Brennstoffüberführungssystem für Luftfahrzeug

Parallel transfer pumps (92,94) operate to transfer fuel from auxiliary tanks (52,60,66) to the main tank (10). A pressure sensor (106) in the pump discharge line in combination with tank level rate means (86,88,90) sequences pumps (92,92) and transfer valves (100,102) if required, and confirms succ...

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Bibliographic Details
Main Authors SECCHIAROLI, LAWRENCE N., STATFORD CONNECTICUT 06497, US, WILSON, THOMAS P., TRUMBULL CONNECTICUT 06611, US, CRESISKI, RAYMOND C., JR., MILFORD CONNECTICUT 06460, US
Format Patent
LanguageGerman
Published 11.05.1994
Edition5
Subjects
AEROPLANES
AIR INTAKES FOR JET-PROPULSION PLANTS
AIRCRAFT
ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT
AVIATION
BLASTING
COMBUSTION ENGINES
CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
COSMONAUTICS
EQUIPMENT FOR FITTING IN OR TO AIRCRAFT
FLYING SUITS
GAS-TURBINE PLANTS
HEATING
HELICOPTERS
HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
LIGHTING
MECHANICAL ENGINEERING
PARACHUTES
PERFORMING OPERATIONS
TRANSPORTING
WEAPONS
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Summary:Parallel transfer pumps (92,94) operate to transfer fuel from auxiliary tanks (52,60,66) to the main tank (10). A pressure sensor (106) in the pump discharge line in combination with tank level rate means (86,88,90) sequences pumps (92,92) and transfer valves (100,102) if required, and confirms successful transfer or alarms when unsuccessful.
Bibliography:Application Number: DE19896013032T