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AIRCRAFT FOR PERFORMING OBSERVATIONS IN THE STRATOSPHERE

机译:用于在平流层中进行观测的飞机

摘要

Aircraft is equipped with a telescope built in the fuselage (1) with the initial angular mirror (2) installed in the open part of the fuselage (1) and the main mirror (7) installed in the cylindrical part of the fuselage. The open part of the fuselage (1) represents an open observation cavity with the base made of the bottom arc section of the fuselage (1) rigidly connected with the nose (2) of the aircraft, main mirror (7) is permanently fixed at the end of the cylindrical part of the fuselage (1) at the tail (5) and the initial angular mirror (2) is rotary fixed to the nose (3). Axis of rotation of the initial angular mirror (2) overlaps the longitudinal axis (12) of the aircraft and optical axis of the main mirror (7), the bottom arc section of the fuselage (1) has a recess (13) for observation of the earth, and the lifting surface (6) is releasably fixed to the cylindrical part of the fuselage (1).
机译:飞机在机身(1)中配备有望远镜,初始角镜(2)安装在机身(1)的开口部分,主镜(7)安装在机身的圆柱形部分。机身(1)的开放部分代表一个开放的观察腔,其底部由机身(1)的底部弧形部分制成,与飞机的机头(2)牢固连接,主镜(7)永久固定在机身(1)的圆柱形部分的尾部(5)的端部和初始角镜(2)旋转固定到机头(3)。初始角镜(2)的旋转轴与飞机的纵轴(12)和主镜(7)的光轴重叠,机身(1)的底部弧形部分具有凹口(13),用于观察提升表面(6)可释放地固定在机身(1)的圆柱部分上。

著录项

  • 公开/公告号WO2020171722A1

    专利类型

  • 公开/公告日2020-08-27

    原文格式PDF

  • 申请/专利权人 INSTYTUT LOTNICTWA;

    申请/专利号WO2020PL00019

  • 发明设计人 ŻURAWSKI RAFAŁ;

    申请日2020-02-19

  • 分类号B64C39/02;B64D37/04;B64D47/08;B64C1/26;

  • 国家 WO

  • 入库时间 2022-08-21 11:09:39

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