Antriebsstrang für ein Flugzeugtriebwerk mit Verstärktem Turbinenmotor

Details

Veröffentlichungs-Nr.

EP4803730

Anmeldetag

3. März 2026

Veröffentlichung

9. September 2026

Rechtsraum

EP

IPC

F02C3/107, F02C3/113, F02C7/36

Abstract

An assembly for an aircraft powerplant (20) includes a first powerplant component, a differential geartrain (156), a first clutch (164), a second clutch (166) and a first turbine engine (26). The first powerplant component includes a first component rotor. The differential geartrain (156) includes a first geartrain component and a second geartrain component. The first clutch (164) is configured to operatively couple the first geartrain component to the first component rotor during a first mode. The first clutch (164) is configured to operatively decouple the first geartrain component from the first component rotor during a second mode. The second clutch (166) is configured to operatively decouple the second geartrain component from the first component rotor during the first mode. The second clutch (166) is configured to operatively couple the second geartrain component to the first component rotor during the second mode. The first turbine engine (26) includes a first engine rotating structure (116) operatively coupled to the second geartrain component.

Anmelder

Firma

RTX Corporation

Land

🇺🇸 USA

Fachgebiete