Release system for evacuation slide assembly

A release system for an evacuation slide assembly of an aircraft includes a fluid delivery manifold, a first actuator, and a second actuator. In various embodiments, a fluid is configured to flow into and pressurize the fluid delivery manifold from a fluid source in response to an evacuation event....

Ausführliche Beschreibung

Gespeichert in:

Bibliographische Detailangaben
Hauptverfasser:	Schmidt, Ryan, Rautenbach, Helperus Ritzema
Format:	Patent
Sprache:	eng
Schlagworte:	AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION COSMONAUTICS EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS PARACHUTES PERFORMING OPERATIONS TRANSPORTING
Online-Zugang:	Volltext bestellen
Tags:	Tag hinzufügen Keine Tags, Fügen Sie den ersten Tag hinzu!

Beschreibung
Zusammenfassung:	A release system for an evacuation slide assembly of an aircraft includes a fluid delivery manifold, a first actuator, and a second actuator. In various embodiments, a fluid is configured to flow into and pressurize the fluid delivery manifold from a fluid source in response to an evacuation event. In various embodiments, the first actuator is fluidly coupled to the fluid delivery manifold, wherein the first actuator is configured to release a blowout panel of the evacuation slide assembly in response to the fluid pressurizing the fluid delivery manifold. In various embodiments, the second actuator is fluidly coupled to the fluid delivery manifold, wherein the second actuator is configured to release a soft cover of the evacuation slide assembly in response to the fluid pressurizing the fluid delivery manifold.