Method for manufacturing a shell element reinforced with support elements

Patent metadata

Field	Value
Publication number	US-10023287-B2
Application number	US-201414566010-A
Country	US
Kind code	B2
Filing date	Dec 10, 2014
Priority date	Dec 12, 2013
Publication date	Jul 17, 2018
Grant date	Jul 17, 2018

Abstract

A method for manufacturing a shell element reinforced with support elements comprises providing a skin element that has an outer surface and an inner surface opposite the outer surface, providing a first support element that has an attaching side and a free side opposite the attaching side, attaching the first support element on the skin element such that the attaching side of the first support element faces the inner surface of the skin element. A first recess is introduced into the first support element that proceeds from the free side of the first support element and extends transversely to the first axis. A second support element is provided that has a support side and a front side opposite the support side. The second support element is inserted into the first recess of the first support element such that the support side faces the inner surface of the skin element.

First claim

What is claimed is:

1. A method for manufacturing a shell element reinforced with support elements, having the following steps of:
(a) providing a skin element that has an outer surface and an inner surface disposed opposite the outer surface;
(b) providing a first support element that extends along a first axis and has an attaching side that is parallel to the first axis, and a free side opposite the attaching side;
(c) attaching the first support element on the skin element such that the attaching side of the first support element faces the inner surface of the skin element;
(d) forming a first recess on the first support element, which proceeds from the free side of the first support element and extends transversely to the first axis;
(e) providing a second support element that extends along a second axis and has a support side that is parallel to the second axis, and a front side opposite the support side;
(f) inserting the second support element into the first recess of the first support element such that the support side faces the inner surface of the skin element, and such that the second axis of the second support element extends transversely to the first axis of the first support element; and
(g) attaching the second support element on the first support element and/or on the skin element;
wherein a projection is provided on the first support element, the projection extending on the free side away from the skin element;
wherein the first recess is formed in the projection; and
wherein the projection is formed by removing material from the first support element, on the free side thereof, on both sides of the first recess and at a distance from the first recess.

2. The method of claim 1 , wherein a second recess is formed on the second support element, the recess extending from the support side of the second support element and transversely to the second axis, and
wherein the second support element is inserted into the first recess of the first support element at the location of the second recess such that the first and second recesses intersect one another during the insertion, and the sections of the second support element located next to the second recess encompass the first support element.

3. The method of claim 2 , wherein the first recess extends from the free side to a first end point that is spaced apart from the attaching side by a first distance,
wherein the second recess extends from the support side to a second end point that is spaced apart from the front side by a second distance, and
wherein the length of the first distance corresponds to the length of the second recess from the support side to the second end point.

4. The method of claim 1 , wherein a first end point of the first recess lies in the plane in which the free side extends next to the projection.

5. The method of claim 1 , further comprising attaching the first support element on the skin element by means of prepreg layers that are placed onto lateral surfaces of the first support element, between the attaching side and the free side, and onto regions of the inner surface of the skin element, next to the first support element, and which are subsequently cured.

6. The method of claim 1 , further comprising attaching the second support element on the first support element by means of prepreg layers that are placed onto lateral surfaces of the first support element, between the attaching side and the free side, and onto lateral surfaces of the second support element, between the support side and the front side, and which are subsequently cured.

7. The method of claim 1 , wherein the second support element is attached on the skin element by means of prepreg layers that are placed onto lateral surfaces of the second support element, between the support side and the front side, and onto regions of the inner surface of the skin element, next to the second support element, and which are subsequently cured.

8. The method of claim 1 , wherein, after the second support element has been attached on the first support element and/or on the skin element, the projection is removed to a level at which the free side extends next to the projection.

9. The method of claim 1 , further comprising providing, on the skin element, additional support elements that are parallel to the first and/or the second support element.

10. A method for manufacturing a shell element reinforced with support elements, having the following steps of:
providing a skin element that has an outer surface and an inner surface disposed opposite the outer surface;
providing a first support element that extends along a first axis and has an attaching side that is parallel to the first axis, and a free side opposite the attaching side;
attaching the first support element on the skin element such that the attaching side of the first support element faces the inner surface of the skin element;
forming a first recess on the first support element, which proceeds from the free side of the first support element and extends transversely to the first axis;
providing a second support element that extends along a second axis and has a support side that is parallel to the second axis, and a front side opposite the support side;
inserting the second support element into the first recess of the first support element such that the support side faces the inner surface of the skin element, and such that the second axis of the second support element extends transversely to the first axis of the first support element; and
attaching the second support element on the first support element and/or on the skin element;
wherein a projection is provided on the first support element, the projection extending on the free side away from the skin element;
wherein the first recess is formed in the projection; and
wherein, after the second support element has been attached on the first support element and/or on the skin element, the projection is removed to a level at which the free side extends next to the projection.

Assignees

• Airbus Operations Gmbh
• Airbus Operation GmbH

Inventors

• Räckers Bernd
• Gerber Martin

Classifications

• B29L2031/3097

  Cosmonautical vehicles; Rockets · CPC title

• B32B38/0004

  Cutting, tearing or severing, e.g. bursting; Cutter details (cutting in general B26D; laminating combined with punching or perforating B32B38/04; removing all or part of the layers B32B38/10; cutting in combination with laying up and registration B32B38/185 takes precedence) · CPC title

• B29C66/5326

  said single elements being substantially flat · CPC title

• B29C66/7212

  characterised by the composition of the fibres · CPC title

• B29L2031/3082

  Fuselages · CPC title