An environmental control system of an aircraft includes at least one heat exchanger and a compression device arranged in fluid communication with the at least one heat exchanger. The compression device includes a plurality of components including a first component and a second component coupled by a shaft. A first bleed port is arranged in fluid communication with the first component and a second bleed port, distinct from the first bleed port, is arranged in fluid communication with the second component.
Simultaneous dual engine bleed thermal management system
2020-08-18
Patent
Electronic Resource
English
SIMULTANEOUS DUAL ENGINE BLEED THERMAL MANAGEMENT SYSTEM
European Patent Office | 2023
|SIMULTANEOUS DUAL ENGINE BLEED THERMAL MANAGEMENT SYSTEM
European Patent Office | 2020
|