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NOVEL JET LIFT AUGMENTATION AND STABILITY AUGMENTATION AMPHIBIOUS AIRCRAFT AND APPLICATION METHOD THEREFOR

机译:新型喷气增升增稳两栖飞机及其应用方法

摘要

Disclosed in the present invention are a novel jet lift augmentation and stability augmentation amphibious aircraft and an application method therefor. An air inlet fan is communicated with an air inlet end of a pressurized air storage tank; an air outlet end of the pressurized air storage tank is communicated with a flow dividing pipeline; the flow dividing pipeline is communicated with a plurality of air chambers, separately; regulating valves are provided at positions where the plurality of air chambers are communicated with the flow dividing pipeline; the plurality of air chambers are distributed at a plurality of positions of the bottom of the aircraft, and the plurality of air chambers are used for jetting outwardly. A navigation state sensing device is used for detecting navigation data of the aircraft and sending the navigation data to an intelligent analysis device; the intelligent analysis device is used for analyzing the navigation data, obtaining a control scheme, and sending the control scheme to a jet control device; the jet control device controls opening and closing states of the regulating valves according to the control scheme, so as to adjust jet states of the plurality of air chambers. The jet volume of the positions of the bottom of the aircraft is adjusted from a plurality of directions, so that the aircraft is assisted in flying stably, and the difficulty in the prior art is practically solved.
机译:本发明公开了一种新型喷气升力增强和稳定性增强两栖飞机及其应用方法。进气风扇与压缩空气储罐的进气端连通;所述压缩空气储罐的出风端与分流管路连通;分流管路分别与多个气室连通;调节阀设置在多个气室与分流管路连通的位置;多个气室分布在飞机底部的多个位置,多个气室用于向外喷射。导航状态传感装置用于检测飞机的导航数据,并将导航数据发送给智能分析装置;智能分析装置用于分析导航数据,获得控制方案,并将控制方案发送给射流控制装置;喷射控制装置根据控制方案控制调节阀的开启和关闭状态,以调整多个气室的喷射状态。从多个方向调整飞机底部位置的喷射量,从而帮助飞机稳定飞行,实际解决了现有技术的难点。

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