QUADROLET

Claims

1. A quadcopter, an aircraft-type aircraft with vertical or shallow takeoff and landing, including an aircraft, a quadcopter and an on-board charger, characterized in that the aircraft is designed with a forward-swept wing, in the root section of which, at a positive angle of attack, in autorotation mode, fans (low-pressure compressors) of the quadcopter are built in, the blades of which have a positive twist in the section that creates lift for vertical takeoff and landing, and a negative twist in the section in the gap of the volute with a flat jet nozzle, with variable geometry, generating thrust for forward motion and maneuvering.

2. A quadcopter according to paragraph 1, including an on-board charging device generator, characterized in that the generator is interlocked with a hydraulic turbine, compressed air cylinders and tanks with antifreeze liquid, with the ability to squeeze liquid onto the hydraulic turbine and return the used liquid to a free tank for repeated (multiple) use.

3. A quadcopter according to paragraph 1 (option 2), characterized in that the on-board charging device is designed as a hybrid power plant based on electric motors and hydrogen fuel cells, which allows for energy recovery during descent and braking.

4. A quadcopter according to paragraph 1, characterized in that the control system is supplemented with AI stabilization algorithms and sensors (LiDAR, computer vision) to improve safety and precise positioning of the aircraft.

5. A quadcopter according to paragraph 1, characterized in that its design is modular, with the possibility of quickly replacing fan units, wing fragments and power plant elements, as well as with redundant control systems and an emergency landing system.