Fuel level control system and method
AssigneeAmerican Honda Motor Co., Inc.
InventorsTimothy J. DOYLE, William E. GORGEN, Paul R. WOODCOCK
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AssigneeAmerican Honda Motor Co., Inc.
InventorsTimothy J. DOYLE, William E. GORGEN, Paul R. WOODCOCK
Estimating the term…
A fuel level control system and method for an aircraft to passively control the movement of fuel center of gravity during the fuel consumption sequence includes an upper tank for storing fuel, a lower tank for storing fuel, wherein the lower tank is disposed below the upper tank, and a fuel transfer line connecting the upper tank to the lower tank. The control system further includes an upper fuel transfer line outlet in the lower tank and a lower fuel transfer line outlet in the lower tank. The upper fuel transfer line outlet and the lower fuel transfer line outlet are in fluid communication with the upper tank via the fuel transfer line. An upper line outlet valve is associated with the upper fuel transfer line outlet for opening and closing the upper fuel transfer line outlet. A lower line outlet valve is associated with the lower fuel transfer line outlet for opening and closing the lower fuel transfer line outlet. The fuel level control system further includes a control shutoff valve disposed on the fuel transfer line for selectively limiting flow through the fuel transfer line.
A fuel level control system for an aircraft, comprising:
An aircraft fuel level control system, comprising:
A fuel level control method for an aircraft, comprising:
Dependencies are inferred from the claim text.