Method for producing a composite skin in the field of aeronautics and astronautics

Patent metadata

Field	Value
Publication number	US-9314875-B2
Application number	US-60245908-A
Country	US
Kind code	B2
Filing date	May 15, 2008
Priority date	May 31, 2007
Publication date	Apr 19, 2016
Grant date	Apr 19, 2016

Abstract

A composite skin for the aeronautics and astronautics industries, and also a method for producing a composite skin of this type is provided. The method comprises the following method steps: removing excess material from a butt plate to form a butt strap at one end thereof, subsequently connecting the other end of the butt plate to a skin plate with a substance-to-substance bond, and then fastening a further skin plate to the butt strap to form the composite skin. The idea behind the invention involves replacing a rivet connection with a substance-to-substance bond. This provides the advantage that the weight of the composite skin and the production costs for the composite skin are reduced.

First claim

The invention claimed is:

1. A method for connecting a skin plate to a further skin plate to produce a skin for aeronautic and astronautic industries, comprising the following steps:
removing excess material at one end of a butt plate and further excess material at an other end of the butt plate to form the butt plate into a substantially Z-shaped cross-section, the butt plate having two parallel portions which overlap in their longitudinal direction in an overlapping region, wherein the overlapping region has a length substantially corresponding to a distance between the other end of the butt plate to an adjacent end of said overlapping region, the butt plate having a butt strap on the one end of the butt plate, the butt plate consisting of metal or metal alloy;
connecting the other end of the butt plate to the skin plate with a substance-to-substance bond, the skin plate consisting of metal or metal alloy, the substance-to-substance bond formed as a butt seam; and
fastening the further skin plate to the butt strap with a plurality of rivet rows to form the skin, wherein the length of the overlapping region is at least greater than a distance between two adjacent rows of the rivet rows, the further skin plate consisting of metal or metal alloy, wherein the skin plate, the butt plate and the further skin plate form a flush surface, wherein the fastening leaves a gap between the butt strap and the further skin plate in an axial direction of the skin, the gap corresponding to a region from which the excess material was removed from the one end of the butt plate.

2. The method according to claim 1 , wherein the substance-to-substance bond of the other end of the butt plate to the skin plate is made by means of friction stir welding, laser welding or electron beam welding.

3. The method according to claim 1 , wherein the excess material is removed by mechanical or chemical processing.

Assignees

• Stephan Andreas
• Airbus Operations Gmbh

Inventors

• Stephan Andreas

Classifications

• B23K2201/18

  Operations & Transport · mapped topic

• B21J15/142

  Aerospace structures · CPC title

• Y02T50/433

  Cross-Sectional Technologies · mapped topic

• Y10T29/49968

  Metal fusion joining · CPC title

• B64C1/069

  Joining arrangements therefor · CPC title