Low-speed aircraft capable of vertically taking off and landing

Abstract

The invention discloses a low-speed aircraft capable of vertically taking off and landing, and the aircraft is a small high efficiency aircraft capable of vertically taking off and landing based on 2032cjc wing section. The structure is composed of wings, ailerons, engine mounting seats, square carbon rods, round carbon rods, a loading cylinder, a landing gear structure and an aircraft electroniccontrol circuit. In structural design, a rectangular large-wing-surface aero-pneumatic layout is adopted for the aircraft and can ensure that the aircraft has a larger lifting force source in the process of ultra-low-speed heavy-load cruising flight so as to ensure the stability of the heavy-load flight. The main structure of an airframe is a wooden airframe and the loading cylinder formed by combining carbon fiber boards and carbon fiber pipes, the control circuit is integrally installed on the middle carbon fiber board of the airframe, the stability of a low-speed heavy-load cruising stagecan be greatly enhanced through the rectangular large-wing-surface aero-pneumatic layout design of the aircraft, the mission efficiency of the aircraft can be effectively improved, and the aircraft has good maneuverability when flying at a low speed.

Description

technical field [0001] The invention relates to the field of aviation aircraft, in particular to the design of the aerodynamic shape and the integrated system of the aircraft. Background technique [0002] The so-called aviation aircraft is a kind of flying machine that can realize complex aerial movements based on flight principles and relying on aerodynamic shape, such as the civil aviation aircraft we usually travel on, the individual drones in the military field, etc., all belong to the field of aviation aircraft. The present invention mainly belongs to the category of small aircrafts. In many small aviation aircrafts today, one or more of the following disadvantages exist: most aircraft models need to take off and land by means of runways; aircraft with slow speeds do not have large load capacity Specific capacity; not suitable for low-speed and high-maneuvering flight; the structure of the model aircraft is not light enough, and the endurance performance is average. T...

AI Technical Summary

Problems solved by technology

[0003] The technical problem that the present invention mainly solves is to provide a kind of slow vertical take-off and landing aircraft, which can solve 1. the difficulty of vertically stable take-off and landing of small aircraft, 2. the characteristics of weak material carrying capacity of small aircraft, 3. The endurance performance of small aircraft is generally too low in efficiency, 4. The problem of difficult control of small vertical take-off and landing aircraft at slow speed

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