Bleed valve system for a gas turbine engine

The present invention relates to a bleed valve for tapping or bleeding a portion of air from a gas turbine engine, and more particularly to a poppet for a bleed valve which provides regulated air flow to an aircraft environmental system. A bleed valve assembly includes a valve poppet having a bleed...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: Winslow, Christopher L, Anduze, Alejandro
Format: Patent
Sprache:eng
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