Verfahren zum Herstellen eines Verbundstoffschalenelements
Anmelder: Airbus Operations GmbH 🇩🇪
Details
- Veröffentlichungs-Nr.
- EP2730397
- Aktenzeichen
- EP12191653
- Anmeldetag
- 7. November 2012
- Veröffentlichung
- 22. Januar 2020
- Erteilung
- 22. Januar 2020
- Rechtsraum
- EP
- IPC
- B29C70/54B29C35/02B29C53/02B29C53/04B32B3/06
Abstract
The present invention relates to the fabrication of composite shell elements and to the assembly of large scale structures comprising such composite shell elements. The composite shell elements comprise two regions in which the resin is cured to different levels. As a consequence, the flexibility of the first region is greater than the flexibility of the second region. Since the first region defines a bending line, the composite shell element can be deformed along the bending line during assembly of the large scale structure. Thus, tolerances in fabrication of the composite shell elements may be compensated for in a time-efficient manner without the need for applying a shimming process.
Anmelder
- Firma
- Airbus Operations GmbH
- Land
- 🇩🇪 Deutschland
Deutsche Tochtergesellschaft des europäischen Luft- und Raumfahrtkonzerns Airbus mit Standorten wie Hamburg. Entwickelt und fertigt Flugzeugstrukturen und Komponenten für die zivile Luftfahrt.
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