Selektive Leistungsverteilung für ein Flugzeugantriebssystem

Details

Veröffentlichungs-Nr.

EP4715178

Anmeldetag

5. September 2023

Veröffentlichung

25. März 2026

Rechtsraum

EP

IPC

F02C3/113

Abstract

An assembly is provided for an aircraft propulsion system. This assembly includes a carrier (90), a first gear system (86), a second gear system (88) and a lock device (106). The first gear system (88) includes a sun gear (92), a first ring gear (94) and a plurality of first intermediate gears (96) between and meshed with the sun gear (92) and the first ring gear (94). Each of the first intermediate gears (96) is rotatably mounted to the carrier (90). The second gear system (88) includes a second ring gear (102) and a plurality of second intermediate gears (104) meshed with the second ring gear (102). Each of the second intermediate gears (104) is rotatably mounted to the carrier (90). The lock device (106) is configured to lock rotation of the carrier (90) about an axis (28) during a first mode. The lock device (106) is configured to unlock rotation of the carrier (90) about the axis (28) during a second mode.

Anmelder

Firma

RTX Corporation

Land

🇺🇸 USA