Zweistufiges Federbein, das eine Geringe Anfängliche Druckbelastung Erlaubt

Details

Veröffentlichungs-Nr.

EP3345828

Aktenzeichen

EP18150196

Anmeldetag

3. Januar 2018

Veröffentlichung

13. Mai 2020

Erteilung

13. Mai 2020

Rechtsraum

EP

IPC

B64C25/60B64D45/00B64C25/22

Abstract

A landing detection system (300) for a landing gear assembly of an aircraft may comprise a moveable member (309) mechanically coupled between an aircraft wheel and a strut piston (212), wherein the moveable member (309) is in communication with a strut chamber pressure of the landing gear assembly, wherein the moveable member (309) moves relative to the strut piston (212) in response to a first force applied to the aircraft wheel and the strut piston (212) strokes in response to a second force applied to the aircraft wheel.

Anmelder

Firma

Goodrich Corporation

Land

🇺🇸 USA

Fachgebiete