Bidirectional fuel supply balance system and correction method for fuel tanks in left and right wings of aircraft

The invention relates to a bidirectional fule supply balance system for fuel tanks in left and right wings of an aircraft, the system comprises a left fuel tank breather pipe, a left stamping air inlet pipe, a right fuel tank breather pipe, a right stamping air inlet pipe, a fuel tank pressure balan...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	XIONG GUIBI, LI XIAOGANG, SUN BAIFENG, LUO HAITAO
Format:	Patent
Sprache:	chi ; 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
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