Modularized airplane

Abstract

The invention relates to a modularized airplane. Wings, an empennage and a mission cabin are modularly arranged; the wings comprise a left outer wing, a right outer wing and a center wing; the left outer wing is connected with the center wing; the center wing is connected with the right outer wing; the mission cabin is connected with the center wing; cabins are connected to the positions, on the center wing, on two sides of the mission cabin; an undercarriage is arranged on the lower part of each cabin; the empennage is arranged on the tail parts of the cabins; when a long endurance mission isexecuted, a turboprop structure is adopted, paddles and a turboprop engine inlet are arranged on the head parts of the cabins; turboprop engines are arranged in the cabins; when a quick response request mission is executed, a jet propelled structure is adopted, and a jet propelled air inlet is arranged on the head parts of the cabins; the corresponding mission cabin is selected according to different combat missions, so that the operational effectiveness and the airplane use ratio are improved; and cabins with different power systems are arranged according to the requirements such as the response speed and the endurance / voyage of the executed missions, and one platform realizes two structures, so that the airplane use efficiency and the mission adaptability are effectively improved.

Description

technical field [0001] The invention relates to the technical field of aircraft design, in particular to a modular aircraft. Background technique [0002] After more than a hundred years of development, the aviation industry has formed various types of aircraft, including fighter jets, transport aircraft, trainer aircraft, and business jets. The aerodynamic layout of various types of aircraft has developed into various forms, including conventional, flying wing, canard, joint wing and other layout forms, and each type of aerodynamic layout has its advantages in some aspects due to its unique characteristics with advantages. With the development of aircraft multi-purpose and large loading requirements, it is difficult for traditional aircraft to carry out modular changes due to the connection relationship between various aerodynamic components; and the fuselage and other components are generally large in size in order to meet loading requirements, resulting in structural wei...

AI Technical Summary

Problems solved by technology

With the development of aircraft multi-purpose and large loading requirements, it is difficult for traditional aircraft to carry out modular changes due to the connection relationship between various aerodynamic components; and the fuselage and other components are generally large in size in order to meet loading requirements, resulting in structural weight. Large, and there is limited space for further improvement of the mounting capacity, which is not enough to meet the needs of multi-tasking flexible configuration, large mounting capacity, and multi-mode use

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