Flugzeugtriebwerkmodul mit Integrierter Elektronik und Flüssigkeitskreislauf

Details

Veröffentlichungs-Nr.

EP4804748

Anmeldetag

5. März 2026

Veröffentlichung

9. September 2026

Rechtsraum

EP

IPC

H05K7/20

Abstract

An assembly for an aircraft powerplant includes an electric device (108A, 108B) and a closed loop fluid circuit (142A, 142B). The electric device includes a device housing (120A, 120B) and electrical circuitry (122A, 122B) housed within an interior of the device housing. The closed loop fluid circuit is configured to cool the electrical circuitry and includes a circuit path (146A, 146B) and a plurality of circuit components (148, 150, 152 and 154). The circuit path extends through the circuit components. Each of the circuit components are at least partially housed within the interior of the device housing. The circuit components may include a heat exchanger (150A, 150B).

Anmelder

Firma

RTX Corporation

Land

🇺🇸 USA

Fachgebiete