An environmental control system includes a low pressure tap at a location on a first compressor section of a main compressor section. The low pressure tap communicates airflow to a first passage leading to a downstream outlet. A compressor is driven by an electric motor. A combined outlet intermixes airflow from the first passage and from the compressor driven by the electric motor and passes the airflow downstream to be delivered to an aircraft use.
SIMPLIFIED ENGINE BLEED SUPPLY WITH LOW PRESSURE ENVIRONMENTAL CONTROL SYSTEM FOR AIRCRAFT
2018-07-26
Patent
Electronic Resource
English
Simplified engine bleed supply with low pressure environmental control system for aircraft
European Patent Office | 2018
|Simplified engine bleed supply with low pressure environmental control system for aircraft
European Patent Office | 2020
|LOW-PRESSURE BLEED AIR AIRCRAFT ENVIRONMENTAL CONTROL SYSTEM
European Patent Office | 2015
|Low-pressure bleed air aircraft environmental control system
European Patent Office | 2017
|LOW-PRESSURE BLEED AIR AIRCRAFT ENVIRONMENTAL CONTROL SYSTEM
European Patent Office | 2015
|