Verfahren zum Verbinden von Strukturprofilen
Anmelder: Airbus Operations GmbH 🇩🇪
Details
- Veröffentlichungs-Nr.
- EP4129817
- Aktenzeichen
- EP21190160
- Anmeldetag
- 6. August 2021
- Veröffentlichung
- 8. Februar 2023
- Rechtsraum
- EP
- IPC
- B64C1/06F16B4/00
Abstract
A method for joining structural profiles (1a, 1b), in particular curved or angular structural profiles of an aircraft, comprises forming a first structural profile (1a) with a first mating contour (2a) at a first opening end (3a) and a second structural profile (1b) with a second mating contour (2b) at a second opening end (3b), the first mating contour being complementary formed to the second mating contour; changing a size of at least one of the structural profiles (1a, 1b) at least at the respective mating contour by expansion or contraction of the respective structural profile; sliding both structural profiles into each other at their respective opening ends while changed in size such that the structural profiles overlap at the mating contours; and reversing the size change of the respective structural profiles by contraction or expansion such that at least one of a form fit or an interference fit is formed between the structural profiles at their mating contours.
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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