An airplane is provided. The airplane includes a pressurized compartment and an environmental control system. The environmental control system includes a compressing device. The compressing device includes a compressor and a turbine. The airplane also includes a first flow of first medium configured to enter the pressurized compartment and a second flow of the first medium configured to enter the turbine.
NO PRIMARY HEAT EXCHANGER AND BLEED AIR (CABIN DISCHARGE AIR) ASSIST
UNTERSTÜTZUNG DER ZAPFLUFT (KABINENABLUFT) OHNE PRIMÄRWÄRMETAUSCHER
ÉCHANGEUR DE CHALEUR NON PRIMAIRE ET ASSISTANCE À L'AIR DE PRÉLÈVEMENT (AIR D'ÉVACUATION DE CABINE)
2024-08-07
Patent
Electronic Resource
English
No primary heat exchanger and bleed air (cabin discharge air) assist
European Patent Office | 2018
|NO PRIMARY HEAT EXCHANGER AND BLEED AIR (CABIN DISCHARGE AIR) ASSIST
European Patent Office | 2016
|NO PRIMARY HEAT EXCHANGER AND BLEED AIR (CABIN DISCHARGE AIR) ASSIST
European Patent Office | 2016
|CABIN DISCHARGE AIR ASSIST WITHOUT A PRIMARY HEAT EXCHANGER
European Patent Office | 2023
|