Upright-standing vertical take-off and landing airplane

Abstract

An upright-standing vertical take-off and landing airplane is designed to solve the technical problems that much difficulty exists in controlling the vertical take-off and landing, hovering and the like of a conventional horizontal vertical take-off and landing airplane, the required cost is relatively higher and the controlling force is insufficient when the airplane uses a pneumatic control plane in the low-speed and idle states in the air. An upright-standing main body is adopted, a jet vane is taken as an airplane control plane, and an engine jet orifice corresponds to the center of the jet vane behind an X-type tail wing in position. The invention has the benefits that the upright-standing vertical take-off and landing airplane is a high-speed aircraft adopting an upright-standing machine body and having the design characteristic that the machine body is fused with a guided missile; owing to the upright take-off, the efficiency of an engine per se can be given into full play and the steering and balancing designs are simplified; the maneuverability is more excellent than that of the conventional layout; the controllability is good and the maneuverability is outstanding; and the airplane on the ground for taking off occupies a small area so as to facilitate hiding.

Description

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AI Technical Summary

Benefits of technology

This patented technology allows for an improved flying vehicle (Flying Aircraft) called Vertecon). It has several technical advantages over traditional piloted vehicles such as helicopters or torsadeers due to their ability to maintain stable flight without rewinding them after takeoff. They also have wings made from multiple small blades connected by diagonal lines instead of just one big blade. These improvements allow for more efficient operation while still being able to perform various tasks like taking turns on level ground surfaces safely.

Problems solved by technology

This patented describes how current methods for lifting an airplane can only use its own propulsive force without being able to make up any extra effort or costs more than necessary due to their inability to actively work with external forces like jet fuel injection systems that are needed during flight operations.

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