AIRCRAFT FUEL SYSTEM WITH REMOVABLE FUEL TANK

AIRCRAFT FUEL SYSTEM WITH REMOVABLE FUEL TANK

The aircraft powerplant (22) includes an injector (74) and a fuel system (100) configured to deliver fuel to the injector (74). The fuel system (100) includes a first tank (114), a first circuit (106) and a second circuit (108) arranged in parallel with the first circuit (106) between the first tank...

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Hauptverfasser: KRAMER, Stephen K, BOARDMAN, Gregory
Format: Patent
Sprache:eng ; fre ; ger
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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creator KRAMER, Stephen K
BOARDMAN, Gregory
description The aircraft powerplant (22) includes an injector (74) and a fuel system (100) configured to deliver fuel to the injector (74). The fuel system (100) includes a first tank (114), a first circuit (106) and a second circuit (108) arranged in parallel with the first circuit (106) between the first tank (114) and the injector (74). The second circuit (108) includes a second tank. The fuel is directed from the first tank (114) to the injector (74) during a first mode through the first circuit (106) and independent of the second circuit (108). The fuel is directed from the second tank to the injector (74) during a second mode through the second circuit (108) and independent of the first circuit (106).
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language eng ; fre ; ger
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subjects 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
title AIRCRAFT FUEL SYSTEM WITH REMOVABLE FUEL TANK
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