Torsionsrohranordnung Welches Axiallasten Übertragen Kann sowie Fertigungsverfahren davon

Details

Veröffentlichungs-Nr.

EP3822164

Aktenzeichen

EP20207815

Anmeldetag

16. November 2020

Veröffentlichung

2. August 2023

Erteilung

2. August 2023

Rechtsraum

EP

IPC

B64C13/28F16C13/02F16D1/072F16D1/08

Abstract

An assembly and a method for manufacturing an assembly for transmitting torque to an aircraft actuator. The assembly and method include a torque tube (105) having a longitudinal axis and an end fitting (301). The ending fitting includes a connector portion (303) and an engagement portion (302) that is inserted into the torque tube. The engagement portion includes a first end (304) adjacent the connector portion, a second end (308) opposite the first end, and a coupling region between the first and second end that includes an outer coupling surface having an outer diameter and a continuous groove (307) formed thereon. The continuous groove includes two axial grooves (310) that extend along the outer coupling surface along the longitudinal axis and a first parallel groove (111) that extends circumferentially about the longitudinal axis along the outer coupling surface that joins the two axial grooves.

Anmelder

Firma

Hamilton Sundstrand Corporation

Land

🇺🇸 USA

Fachgebiete