Jet Vertical Lift Pneumatic System

Abstract

The present invention relates to a jet-type vertical lift aerodynamic system, which includes a body with upper and lower hatches, an engine, and two power assemblies respectively arranged on the left and right wings. When the engine is in a raised or lowered state due to the pivoting angle, the propeller assembly can be pushed out of the pipe body by means of the two power components and pivoted to make it perpendicular to the body, so that the body can be raised vertically or vertically by adjusting the deflection angle or rotational speed of the propeller assembly. It can be in a balanced state when landing, and then achieve the purpose of vertical lifting.

Description

Technical field [0001] The present invention relates to a jet whispered pneumatic system, especially for the flight carrier. Background technique [0002] Generally, the flight carrier is roughly divided into fixed-wing aircraft and rotor aircraft (eg helicopters or rotor), and fixed-wing flying machines are mainly given to advancement of the power unit. Above the air pressure difference from the airfoil and the airflow impact effect of the airflow, therefore, the flight speed is fast, the amount of load is high, but the fixed-wing flight machine needs the runway to take off and land, so the land floor is limited sex. The rotor helicopter generates rising power with the engine drives the rotating wings, so it can be vertically rising in small area venues, and can be flying at low altitude, but the helicopter is short, slow speed, and is affected by the weather. In addition, the rotor machine rotates the rotor with a relative airflow to generate the rotor, and therefore, the take-...

AI Technical Summary

Problems solved by technology

[0002] General flying vehicles can be roughly divided into fixed-wing aircraft and rotary-wing aircraft (such as helicopters or rotorcraft) according to different flight principles and functions. The air pressure difference above and below the wing and the impact effect of the airflow generate lift. Therefore, the flight speed is fast, the carrying capacity is large, and the flight efficiency is high. However, the fixed-wing aircraft needs a runway to provide take-off and landing, so the take-off and landing space is limited. sex

The rotary-wing helicopter relies on the engine to drive the rotor to rotate to generate upward power. Therefore, it can vertically ascend and descend on a small-area site, and can fly at low altitude and low speed. However, the helicopter has a short range, slow speed, and is greatly affected by the weather.

In addition, the rotorcraft relies on the forward relative airflow to make the rotor rotate and generate lift. Therefore, the takeoff and landing distance is short and it can fly at low speed and low altitude, so its flight speed and efficiency are far inferior to those of fixed-wing aircraft.

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