US 2013/0094898 A1Published application

Component, reinforcement member, structural arrangement, aircraft or spacecraft and method

AssigneeAirbus Operations GmbH

InventorsOliver SEACK, Alexander BRUNS

Life of this patent

Estimating the term…

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Abstract

A component for connecting structures to intersection regions of said component is disclosed, particularly for an aircraft or spacecraft, including a coupling element, including a first fibre which wraps around the coupling element so that the first fibre extends in a first plane in front of the coupling element and in a second plane behind the coupling element, the first and second planes intersecting, and including a second fibre which wraps around the coupling element so that the second fibre extends in a third plane in front of the coupling element and in a fourth plane behind the coupling element, the third and fourth planes intersecting, and with the first fibre portions of the first and second fibres crossing over in a first region and the second fibre portions of the first and second fibres crossing over in a second region.

Claims15

Dependent claims

A component for connecting structures to intersection regions of said component, in particular for an aircraft or spacecraft,

comprising a coupling element,
comprising a first fibre which wraps around the coupling element in such a way that the first fibre extends, with a first fibre portion, in a first plane in front of the coupling element and, with a second fibre portion, in a second plane behind the coupling element, the first and second planes intersecting, and
comprising a second fibre which wraps around the coupling element in such a way that the second fibre extends, with a first fibre portion, in a third plane in front of the coupling element and, with a second fibre portion, in a fourth plane behind the coupling element, the third and fourth planes intersecting,
the first fibre portions of the first and second fibres crossing over in a first region and the second fibre portions of the first and second fibres crossing over in a second region.

1 more element

Dependencies are inferred from the claim text.

Facts

Application: 13/649,203Filed 11 Oct 2012
Priority: DE 10 2011 084 433.313 Oct 2011
Published: 18 Apr 2013
Term ends: Not estimatedThe source records don’t support an estimate.

Classification10 codes

B64C 1/00
Fuselages
B29C 70/205
Oriented in a single direction, e.g. roofing or other parallel fibres: the structure being shaped to form a three-dimensional configuration
B29C 70/222
Oriented in at least two directions forming a two-dimensional [2D] structure: the structure being shaped to form a three dimensional configuration
B29C 70/86
By incorporating or moulding on preformed parts, e.g. inserts or layers , e.g. foam blocks: incorporated in coherent impregnated reinforcing…