AIRCRAFT PNEUMATIC SYSTEM

ABSTRACT An aircraft pneumatic system including a pneumatic actuator arranged to operate at a pressure value at least equal to a pressure threshold, a line fluidly connected between a pneumatic source and the pneumatic actuator, and a venturi disposed upstream of the line and downstream of the pneum...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: OLVER, BRYAN WILLIAM, ALECU, DANIEL, STINA, NICK
Format: Patent
Sprache:eng ; fre
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