A water extractor for an environmental control system of an aircraft includes a water extraction vessel arranged in fluid communication with the separation mechanism. The water extraction vessel includes a first portion for receiving a first airstream and a second portion for receiving a second airstream. A stationary diffuser is mounted within the second portion.
Vented dynamic pressure recovery module for aircraft ECS
2020-08-18
Patent
Electronic Resource
English
VENTED DYNAMIC PRESSURE RECOVERY MODULE FOR AIRCRAFT ECS
European Patent Office | 2019
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