Reduzierung der Wirbelstromausbreitung in einem Gehäuse einer Elektrischen Vorrichtung

Details

Veröffentlichungs-Nr.

EP4776776

Anmeldetag

17. Dezember 2025

Veröffentlichung

15. Juli 2026

Rechtsraum

EP

IPC

H05K9/00

Abstract

An aircraft assembly includes a first electric cable (124A) and an electric device (122). The electric device (122) includes a device housing (126) and a first electric terminal (156A) disposed within an internal volume (130) of the device housing (126). The device housing (126) includes a first metal sidewall (140A), a first wall cable port (150) and an open first wall aperture (152A-C) next to the first wall cable port (150). The first metal sidewall (140A) is between and borders the internal volume (130) and an external environment (148). The first wall cable port (150) projects through the first metal sidewall (140A) from the external environment (148) to the internal volume (130). The open first wall aperture (152A-C) projects through the first metal sidewall (140A) from the external environment (148) to the internal volume (130). The first electric cable (124A) projects longitudinally through the first wall cable port (150) into the internal volume (130). The first electric cable (124A) is received by and is electrically coupled to the first electric terminal (156A) within the internal volume (130).

Anmelder

Firma

RTX Corporation

Land

🇺🇸 USA

Fachgebiete