The present application discloses an aircraft configured for vertical take-off and landing and horizontal flight. The aircraft includes a valve configured to control the permitting or restricting of a release of gas from different regions of a fuel tank when the aircraft is in a vertical take-off and landing orientation and when the aircraft is in a horizontal flight orientation.
FUEL VENTING FOR VERTICAL TAKE-OFF DUAL-ENGINE AIRCRAFT
2025-03-13
Patent
Electronic Resource
English
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