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
18.08.2020
Patent
Elektronische Ressource
Englisch
VENTED DYNAMIC PRESSURE RECOVERY MODULE FOR AIRCRAFT ECS
Europäisches Patentamt | 2019
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