首页> 外国专利> Inclined starting and landing disc aircraft for aerospace industry, has internal coaxial twin turbines to develop operation impulse, and main components, corpuses and turbine separating construction, which form twin turbine shells

Inclined starting and landing disc aircraft for aerospace industry, has internal coaxial twin turbines to develop operation impulse, and main components, corpuses and turbine separating construction, which form twin turbine shells

机译:用于航空航天的倾斜起降盘式飞机,具有内部同轴双涡轮机以产生运行冲力,主要部件,主体和涡轮机分离结构形成双涡轮机壳

摘要

The aircraft has upper and lower corpuses, and internal coaxial twin upper and lower turbines (11, 12) to develop operation impulse. A wall opposite to the upper turbine runs to its diagonal, rotatarily moves outward and downwards and stops at a turbine separating disc. The main components, upper corpus, lower corpus and turbine separating construction form the twin turbine shells. The upper corpus is connected with a main shaft.
机译:该飞机具有上,下主体,以及内部同轴双上,下涡轮(11、12),以产生运行冲动。与上部涡轮机相对的壁沿其对角线延伸,可旋转地向外和向下移动,并停在涡轮机分离盘处。上主体,下主体和涡轮分离结构的主要组成部分构成了双涡轮壳体。上语料库与主轴连接。

著录项

  • 公开/公告号DE102004050146A1

    专利类型

  • 公开/公告日2006-04-20

    原文格式PDF

  • 申请/专利权人 MENACHO PAUL;

    申请/专利号DE20041050146

  • 发明设计人 MENACHO PAUL;

    申请日2004-10-11

  • 分类号B64C29/00;

  • 国家 DE

  • 入库时间 2022-08-21 21:20:41

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