The project was dedicated to developing the concept of a promising aircraft with vertical takeoff and landing, combining the advantages of an airplane and a multicopter.
The work began with the study of various architectures of the device and the search for the most rational layout. In the early stages, dozens of sketches were created, differing in the location of the power plant, the configuration of the wing, the shape of the fuselage and the general aerodynamic scheme. After analyzing the options, together with the customer's engineers, the most promising solutions were selected for further study.
During the development process, the industrial design was constantly adjusted to take into account aerodynamic requirements, alignment, power plant features and production adaptability. This iterative process made it possible to combine engineering requirements with the modern appearance of the aircraft.
Conceptual renderings and demonstration materials were prepared for the presentation of the project, illustrating the appearance of the device and various application options. The project became an example of a complex work in which industrial design developed in parallel with engineering research.
Project Features
- study of several aerodynamic schemes;
- development of alternative layouts;
- search for optimal aircraft architecture;
- collaboration of designers and engineers;
- adaptation of the design to engineering constraints;
- conceptual visualization of a promising product;
- iterative development from the sketch to the final concept.
Project result
A series of concepts for an aircraft with vertical takeoff and landing have been developed, reflecting various options for the layout and architecture of the product. As a result of the joint work with the engineering team, the final concept was formed, combining the requirements of aerodynamics, manufacturability and industrial design.
