Dämpfer für eine Welle in einem Flugzeug

Details

Veröffentlichungs-Nr.

EP4273417

Aktenzeichen

EP23170446

Anmeldetag

27. April 2023

Veröffentlichung

8. November 2023

Rechtsraum

EP

IPC

F16D3/72F16D13/26F16F15/129B64D27/40F16C23/02F16F7/04F16F15/121F16F15/10F16C3/02

Abstract

A shaft system (34) includes an outer shaft (38) including an outer surface and an inner surface defining a conduit (50) and an inner shaft (52) extending along at least a portion of the conduit. The inner shaft (52) includes a radially extending passage. The inner shaft (52) has a first end (55) and a second end (57) that is opposite the first end. An input member (59) is arranged at the first end (55) of the inner shaft. A thrust damper (140) is arranged between the input member (59) and the inner shaft (52). The thrust damper (140) constrains relative rotation between the inner shaft (52) and the outer shaft (38).

Anmelder

Firma

Hamilton Sundstrand Corporation

Land

🇺🇸 USA

Fachgebiete