Rudderless aircraft with independent air supply

Abstract

The invention provides a rudderless aircraft supplied by an independent air source, the basic configuration is a fixed-wing aircraft with a canard layout, including a fuselage, a main wing, a canard, a push-back power unit, a propeller, and a winglet 1. The main landing gear and the front landing gear rely on a set of circulation control device to replace the traditional rudder surface, which has a simple structure and is easy to maintain. And because the conventional rudder surface is canceled, the original sharp edges, openings and bosses on the wing surface will disappear, which will reduce the radar scattering area of ​​the aircraft and improve the stealth of the aircraft.

Description

technical field [0001] The invention relates to the field of aviation machinery, in particular to a rudderless aircraft supplied with air from an independent air source. Background technique [0002] The effective steering control produced by the control surfaces of the aircraft, so that it can carry out stable flight. However, the traditional rudder surface has many defects, such as complex structure, cumbersome maintenance, increased flight resistance and reduced stealth. Excellent aerodynamic performance, long range, long endurance and high stealth are important indicators in the design of next-generation aircraft. Traditional circulation control technology often provides air source for the device from engine bleed air, which will affect the power output of the engine. Contents of the invention [0003] In order to solve the problems of the prior art, the present invention provides an aircraft without rudder surfaces supplied by an independent air source, which replac...

AI Technical Summary

Problems solved by technology

Traditional circulation control technology often uses bleed air from the engine to provide air source for the device, which will affect the power output of the engine

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