AIRBUS Operations GmbH, Hamburg, DE;
Abstract
A load introducing element for a control surface of an aircraft or a spacecraft comprises at least one first component, one second component and one first flange. At least one surface area of the first component is adapted to conform to the inner contour of the control surface. The second component has at least one eye for receiving bearing means for mounting the control surface. A cross sectional profile of the first component has two or more essentially straight legs, which are connected together on their upper side by an upper edge which is adapted to an upper contour of the control surface. The load introducing element is formed by a fiber reinforced composite material having an integral type of construction in which all of the components are jointly infiltrated and cured. The invention also provides a method for producing such a load introducing element, a drive armature and an aircraft that includes such a load bearing element.