FLYING WING VERTICAL TAKE-OFF AND LANDING AIRCRAFT

Smart overview of the Invention

A novel vertical take-off and landing (VTOL) aircraft design incorporates a flying wing structure, integrating components into a single blended wing to enhance efficiency. The aircraft features a passenger compartment and utilizes multiple rotors for lift and propulsion. This configuration aims to reduce weight and drag compared to traditional fixed-wing VTOL designs, which often include separate fuselage, wing, and tail components.

The aircraft's rotor system includes two sets: a forward set with at least four rotors and a rearward set with at least two rotors. These rotors can be configured to tilt between providing vertical lift for take-off and landing and forward thrust for cruising. The design emphasizes flexibility, allowing some or all rotors to tilt, which enhances control and potentially reduces the aircraft's overall weight and drag.

Designed with passenger comfort in mind, the compartment allows passengers to face forward during critical phases of flight. The innovative flying wing design not only improves aerodynamics but also minimizes the ground footprint of the aircraft. This makes it more suitable for urban environments where space is limited.

In some configurations, the aircraft employs a control system that independently adjusts rotor tilt, offering enhanced maneuverability and redundancy. This capability is particularly useful for generating yawing moments necessary for precise flight control. The aircraft's design may include additional features such as winglets and electrically powered systems, contributing to its modern, efficient operation.

The patent outlines various embodiments of the aircraft, including different rotor counts and configurations. These variations provide flexibility in design, allowing for optimization based on specific operational needs. By integrating the passenger compartment and power systems into the wing structure, the design further reduces unnecessary weight and improves overall performance.