Elektrische Kabelleitung für ein Flugzeugtriebwerk

Details

Veröffentlichungs-Nr.

EP4745038

Anmeldetag

14. November 2025

Veröffentlichung

20. Mai 2026

Rechtsraum

EP

Abstract

An assembly for an aircraft powerplant (20) includes an engine case (72), a gearbox (102), a conduit (122), a first electric machine (92A), a first controller (94A) and a first electric cable (114A). The gearbox (102) is offset from the engine case (72). The conduit (122) extends longitudinally from a first end (124) of the conduit (122) to a second end (126) of the conduit (122). The conduit (122) is anchored to the engine case (72) at the first end (124) of the conduit (122) by a first conduit mount (136). The conduit (122) is anchored to the gearbox (102) at the second end (126) of the conduit (122) by a second conduit mount (138). The conduit (122) is self-supported longitudinally between the first conduit mount (136) and the second conduit mount (138). The first electric machine (92A) is mounted to the gearbox (102). The first controller (94A) is mounted to the engine case (72). The first electric cable (114A) electrically couples the first electric machine (92A) to the first controller (94A). The first electric cable (114A) extends longitudinally through a bore (134) of the conduit (122).

Anmelder

Firma

RTX Corporation

Land

🇺🇸 USA