System for supplying pressured air installed in an aircraft turbine engine including sealing means
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United States of America Patent
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Jun 12, 2018
Issued Date -
Jul 20, 2017
app pub date -
Jul 22, 2015
filing date -
Jul 25, 2014
priority date (Note) -
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Abstract
A system for supplying pressurized air installed in an aircraft turbine engine, configured to supply pressurization air to a portion of the aircraft for using compressed air from pressurization air collected from a portion for collecting compressed air, characterized 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.
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