发明申请
US20140027575A1 FUEL TRANSFER SYSTEM CONTROLLED BY FLOAT VALVES 有权
燃油转运系统由浮阀控制

FUEL TRANSFER SYSTEM CONTROLLED BY FLOAT VALVES
摘要:
A fuel transfer system for an aircraft includes an upper tank, a lower tank, a fuel transfer line connecting the upper tank to the lower tank, an upper fuel transfer line outlet in the lower tank, a lower fuel transfer line outlet in the lower tank, an upper float valve associated with the upper fuel transfer line outlet, and a lower float valve associated with the lower fuel transfer line outlet. The upper fuel transfer line outlet, which is in the lower tank, is in fluid communication with the upper tank. The lower fuel transfer line outlet, which is located in the lower tank, is in fluid communication with the upper tank.
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