首页> 外国专利> Passenger aircraft i.e. airplane, has intense internal thruster arranged at rear of fuselage, and intake ports integrated into sides of body, where air intake ports are arranged to obtain favorable aerodynamic form

Passenger aircraft i.e. airplane, has intense internal thruster arranged at rear of fuselage, and intake ports integrated into sides of body, where air intake ports are arranged to obtain favorable aerodynamic form

机译:客机,即飞机,在机身后部装有强劲的内部推进器,进气口集成在机身侧面,进气口布置成获得良好的空气动力学性能

摘要

The aircraft has an intense internal thruster (1) arranged at a rear of a fuselage, where the thruster is provided with a gear box. Air intake ports (2) are integrated into the sides of a body, where the air intake ports are arranged to obtain a favorable aerodynamic form such that thrust emerges from a thrust nozzle (3) at a rear of the aircraft. An extensible escalator (4) is attached to the body, and two ram-jet engines are arranged under idle bearing areas. Two turbines and two compressors are arranged in a longitudinal axis of the thruster.
机译:该飞机在机身后部装有一个强力的内部推进器(1),该推进器配有齿轮箱。进气口(2)被集成到机体的侧面,进气口被布置成获得良好的空气动力学形式,使得推力从飞机后部的推力喷嘴(3)出现。可伸缩的自动扶梯(4)安装在车身上,在空转轴承区下方布置了两个冲压发动机。在推进器的纵轴上布置有两个涡轮机和两个压缩机。

著录项

  • 公开/公告号DE102010018928A1

    专利类型

  • 公开/公告日2011-11-03

    原文格式PDF

  • 申请/专利权人 BIHLER GERHARD;

    申请/专利号DE20101018928

  • 发明设计人 BIHLER GERHARD;

    申请日2010-04-30

  • 分类号B64D27/20;B64C1/24;F02K3/12;F02C1/05;F02K7/10;

  • 国家 DE

  • 入库时间 2022-08-21 17:47:15

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