An aircraft includes an engine, a fuel tank, a chamber, a system, and an introduction line. The chamber is located in the tank, occupies only a part of the tank, and includes a sensor for measuring a property of the fuel. The system injects fuel into the line. The introduction line introduces fuel from the injection system into the chamber. The introduction line includes a valve capable of preventing an introduction of fuel from the injection system into the chamber via the line.
AIRCRAFT COMPRISING, IN ITS FUEL TANK, A CHAMBER PROVIDED WITH A SENSOR
2023-06-29
Patent
Elektronische Ressource
Englisch
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