Flight vehicle and flight vehicle system with power receiving coil provided on or in landing portion of leg

A flight vehicle comprising:

• a driver to rotate a rotor blade about a rotation axis;
• a battery that is chargeable and dischargeable and operable to supply power to the driver;
• a main body that accommodates the battery;
• a leg to support the main body during landing;
• a power receiving coil with an annular shape and electrically connected to the battery;
• a luggage room capable of housing a transported object;
• a door through which the transported object is capable of passing, the door being openable and closable and located on a lower surface of the luggage room;
• and
• a controller configured or programmed to control opening and closing of the door;
• wherein
• the leg includes a landing portion to contact a landing surface during landing;
• a central axis of the power receiving coil extends parallel or substantially parallel to an axial direction of the flight vehicle;
• the power receiving coil is located on or in the landing portion;
• and
• an area inside the annular shape of the power receiving coil is larger than a total area of the luggage room.