Modular flying wing type multi-fuselage aircraft splicing method

Abstract

The invention discloses a modular flying wing type multi-fuselage aircraft splicing method. The modular flying wing type multi-fuselage aircraft splicing method is characterized by comprising the following steps that firstly, a fuselage and a wing separation surface are built on the theoretical appearance of a flying wing type aircraft, and fuselage and wing basic units are formed; then, rapid abut joint structures are arranged on the separating surface; and finally, the multiple fuselage are spliced and combined through the rapid abut joint structures. According to the method, the fuselage unit and the wing unit of the modular flying wing type aircraft are built on the basis of a traditional flying wing type aircraft, rapid splicing is realized by means of the comb-shaped structure, and the modular flying wing type multi-fuselage aircraft is built.

Description

technical field [0001] The invention belongs to the field of aircraft digital design, and relates to a splicing method of a modular flying-wing multi-fuselage aircraft. Background technique [0002] The traditional flying-wing aircraft is an aircraft in which the fuselage and wings are integrated. It has the characteristics of light structure, large effective load, low flight resistance, high lift-to-drag ratio, and good stealth performance. However, due to the structure of the traditional flying-wing aircraft is fixed from the beginning of the design, the parameters of the aircraft's maximum take-off weight, maximum range, maximum load and weapon loading are also fixed accordingly, and it cannot carry more than the maximum load. The weight of cargo cannot be flexibly adjusted according to the type and quantity of the cargo being carried, so as to meet the needs of various missions with low fuel consumption and high transportation capacity. At the same time, traditional fly...

AI Technical Summary

Problems solved by technology

However, due to the structure of the traditional flying-wing aircraft is fixed from the beginning of the design, the parameters of the aircraft's maximum take-off weight, maximum range, maximum load and weapon loading are also fixed accordingly, and it cannot carry more than the maximum load. The heavy cargo cannot be flexibly adjusted according to the type and quantity of the cargo being carried, so as to meet the needs of various missions with low fuel consumption and high transportation capacity

At the same time, traditional flying-wing aircraft are limited by range and weapon loading, and cannot greatly improve the combat performance of the aircraft through rapid modification to meet the military's mission requirements for longer cruise and stronger firepower.

Due to the limited structure of traditional flying wing aircraft, it cannot meet the needs of multi-role switching and efficient tasks such as detection, rescue, and transportation of the same aircraft, as well as the rapid structural replacement and maintenance of faulty aircraft.

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