Aircraft with fused canard layout

Abstract

The invention discloses an aircraft with a fused canard layout, and particularly relates to the field of aircraft starting design. Comprising an aircraft with a pair of canards, and the pair of canards are symmetrically arranged on the front portion of a fuselage of the aircraft and rotationally connected with the fuselage of the aircraft. By the adoption of the technical scheme, the problem that an existing flying wing aircraft cannot give consideration to the aerodynamic performance and the stealth performance at the same time is solved, and the aerodynamic performance and the stealth performance of the aircraft can be both considered.

Description

technical field [0001] The invention relates to the field of aircraft start-up design, in particular to an aircraft with a fusion canard layout. Background technique [0002] Compared with the traditional aircraft, the flying-wing layout aircraft cancels the horizontal tail and vertical tail design, so it is lighter in weight, lower in resistance, and has a higher lift-to-drag ratio and better stealth performance. Therefore, the flying wing layout is an important development trend of future fighter jets. However, since the control surface of the flying-wing aircraft is mainly located at the trailing edge of the wing, the moment arm is short, which leads to the weak control ability of the control surface of the aircraft with the flying-wing configuration. If you want to get the pitch control effect equivalent to the conventional layout, you need to pay more lift loss. [0003] In view of the problems existing in the flying wing layout aircraft, the canard flying wing layout...

AI Technical Summary

Problems solved by technology

[0004] The present invention intends to provide an aircraft with integrated canard layout, which solves the problem that the existing flying wing layout aircraft cannot take into account both aerodynamic performance and stealth performance

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