Verfahren zur Herstellung eines Lasteinleitungsmerkmals für ein Faserverbundlaminatteil
Anmelder: Airbus Operations GmbH 🇩🇪
Details
- Veröffentlichungs-Nr.
- EP4112283
- Aktenzeichen
- EP21182907
- Anmeldetag
- 30. Juni 2021
- Veröffentlichung
- 4. Januar 2023
- Rechtsraum
- EP
- IPC
- B29C70/82B29C70/24B29C70/68B29C65/62B29C70/72// D04B21/16B64C1/00
Abstract
In order to improve load introduction into a fiber composite laminate part (52), the invention proposes to integrate a mounting lug (54) by pulling a cord (18) through an initial laminate structure (10) such that an opening (30) is formed. The ends (20, 22) of the cord (18) are split and pressed onto the laminate structure (10) thereby forming fixing members (36) that are subsequently covered by another laminate structure (38). Laminate patches (42) may be arranged next to the fixing members (36) so as to improve smoothness of the surface. The mounting lug (54) may be clamped between two plates (58) for mounting to another structure.
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.
4.382 Patente in unserer Datenbank