Joining components

Patent metadata

Field	Value
Publication number	US-10987876-B2
Application number	US-201816182022-A
Country	US
Kind code	B2
Filing date	Nov 6, 2018
Priority date	Nov 8, 2017
Publication date	Apr 27, 2021
Grant date	Apr 27, 2021

Abstract

A method for joining a first component and a second component. The method includes forming a first bond between the first component and the second component by providing a plurality of projections on the first component and embedding the plurality of projections in the second component; creating a fastener hole which passes through the first component and the second component and which encompasses at least one of the projections; and forming a second bond between the first component and the second component by installing a fastener in the fastener hole.

First claim

The invention claimed is:

1. A method for joining a first component and a second component, the method comprising:
forming a first bond between the first component and the second component by providing a plurality of projections on the first component and embedding the plurality of projections in the second component;
creating a fastener hole which passes through the first component and the second component and which encompasses at least one of the projections; and
forming a second bond between the first component and the second component by installing a fastener in the fastener hole,
wherein the plurality of projections comprises a first array of one or more projections provided on a first region of the first component and a second array of one or more projections provided on a second region of the first component, and
wherein the fastener hole encompasses the first array of one or more projections, such that the first array of one or more projections is entirely removed by the creation of the fastener hole.

2. The method of claim 1 , wherein a location of each of the first region and the second region corresponds to an intended fastener location for fastening the first component to the second component.

3. The method of claim 1 , further comprising creating a further fastener hole which passes through the first component and the second component and which encompasses at least some of the projections not encompassed by the fastener hole, wherein a second bond is formed additionally by installing a further fastener into the further fastener hole.

4. The method of claim 3 , wherein the further fastener hole encompasses the second array of one or more projections, such that the second array of one or more projections is entirely removed by the creation of the further fastener hole.

5. The method of claim 1 , wherein the fastener hole is a pilot hole having a diameter smaller than the diameter of a final fastener hole intended to be created at the same location as the pilot hole, and wherein the fastener is a temporary fastener.

6. The method of claim 1 , wherein the second component comprises a composite material, and wherein embedding the plurality of projections into the second component comprises penetrating the plurality of projections into the second component in a pre-cured state of the second component, and subsequently curing the second component.

7. The method of claim 1 , wherein the at least one projection encompassed by the fastener hole is comprised in a subcomponent, and wherein providing a plurality of projections on the first component comprises arranging the subcomponent on the first component.

8. The method of claim 7 , wherein the fastener hole encompasses the subcomponent, such that the subcomponent is entirely removed by the creation of the fastener hole.

9. The method of claim 7 , wherein the subcomponent comprises a head and a shaft, wherein the at least one projection is on an end of the shaft distal from the head, and wherein when the subcomponent is arranged on the first component the shaft extends through a hole in the first component such that the head is adjacent one side of the hole and the at least one projection extends from an opposite side of the hole.

10. The method of claim 9 , wherein forming the first bond between the first component and the second component comprises:
arranging the second component adjacent to the hole in the first component; and
inserting the shaft of the subcomponent into the hole in the first component such that the at least one projection on the subcomponent penetrates the second component.

11. The method of claim 7 , wherein the subcomponent is formed by an additive manufacturing process and the first component is not formed by an additive manufacturing process.

12. The method of claim 1 , wherein the plurality of projections is formed by an additive manufacturing process.

13. The method of claim 1 , wherein the first and second components are aircraft components.

Assignees

• Airbus Operations Ltd

Inventors

• Gow Piers

Classifications

• B29C65/562 Primary

  using extra joining elements, i.e. which are not integral with the parts to be joined (using plastic snap elements B29C65/58; using plastic rivets B29C65/601) · CPC title

• B29C2793/0045

  Perforating · CPC title

• B33Y80/00

  Products made by additive manufacturing · CPC title

• B29C66/3034

  making use of additional elements, e.g. meshes · CPC title

• B29C66/73753

  the to-be-joined area of at least one of the parts to be joined being partially cured, i.e. partially cross-linked, partially vulcanized · CPC title