Thermally actuated passive gas turbine engine compartment venting

A thermally actuated venting system includes a thermally actuated vent for opening a vent outlet in a gas turbine engine associated compartment with a passive thermal actuator located in the compartment based on a temperature of the compartment. Outlet may be located at or near a top of a core engin...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: DIAZ CARLOS ENRIQUE, LABORIE DANIEL JEAN-LOUIS, GEARY STEPHEN DENNIS
Format: Patent
Sprache:eng
Schlagworte:
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