Load structure integrated sensor flight vehicle

Abstract

The invention belongs to the technical field of unmanned aerial vehicles and specifically relates to a load structure integrated sensor flight vehicle. The load structure integrated sensor flight vehicle comprises a fuselage, wherein along the horizontal direction, the fuselage has a flat shape; a flight control system, a measurement control system and an electric system are mounted in a middle region of the fuselage; radar, electronic reconnaissance, communication and electronic warfare equipment is composed of an antenna, a receiving-transmitting array module, a comprehensive treatment extension and on-board control equipment; the antenna is arrayed along the peripheral direction of an edge region of the flat fuselage; the antenna and a skin of the fuselage form an integrated structure; the fuselage is fixedly mounted on a pneumatic structure, which is formed by assembling wings, an empennage, an engine and an adapting piece, through a bracket, and the fuselage and the pneumatic structure are arranged along the vertical direction in a manner of forming a distance. By adopting the load structure integrated sensor flight vehicle, all-directional 360-degree scanning of on-board task load equipment is convenient to carry out and reconnaissance and monitoring tasks are implemented; the problem of mutual interference and shielding of a conventional aerial vehicle structure and a task load function is overcome and the performance of the on-board task load equipment is optimized.

Description

technical field [0001] The invention belongs to the technical field of unmanned aerial vehicles, and in particular relates to a load-structure integrated sensor aircraft. Background technique [0002] Now the common aerial electronic reconnaissance and early warning platforms are all modified by the aircraft shape and number that have been put into use, and a balance beam or disc antenna structure is installed on the back of the fuselage. This design method greatly destroys the aerodynamic layout of the original aircraft, at the cost of sacrificing the performance of the aircraft platform, and what’s more, it needs to change the aerodynamic layout of the carrier aircraft, and add additional tail end plates, fuselage dorsal fins or pelvic fins to improve flight The performance can barely meet the design requirements; the modified structure of the fuselage and the structure installed to meet the needs of mission equipment will greatly increase the weight of the aircraft, short...

AI Technical Summary

Problems solved by technology

[0003] Using the air system with a balance beam structure antenna and a disc structure antenna installed on the upper part of the aircraft fuselage, the radio signals sent and received by the reconnaissance and early warning mission equipment will be blocked, interfered by structures such as the fuselage, wings, and vertical tail. Restrictions, there are observation blind spots, and the performance cannot be fully utilized

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