Komponentenhalte- und -Freigabeanordnung für ein Flugzeug und Flugzeug mit Solch einer Halte- und Freigabeanordnung

EP4516669 Art B1 10. Dezember 2025

Anmelder: Airbus Defence and Space GmbH 🇩🇪

Details

Veröffentlichungs-Nr.
EP4516669
Aktenzeichen
EP23193753
Anmeldetag
28. August 2023
Veröffentlichung
10. Dezember 2025
Erteilung
10. Dezember 2025
Rechtsraum
EP
IPC
B64D9/00
Offizieller Volltext

Abstract

A component hold and release arrangement (100) for an aircraft (1000) and an aircraft (1000) with such an arrangement is provided. The component hold and release arrangement (100) comprises a controller (10) and a first holding mechanism (20). The first holding mechanism (100) comprises a first latch (21), a first passive holding device (22) and a release threshold adjustment device (23). The first passive holding device (22) is connected to the first latch (21) and configured to prevent movement of the first latch (21) when a force exerted onto the first latch (21) is smaller than a first release threshold and to release the first latch (21) when the force exerted onto the first latch (21) reaches the first release threshold. The release threshold adjustment device (23) is functionally coupled to the first passive holding device (22) and adapted to adjust the first release threshold. The controller (10) is in communication with the release threshold adjustment device (23) and configured to communicate a corresponding adjustment value to the release threshold adjustment device (23) so as to adjust the first release threshold.

Anmelder

Firma
Airbus Defence and Space GmbH
Land
🇩🇪 Deutschland
🇩🇪 Airbus Defence and Space

Deutsche Sparte des Airbus-Konzerns, die militärische Flugzeuge, Satelliten, Raumfahrttechnik sowie Verteidigungs- und Sicherheitssysteme entwickelt.

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