A system for supplying pressurised air installed in an aircraft turbine engine, configured to supply pressurisation air to a portion of the aircraft for using compressed air from pressurisation air collected from a portion for collecting compressed air, characterised in that it comprises a collection port formed on a casing of the compressed air collection portion, a collection member coupled to the collection port, a through port of the collection member formed on a casing of a compartment of the turbine engine, said casing being subjected to small movements relative to the casing of the compressed air portion, the collection member crossing the through port with a freedom of movement relative to the latter during said small movements, a high-pressure space crossed by the collection member, located between the casing of the compressed air collection portion and the casing of the compartment.
SYSTEM FOR SUPPLYING PRESSURISED AIR INSTALLED IN AN AIRCRAFT TURBINE ENGINE INCLUDING SEALING MEANS
2017-07-20
Patent
Elektronische Ressource
Englisch
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