The invention provides a novel passenger life escape device of a civil aircraft, which comprises an aircraft body, a turbofan engine mounted on each of the left and right sides of the aircraft body, two turbojet subsonic combustion impact combined cycle engines mounted on a stabilizer at the rear part of the aircraft, and three pairs of staggered semicircular wings arranged on the two sides of the aircraft body, the aircraft is novel in structural design, the semicircular wings are adopted, the cargo hold space of the whole mother aircraft is saved, the sufficient flight speed is kept in the flight process of being separated from the mother aircraft, the flight speed is high, the flight speed is high, and the flight speed is high. And air resistance is reduced, so that the escape device can quickly enter sky clouds above severe weather and enter a safe height, and the escape safety is further improved.

    本申请提供一种新型民航飞机的旅客生命逃生装置,包括机身,机身左右两侧分别安装一台涡扇发动机,飞机后部安定位上装有二台涡轮喷气亚燃冲击组合循环发动机,还包括三对半圆形机翼,且机身两侧有错开的3对半圆形机翼,三对半圆形机翼环圈在机身外壁,半圆形机翼外端部设置机翼卡口,机翼卡口处安装卡紧组件,卡紧组件卡紧长臂翼一端,本发明结构设计新颖,采用半圆形机翼,节省整个母机的货舱空间,且在脱离母机的飞行过程中保持足够的飞行速度,以及整体升力,减少空气阻力,有利于快速进入恶劣天气以上的的天空云层,进入安全高度,进一步提高了逃生安全性。


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    Title :

    Novel passenger life escape device of civil aircraft


    Additional title:

    一种新型民航飞机的旅客生命逃生装置


    Contributors:
    KE JIAXIANG (author)

    Publication date :

    2024-12-20


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen



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