Flugzeug mit einer Brennstoffzelle und einer Struktur mit einem Behälter mit einer Wärmeübertragungsflüssigkeit zur Sicherstellung der Kühlung der Brennstoffzelle

Details

Veröffentlichungs-Nr.

EP4029785

Aktenzeichen

EP22151288

Anmeldetag

13. Januar 2022

Veröffentlichung

9. April 2025

Erteilung

9. April 2025

Rechtsraum

EP

IPC

B64D33/02B64D33/08B64D37/00B64D37/30B64D41/00

Abstract

The invention relates to an aircraft comprising a structure (202) comprising a leakproof tank (210) delimited by walls, of which at least one is in contact with the air outside the aircraft, and filled partly with a two-phase heat-transfer fluid, a fuel cell (102) that is passed through by a heat-transfer fluid, and a line (106) which takes the heat-transfer fluid at an output of the fuel cell (102) and which reintroduces this heat-transfer fluid at an input of the fuel cell (102). The line (106) passes through the leakproof tank (210) immersed in the heat-transfer fluid in liquid phase.Such an installation avoids having to install a heat exchanger of large dimensions.

Anmelder

Firma

AIRBUS OPERATIONS

Land

🇫🇷 Frankreich

Fachgebiete