Klappflügel für einen Flugkörper und Flugkörper mit mindestens einem Darauf Angeordneten Klappflügel

Details

Veröffentlichungs-Nr.

EP3165870

Aktenzeichen

EP16197396

Anmeldetag

4. November 2016

Veröffentlichung

11. Juli 2018

Erteilung

11. Juli 2018

Rechtsraum

EP

IPC

F42B10/14F42B10/16

Abstract

A folding wing (2) for a missile comprises a wing root (6), an upper wing part (4) foldably supported at the wing root (6) around a swiveling axis (10), at least one first elastically pre-stressed force element and a latching device. The at least one first elastically pre-stressed force element (42) is coupled with the wing root (6) and the upper wing part (4) and is designed for permanently urging the upper wing part (4) into a working position relative to the wing root (6) through introducing a torque. The latching device is designed for arresting the upper wing part (4) on reaching the working position automatically.

Anmelder

Firma

MBDA Deutschland GmbH

Land

🇩🇪 Deutschland

Fachgebiete