Planar structure for joining at least two components

Patent metadata

Field	Value
Publication number	US-9694441-B2
Application number	US-55990409-A
Country	US
Kind code	B2
Filing date	Sep 15, 2009
Priority date	Oct 8, 2008
Publication date	Jul 4, 2017
Grant date	Jul 4, 2017

Abstract

The invention relates to a planar structure for joining, in particular for the material-uniting joining, of at least two components. According to the invention, the planar structure is flexible and formed by at least one reaction strand. The reaction strand comprises a preferably cylindrical core, which is provided, at least in some areas, with a coating, which is constructed with a plurality of coaxially applied layers with a small thickness. To produce the layers, two different materials are used, the layers being constructed alternately with one of the two materials. Because of the high degree of flexibility of the reactive planar structure and its arbitrary area extent, components with a complex geometry in the region of the joint faces as well as large-format components can be joined in a material-uniting manner without problems. The reactive planar structure can be produced here using the methods known from textile engineering with virtually any dimensions and, in addition, by a continuous industrial production process. Moreover, the invention relates to a method for providing a material-uniting connection between two components, in particular by means of the planar structure according to the invention.

First claim

The invention claimed is:

1. A joint arrangement of a first component and a second component of an aircraft or spacecraft having curved joint faces, comprising:
a first component having a curved joint face;
a second component having a curved joint face, the joint face of the first component and the joint face of the second component being arranged adjacent to each other; and
a planar structure for the material-uniting joining of the first component and the second component arranged between the joint face of the first component and the joint face of the second component,
wherein the planar structure is adapted for use between curved joint faces and is formed by at least a first reaction strand and a second reaction strand, the first reaction strand and the second reaction strand being woven, interlaced, knitted or spatially arranged by any combination thereof, wherein the first and second reaction strands have a substantially cylindrical core respectively, which is provided, at least in some areas, with a coating and wherein an exothermic reaction can be triggered in the coating by a supply of heat, to join the first component and second component by a substance-to-substance bond, the first component and the second component being adapted to at least partially melt and to a limited extent mix their materials in the surface region, wherein the coating is formed by at least five coaxially applied thin layers, a first, third and fifth layer being formed by titanium and a second and fourth layer being formed by nickel, the first layer being arranged on the substantially cylindrical core, the second layer being arranged on the first layer, the third layer being arranged on the second layer, the fourth layer being arranged on the third layer and the fifth layer being arranged on the fourth layer.

2. The joint arrangement according to claim 1 , wherein the at least two layers each have a thickness of between 1.0 μm and 0.01 nm.

3. The joint arrangement according to claim 1 , wherein the core is formed by one carbon fibre filament.

4. The joint arrangement according to claim 1 , wherein at least one component is formed by a metallic material, formed by an aluminum alloy.

5. The joint arrangement according to claim 1 , wherein at least one component is formed by a non-metallic material, formed by a fibre-reinforced plastics material.

6. The joint arrangement according to claim 1 , wherein the planar structure is configured as a reinforcement fibre arrangement, wherein the reinforcement fibre arrangement is formed by a plurality of spatially arranged reinforcement fibres.

Assignees

• Syassen Freerk
• Winkelmann Yvonne
• Airbus Operations Gmbh

Inventors

• Syassen Freerk
• Winkelmann Yvonne

Classifications

• B29K2709/08

  Glass · CPC title

• B29K2101/12

  Thermoplastic materials · CPC title

• B29C66/7394

  characterised by the material of at least one of the parts being a thermoset · CPC title

• Y10T156/10

  Methods of surface bonding and/or assembly therefor · CPC title

• B29C66/472

  said single elements being substantially flat · CPC title