An aircraft pressurization system, includes an auxiliary compressor (42) for further compressing compressed air received from a low pressure compressor section (22) of a gas turbine engine (10) while the compressed air is below a predetermined pressure level; a bleed passage (40) for fluidically connecting the auxiliary compressor (42) to the low pressure compressor section (22); and an environmental control system (38) coupled to an output of the auxiliary compressor (42) for conditioning the compressed air to a predetermined level.
Low pressure compressor bleed exit for an aircraft pressurization system
Entlüftungsausgang eines Niedrigdruckkompressors für ein Flugzeugdruckregelanlage
Sortie de purge d'un compresseur basse pression pour un système de pressurisation d'un avion
2015-11-04
Patent
Electronic Resource
English
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