Integrated type frame light aircraft

Abstract

The invention relates to an integrated type frame light aircraft. A fuselage, a nose, a tail and wings are included; the aircraft comprises an integrated type frame which comprises a nose and tail frame, a wing frame / at least one of the nose and tail frame and the wing frame, and a fuselage frame; a plurality of main steel ropes are wound on the outer side of the integrated type frame, and form asupporting network surface on the outer side of the integrated type frame, and the supporting network surface is provided with an outer protective layer of a flexible material; and a cabin body is formed in the wing frame. The integrated type frame light aircraft is convenient to manufacture, and a traditional airplane riveting welding type complex manufacturing process is changed; an airplane issmall in weight, and except the frame, the airplane basically does not need a metal material, so that use of metal is reduced in a large scale; the wings are provided with storage spaces, so that thegoods carrying capacity of the airplane is improved; and radar preventing is achieved, the outer protective layer is on the outer layer of the airplane, a nonmetallic material is adopted, radar preventing is effective, and the integrated type frame light aircraft is applicable to a military aircraft.

Description

technical field [0001] The invention relates to the technical field of aircraft, in particular to an integrated frame lightweight aircraft. Background technique [0002] In the existing aircraft manufacturing process, the wing and the fuselage cannot be integrated, and in the existing aircraft, the wing, as an important part of the aircraft, occupies a large space, but the flat design of the wing makes it difficult to There is storage space, but the cabin space of the aircraft is limited, resulting in a small storage space of the aircraft, which cannot maximize the storage capacity of the aircraft. [0003] In addition, the existing aircraft construction is made of metal frames and metal materials. The quality of the aircraft is large, the production is difficult, and the production cost is high. How to reduce the weight of the aircraft and reduce the production cost has become a difficult problem for technicians. Contents of the invention [0004] The technical problem t...

AI Technical Summary

Problems solved by technology

[0002] In the existing aircraft manufacturing process, the wing and the fuselage cannot be integrated, and in the existing aircraft, the wing, as an important part of the aircraft, occupies a large space, but the flat design of the wing makes it difficult to There is storage space, but the cabin space of the aircraft is limited, resulting in a small storage space of the aircraft, which cannot maximize the storage capacity of the aircraft

[0003] In addition, the existing aircraft construction is made of metal frames and metal materials. The quality of the aircraft is large, the production is difficult, and the production cost is high. How to reduce the weight of the aircraft and reduce the production cost has become a difficult problem for technicians.

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