AERONEXT INC.

A flying vehicle with a flight part connected to a plurality of rotor wing parts and a main wing, wherein the main wing is configured such that the lift produced by the main wing during landing is reduced compared to the lift produced by the main wing during cruising. Furthermore, the main wing is fixed at a forward tilt with respect to the flight part. Furthermore, the rotor wing is connected at an angle that produces propulsion and lift during cruise. Furthermore, the rotor blades are connected at an angle that generates propulsive force during cruise.

A moving body that can be transported in a state to stabilize the posture of the transport object, without affecting the transport object due to the inclination of the moving body when moving forward. A moving body comprising a holding mechanism that has a rotation unit that rotates in the pitch direction, and approximately horizontally holds an object to be transported from the side near the center of gravity of a transport unit capable of storage or above the center of gravity. Further, a moving body wherein the holding mechanism has a uniaxial rotation unit that rotates only in the pitch direction. Further, a moving body wherein the holding mechanism approximately horizontally holds the transport unit by active control. Alternatively, the holding mechanism approximately horizontally holds the transport unit by passive control.

The invention is a flying object equipped with a loading part holding a delivery payload, and the loading part or the delivery payload is attached to an airframe so that the loading part or the delivery payload is tilted backward in the forward and backward direction in a landing state or hovering state. The loading part or delivery payload is attached to the airframe so that the loading part or delivery payload is substantially horizontal during cruising.

An aircraft that can improve cruising speed by making the body shape of the airframe (especially, multicopter) into a shape that has less unnecessary positive lift force by the main body and less drag in the cruising posture of the airframe. An aircraft equipped with a plurality of rotary blades including a propeller and a motor, wherein the aircraft comprises a main body with an inverted airfoil shape. The main body has an attack angle that does not generate a lift force or produces a negative lift force during cruising. The main body has a positive attack angle of 12 degrees or less. Further, it is provided with a mounting unit on which a mounted object can be mounted. The mounting unit is connected to the main body via the connection unit.

An information processing system includes: an acquisition unit that acquires schedule information regarding a travel schedule of a recipient who receives a package; and a designation unit that designates, based on the schedule information, a delivery slot corresponding to a scheduled time at which the recipient arrives at a receiving location of the package among a plurality of delivery slots included in a delivery plan of a mobile body used for delivery of the package.

An information processing system includes a notification unit that notifies a recipient who receives a package, of reference information regarding a package of another recipient corresponding to registration information that is registered in advance by the recipient.

An information processing system includes: a communication unit that notifies a service provider terminal used by a candidate for a service provider being a provider of a service of collection and transportation of a package and estimated to be capable of providing a service of collection and transportation of the package in accordance with a condition on collection and transportation of the package by another different transportation means, of an offer for the service, a control unit that approves the service provider candidate as the service provider, and a screen generation unit that generates notification of information on the service of collection and transportation of the package.

To stabilize a frame of a flight body, a frame assembly for a flying body includes a first frame member extending in at least two parallel and first directions, a second frame member extending in a second direction perpendicular to said first direction, and a fixing member fixed to each of the first and second frame members, wherein at least one of the fixing members has an opening.

The invention is a flying object equipped with a loading part holding a delivery payload, and the loading part or the delivery payload is attached to an airframe so that the loading part or the delivery payload is tilted backward in the forward and backward direction in a landing state or hovering state. The loading part or delivery payload is attached to the airframe so that the loading part or delivery payload is substantially horizontal during cruising.

A flight vehicle capable of improving the accuracy of the arrival position of baggage. The flight vehicle according to the present disclosure includes a mounting unit that holds a mounted object, holds the mounting unit via a string member, and has a moving means including a rotor blade provided between the upper end and the lower end of the mounting unit, when the mounting unit is viewed from the side.