Aircraft section
US-2024343406-A1 · Oct 17, 2024 · US
Shell component for an aircraft or spacecraft
US9150299B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-9150299-B2 |
| Application number | US-200913130257-A |
| Country | US |
| Kind code | B2 |
| Filing date | Nov 25, 2009 |
| Priority date | Dec 1, 2008 |
| Publication date | Oct 6, 2015 |
| Grant date | Oct 6, 2015 |
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- Title
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Abstract
Official abstract text for this publication.
A shell component for an aircraft or spacecraft. The shell component includes a skin panel, a plurality of stringers which are arranged on the skin panel, a former which includes a fiber composite material and is arranged over the stringers so as to cross the stringers, and a former connection structure which includes a ductile material and a plurality of foot portions fixed to the skin panel. The foot portions each transition integrally into a shoulder portion fixed to the former over an associated fixing span, the fixing spans associated with the foot portions extending along the former substantially continuously over the stringers.
First claim
Opening claim text (preview).
The invention claimed is: 1. A fuselage shell component for an aircraft or spacecraft, comprising: a skin panel; a plurality of stringers which are arranged on the skin panel; a former which comprises a fibre composite material and is arranged over the stringers; and a former connection structure which comprises a ductile material, which is formed so as to absorb energy upon impact, and a plurality of foot portions fixed to the skin panel, each of which foot portions transitions in…
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Classifications
- B64C1/061Primary
Operations & Transport · mapped topic
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Frequently asked questions
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- What does patent US9150299B2 cover?
- A shell component for an aircraft or spacecraft. The shell component includes a skin panel, a plurality of stringers which are arranged on the skin panel, a former which includes a fiber composite material and is arranged over the stringers so as to cross the stringers, and a former connection structure which includes a ductile material and a plurality of foot portions fixed to the skin panel. …
- Who is the assignee on this patent?
- Tacke Stefan, Airbus Operations Gmbh
- What technology area does this patent fall under?
- Primary CPC classification B64C1/061. Mapped technology areas include Operations & Transport.
- When was this patent published?
- Publication date Tue Oct 06 2015 00:00:00 GMT+0000 (Coordinated Universal Time) (B2). Legal status and post-grant events are not shown on this page.
- What related patents are in patentsdb?
- We list 8 related publications on this page (citations in our corpus or others sharing the same primary CPC).