Joint between aircraft components
US-9242715-B2 · Jan 26, 2016 · US
US10072690B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-10072690-B2 |
| Application number | US-201214342773-A |
| Country | US |
| Kind code | B2 |
| Filing date | Jun 14, 2012 |
| Priority date | Sep 5, 2011 |
| Publication date | Sep 11, 2018 |
| Grant date | Sep 11, 2018 |
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A hybrid component is formed by a profiled component of a first material, which is materially bonded in certain sections to a component made of a second material, and is connected by a form-fit and/or force-fit connection outside the sections with a material bond. This creates sections that relieve the strains resulting from differing thermal expansion.
Opening claim text (preview).
The invention claimed is: 1. A hybrid component for a structural element of vehicle seats, comprising: a profiled component made of a first material; and a component made of a second material, wherein the first material and the second material are different, wherein the profiled component is partially connected by a material connection to the component and is connected by a form-fitting connection and/or frictional connection outside the portions with the material connection, wherein the profiled component, which has a U-shaped cross section and a substantially planar flange region on both sides, is placed with its flange regions on a planar portion of the component, such that an internal space is formed between the profiled component and the component, wherein between the component and the flange regions an adhesive material is partially arranged as the material connection, wherein riveted connections are formed as the form-fitting connection and/or frictional connection outside the portions provided with the adhesive material in the flange regions, wherein, outside of the portions with the material connection and outside of the portions with the riveted connections, openings are formed on the profiled component and/or the component to allow for thermal compensation and/or to reduce the weight of the hybrid component, wherein riveted connections do not extend through the openings; and wherein the openings are elongated holes, wherein the portions of the flange regions provided with adhesive material are interrupted by regions in which the elongated holes are arranged, wherein the elongated holes are formed in the component and/or in the flange region of the profiled component, and wherein the elongated holes are aligned in their longitudinal extent according to the longitudinal extent of the flange region, such that the openings, the adhesive material, and the riveted connections are arranged alternately at the flange regions along the longitudinal extent of the hybrid component. 2. The hybrid component as claimed in claim 1 , wherein the openings are formed on the component. 3. The hybrid component as claimed in claim 1 , wherein the openings are through-holes.
including mechanical interlock · CPC title
Connections by glue bonding (in general F16B11/00; processes C09J5/00) · CPC title
preformed metal and synthetic material elements being joined together, e.g. by adhesives · CPC title
Assembling or joining · CPC title
Joining means · CPC title
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