Simultanes Dual-Bleed System für ein Wärmemanagementsystem

Details

Veröffentlichungs-Nr.

EP3587268

Aktenzeichen

EP19171570

Anmeldetag

29. April 2019

Veröffentlichung

12. April 2023

Erteilung

12. April 2023

Rechtsraum

EP

IPC

B64D13/06

Abstract

An environmental control system of an aircraft includes at least one heat exchanger (70) and a compression device (60) arranged in fluid communication with the at least one heat exchanger. The compression device includes a plurality of components including a first component (62) and a second component (64) coupled by a shaft (68). A first bleed port (38) is arranged in fluid communication with the first component and a second bleed port (40), distinct from the first bleed port, is arranged in fluid communication with the second component.

Anmelder

Firma

Hamilton Sundstrand Corporation

Land

🇺🇸 USA

Fachgebiete