고고도 비행선의 기낭 구조
    1.
    发明公开
    고고도 비행선의 기낭 구조 无效
    高海拔平原的包容性结构

    公开(公告)号:KR1020030050310A

    公开(公告)日:2003-06-25

    申请号:KR1020010080723

    申请日:2001-12-18

    CPC classification number: B64B1/58 B64C39/02 B64C2201/022

    Abstract: PURPOSE: An envelope structure is provided to prevent the sudden inclination of helium and the large change of a helium volume ratio by a simple structure. CONSTITUTION: A front partition(2) and a rear partition(3) divide the inside of a plane(1) to three parts. Separating films(7,8,9) are installed in the center of the front partition and the rear partition. A front helium envelope(4), a middle helium envelope(5) and a rear helium envelope(6) are divided in the upper part and a front air envelope(10), and a middle air envelope(11) and a rear air envelope(12) are divided by the separating films. Thereby, the sudden inclination of helium and the large change of a helium volume ratio are prevented.

    Abstract translation: 目的:提供一种包络结构,通过简单的结构防止氦的突然倾斜和氦体积比的大的变化。 构成:前隔板(2)和后隔板(3)将平面(1)的内部分成三部分。 分隔膜(7,8,9)安装在前隔板和后隔板的中心。 前氦气封(4),中氦气囊(5)和后氦气囊(6)被分成上部和前部气囊(10),中部空气气囊(11)和后部空气 信封(12)被分离膜分隔。 从而防止氦的突然倾斜和氦体积比的大的变化。

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