Flugzeug mit einem Wärmetauscher

Details

Veröffentlichungs-Nr.

EP3069997

Aktenzeichen

EP15382117

Anmeldetag

16. März 2015

Veröffentlichung

29. April 2020

Erteilung

29. April 2020

Rechtsraum

EP

IPC

B64D13/06

Abstract

The invention provides an aircraft (1) comprising a heat exchanging pack (10) comprising an energy recovering module (11) with a hot and a cold side, the hot side being in thermal contact with the cold side, thus causing a heat exchange. The heat exchanging pack also comprises a secondary heat exchanger (12) and a compressor (13) coupled with a turbine (14). The hot side inlet (111) of the energy recovering module (11) is in fluid communication with the bleed air duct (3), the cold side inlet (113) of the energy recovering module (11) is in fluid communication with the ram air duct (5), the hot side outlet (112) of the energy recovering module (11) is in fluid communication with the compressor inlet, the compressor outlet is in fluid communication with the hot side inlet (121) of the secondary heat exchanger (12), the hot side outlet (122) of the secondary heat exchanger (12) is in fluid communication with the turbine inlet, and the cold side inlet of the secondary heat exchanger (12) is in fluid communication with the ram air duct (5). Furthermore, the energy recovering module (11) comprises conversion means (6), adapted to generate energy out from the heat exchange that takes place in the energy recovering module (11) between the hot side and the cold side.

Anmelder

Firma

Airbus Operations S.L.

Land

🇪🇸 Spanien

Fachgebiete