Method and system for connecting two aircraft components from a thermoplastic composite material
US-10822120-B2 · Nov 3, 2020 · US
US11754102B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-11754102-B2 |
| Application number | US-202016749051-A |
| Country | US |
| Kind code | B2 |
| Filing date | Jan 22, 2020 |
| Priority date | Jan 31, 2019 |
| Publication date | Sep 12, 2023 |
| Grant date | Sep 12, 2023 |
A practical reading order for non-experts. Skip the full description unless you need deep technical detail.
What the patent document calls the invention.
A short plain-language summary of the technical disclosure.
Who owns or filed the patent and who is credited as inventor.
Filing, priority, publication, and grant dates set the timeline.
The legal scope of protection — read this for what is actually claimed.
Technology tags used to group this patent with similar filings.
Prior art links and similar publications in this corpus.
Official abstract text for this publication.
A method is provided for producing a common connecting opening in two components, at least one of which is made from a plastically deformable material. In the method, at least the edge region of a first prefabricated opening of the first component is softened in order subsequently to introduce a mandrel which displaces the material softened by the heating so that a common connecting opening having a predetermined diameter is obtained.
Opening claim text (preview).
The invention claimed is: 1. A method for producing a common connecting opening in two components, at least one of which is made from a plastically deformable material, comprising the steps: providing a first component made of a plastically deformable material, the first component having a first opening, a first sidewall around the first opening, and a thickness at the first opening defined in an axial direction at the first sidewall, providing a second component having a second opening, a second sidewall around the second opening, and a thickness at the second opening defined in the axial direction at the second sidewall, assembling the first component and the second component so that the first opening and the second opening lie on one another, enclosing the first component and the second component between a first restricting body and a second restricting body in an edge region around the respective opening, softening the material at least of the edge region of the first component, heating a mandrel, introducing the mandrel into the first and second openings so that softened material moves between the two edge regions and surrounds the mandrel in order to provide a common connecting opening, and setting the material, the mandrel having an outer diameter which corresponds to a target diameter of the common connecting opening, wherein the first opening has a first opening radius, wherein the second opening has a second opening radius, wherein the mandrel has a mandrel outer radius, and wherein the first opening radius, the second opening radius and the mandrel outer radius are dimensioned in such a way that, when the mandrel is introduced and extends through the first opening and the second opening, the first component, the second component and the mandrel are in flush surface contact with one another, and a sum of the thickness at the first opening of the first component and the thickness at the second opening of the second component is unchanged. 2. The method according to claim 1 , wherein the softening of the material comprises softening of the material of the edge regions of the first component and the second component. 3. The method according to claim 1 , wherein the first opening has a smaller diameter than the second opening. 4. The method according to claim 1 , wherein a mandrel outer diameter is greater than a diameter of the first opening and less than a diameter of the second opening. 5. The method according to claim 1 , wherein the mandrel is driven from a cavity arranged in the first restricting body into a second cavity of the second restricting body. 6. The method according to claim 1 , furthermore comprising the use of a connecting element as the mandrel, which remains in the common connecting opening after the setting of the material.
using mechanical means {or mechanical connections, e.g. form-fits} · CPC title
of sheets or plates mutually (joining sheets by riveting without the use of separate rivets F16B5/045) · CPC title
by using permanent deformation · CPC title
Joining a non-plastics element to a plastics element, e.g. by force (B29C65/44 takes precedence) · CPC title
by heating, with or without pressure · CPC title
Related publications grouped by family.
Answers are generated from the same data shown on this page.