MIXING BLEED AND RAM AIR USING A DUAL USE TURBINE SYSTEM

An airplane is provided. The airplane includes a pressurized volume and an air conditioning system. The air conditioning system includes a compressor (312) configured to receive a flow of a first medium, a turbine (313) downstream of the compressor in a flow path of the first medium, a first valve (...

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Bibliographic Details
Main Authors BRUNO, Louis J, HIPSKY, Harold W
Format Patent
LanguageEnglish
French
German
Published 06.05.2020
Subjects
AIRCRAFT
ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT
AVIATION
COSMONAUTICS
EQUIPMENT FOR FITTING IN OR TO AIRCRAFT
FLYING SUITS
PARACHUTES
PERFORMING OPERATIONS
TRANSPORTING
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Summary:An airplane is provided. The airplane includes a pressurized volume and an air conditioning system. The air conditioning system includes a compressor (312) configured to receive a flow of a first medium, a turbine (313) downstream of the compressor in a flow path of the first medium, a first valve (V1) that diverts the flow of the first medium around the turbine, a second valve (V2) that provides a second medium to the turbine, and a third valve (V3) downstream of the turbine that directs an outlet flow of the turbine towards the pressurized volume and that directs the outlet flow of the turbine away from the pressurized volume.
Bibliography:Application Number: EP20170172834