Ducted aircraft capable of being reconstructed aerially in real time, and docking separation method and system

Abstract

The invention provides a ducted aircraft capable of being reconstructed aerially in real time, and a docking separation method and system. The ducted aircraft comprises a first ducted aircraft body, asecond ducted aircraft body and a reconstruction controller. The first ducted aircraft body is provided with a first connecting mechanism, and the second ducted aircraft body is provided with a second connecting mechanism; and the reconstruction controller is used for controlling the first connecting mechanism and the second connecting mechanism to be docked or separated when the first ducted aircraft body and the second ducted aircraft body are in a flight state. The two independent ducted aircraft bodies have the capability of being reconstructed into an integrated mode for collaborative operation under the aerial flight operation condition. In addition, the reconstruction controller can also control the first ducted aircraft body and the second ducted aircraft body which are docked inthe flight state to be separated into the two independent ducted aircraft bodies in real time.

Description

technical field [0001] The invention relates to the technical field of aircraft, in particular to a ducted aircraft capable of real-time reconfiguration in the air, a docking and separation method and a system. Background technique [0002] In highly complex urban environments and mountainous environments, unmanned aerial vehicles, as airborne platforms for detection equipment and operating equipment, often emphasize low-altitude, low-speed and stable flight performance. Compared with the traditional open rotor aircraft, the ducted aircraft can take off, land and hover vertically, and requires less space for take-off and safe flight. It is especially suitable for various complex environments such as urban buildings, post-disaster ruins, and narrow alleys. The flight operation in the middle; the effect of increasing the lift of the duct is significant at low altitude and low speed flight, which makes the ducted aircraft require less power under the same diameter of the propel...

AI Technical Summary

Problems solved by technology

[0004] The present invention proposes a ducted aircraft that can be reconfigured in real time in the air, a docking and separation method and system, overcomes the contradiction between maneuverability and load capacity in the field of traditional aircraft, and aims to solve the problem that the current combinable aircraft must return to the ground for docking and separation. The problems of low operating efficiency and limited applicable environment

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