Zero minusg fuel feeding turbocharging system in aircraft

The utility model relates to an aircraft fuel feeding turbocharging system technical field, more specifically relate to a zero minusg fuel feeding turbocharging system in aircraft to make fuel oil system satisfy the fuel feeding requirement under the zero minusg state. The utility model discloses a...

Ausführliche Beschreibung

Gespeichert in:

Bibliographische Detailangaben
Hauptverfasser:	ZHUANG QUAN, SHAN YUWEI, DING ENLIANG, LI ZHENGHONG, LIU JING
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:	The utility model relates to an aircraft fuel feeding turbocharging system technical field, more specifically relate to a zero minusg fuel feeding turbocharging system in aircraft to make fuel oil system satisfy the fuel feeding requirement under the zero minusg state. The utility model discloses a zero minusg fuel feeding turbocharging system in aircraft, gas cylinder can be through device corresponding on pressure boost pipeline and the pressure boost pipeline and pressure accumulation oil tank intercommunications, can be in that the engine bleed be gaseous possibly can't satisfy the required pressure boost gas of pressure accumulation oil tank fuel feeding and require the time, provide pressure boost gas for the pressure accumulation oil tank for fuel oil system satisfies the fuel feeding requirement under the zero minusg state, simple structure, and with low costs and the pressure boost is efficient