Abstract: Systems and methods are configured for power distribution in a hybrid fixed-wing VTOL drone aircraft. A drone aircraft includes two modes of operation. In a first mode of operation, the internal combustion engine is shut off while an electric motor-based VTOL system provides lift and thrust. In a second mode of operation, an internal combustion engine provides thrust while a set of fixed wings provide lift. In the second mode of operation, mechanical power from the internal combustion engine provides for power generation to charge an electrical battery to power the electric motor-based VTOL system.

Abstract: Systems and methods for power distribution in a hybrid fixed-wing VTOL drone aircraft are disclosed. In an embodiment, a drone aircraft is capable of two modes of operation. In a first mode of operation, the internal combustion engine is shut off while an electric motor-based VTOL system provides lift and thrust. In a second mode of operation, an internal combustion engine provides thrust while a set of fixed wings provide lift. In the second mode of operation, mechanical power from the internal combustion engine provides for power generation to charge an electrical battery to power the electric motor-based VTOL system.

Abstract: Systems and methods for power distribution in a hybrid fixed-wing VTOL drone aircraft are disclosed. In an embodiment, a drone aircraft is capable of two modes of operation. In a first mode of operation, the internal combustion engine is shut off while an electric motor-based VTOL system provides lift and thrust. In a second mode of operation, an internal combustion engine provides thrust while a set of fixed wings provide lift. In the second mode of operation, mechanical power from the internal combustion engine provides for power generation to charge an electrical battery to power the electric motor-based VTOL system.

Abstract: A payload apparatus for selectively releasing a payload is disclosed. The payload apparatus may be used to deliver payloads from an aircraft such as an unmanned aerial vehicle. Embodiments of the payload apparatus include a payload container and a matching lid. The payload container may include one or more latches configured to engage the lid, and the lid may include one or more actuators to selectively disengage the one or more latches, thus releasing the payload container.

Abstract: A payload apparatus for selectively releasing a payload is disclosed. The payload apparatus may be used to deliver payloads from an aircraft such as an unmanned aerial vehicle. Embodiments of the payload apparatus include a payload container and a matching lid. The payload container may include one or more latches configured to engage the lid, and the lid may include one or more actuators to selectively disengage the one or more latches, thus releasing the payload container.