SYSTEM AND METHOD FOR LOADING AND SECURING PAYLOAD IN AN AIRCRAFT
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United States of America
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Issued Date -
Jun 30, 2022
app pub date -
Dec 30, 2020
filing date -
Dec 30, 2020
priority date (Note) -
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Abstract
In an aspect a system for loading and securing a payload in an electrical vertical take-off and landing (eVTOL) aircraft may comprise a fuselage further comprising structural elements configured to provide physical support for the aircraft fuselage. An eVTOL aircraft may also comprise a swing nose, where a portion of the nose of the aircraft may swing on a hinge in a radial direction orthogonal to the longitudinal axis of the aircraft. The hinge may be coupled to at least a portion of the fuselage and at least a portion of the nose of the aircraft. A latching mechanism may be configured to secure a payload in an aircraft fuselage. A conveyor mechanism may be configured to transport a payload into the fuselage from the opening of the aircraft.
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