Vibration der Federbeine eines Flugzeugs zur Entlastung eines Teils der auf die Federbeine Wirkenden Statischen Reibungskräfte vor der Bestimmung des Gewichts und des Gleichgewichts des Flugzeugs

Details

Veröffentlichungs-Nr.

EP4814449

Anmeldetag

10. März 2026

Veröffentlichung

30. September 2026

Rechtsraum

EP

IPC

G01G19/07

Abstract

A system for an aircraft includes a shock strut of a landing gear. The system includes one or more excitation devices coupled to the shock strut. The one or more excitation devices are configured to vibrate the shock strut to enable the shock strut to transition from a first static state where an outer cylinder of the shock strut is stationary relative to an inner cylinder of the shock strut to a dynamic state where the outer cylinder moves relative to the inner cylinder and to transition from the dynamic state to a second static state. The system also includes a resonance system coupled to the one or more excitation devices. The resonance system is configured to provide a first signal to the one or more excitation devices to activate the one or more excitation devices to vibrate the shock strut.

Anmelder

Firma

The Boeing Company

Land

🇺🇸 USA

Fachgebiete