Tilt-rotor fixed wing aircraft with vertical take-off and landing function

Abstract

The invention relates to a tilt-rotor fixed wing aircraft with a vertical take-off and landing function. The tilt-rotor fixed wing aircraft comprises an aircraft body, wings and a tail, wherein the wings and the tail are mounted on the aircraft body. Pitching and tilting power devices are arranged on the left side and the right side of the aircraft body. A front landing gear and a main landing gear are arranged at the bottom of the aircraft body. An equipment hatch is arranged on the upper portion of the aircraft body, and an aviation telemetering camera is arranged in an equipment cabin. A control cabin hatch is arranged on the upper portion of the aircraft body, and a control device is arranged in a control cabin. A reverse-torsional balance power device is arranged on the rear portion of the aircraft body. The wings are mounted on the two sides of the aircraft body and provided with wing control planes. The tail is connected with the aircraft body through tail supporting rods and comprises a horizontal tail, a pitching control plane, a vertical tail and a yaw control plane. The tilt-rotor fixed wing aircraft has the advantages that the vertical take-off and landing, tilting and level flight of the aircraft can be achieved through one power system, take-off and landing of an unmanned aerial vehicle are not limited by fields, the structural weight can be better reduced, the aircraft can fly more stably, the flying time is longer, operation is simpler, and the flying process is more intelligent.

Description

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AI Technical Summary

Benefits of technology

This patented design allows for efficient takeoff and landings on drones without requiring expensive equipment or heavy structures at their destination. It also saves space while still providing stability during high altitude flights. Additionally, it uses advanced technologies like carbon fibers frames (CF) made from polyimide resin impregnated into molded plastic sheets instead of traditional materials such as aluminum alloys due to its lightweight properties compared to other options. Overall, these technical improvements make dronies highly versatile and cost-effective.

Problems solved by technology

The technical problem addressed in this patented text relates to how complex an airborne vehicle's structures are designed for carrying passengers during flight operations due to environmental factors such as altitude changes or wind conditions that affect its ability to lift heavy loads effectively without reducing their lifespan.

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