首页> 外国专利> TURBOFAN METHOD OF PRODUCING AIRCRAFT LIFT IN HORIZONTAL FLIGHT, AIRCRAFT-TURBOCRAFT, INCREASED LOAD-LIFTING CAPACITY AIRCRAFT

TURBOFAN METHOD OF PRODUCING AIRCRAFT LIFT IN HORIZONTAL FLIGHT, AIRCRAFT-TURBOCRAFT, INCREASED LOAD-LIFTING CAPACITY AIRCRAFT

机译:在水平飞行中制造飞机升力的涡轮风机方法,飞机-涡轮,增加的起升能力飞机

摘要

FIELD: transport.;SUBSTANCE: set of invention relates to aircraft engineering. Proposed method consists in using lifting-bearing turbofans with gas drive from turbojet engines, while horizontal flight is performed by turbojet or piston engines with longitudinal thrust vector with respect to aircraft. Aircraft flight is controlled by elevation and vertical rudders. High-speed aircraft-turbocraft comprises airframe, turbojet engines, lifting-bearing turbofans with gas drive from turbojet engines arranged along aircraft sides or above airframe. High-speed increased load-lifting capacity aircraft comprises combined flight complex consisting of aerodynamic control surface, lifting-bearing variable thrust vector turbofans, turbojet or piston engines, and has-jet rudders. Turbofan engines can be used as gas generators.;EFFECT: reduced drag and take-off-and landing run time.;6 cl, 4 dwg
机译:技术领域本发明涉及飞机工程。提出的方法包括使用带有涡轮喷气发动机的气体驱动的带轴承的涡轮风扇,而水平飞行则由具有纵向推力矢量的涡轮喷气发动机或活塞发动机进行。飞机的飞行由仰角和垂直方向舵控制。高速飞机涡轮飞机包括机身,涡轮喷气发动机,带有气动力的起重涡轮风扇,这些涡轮发动机的气体驱动来自沿着飞机侧面或机身上方布置的涡轮喷气发动机。高速增加的起重能力飞机包括由空气动力学控制面,起升轴承的可变推力矢量涡轮风扇,涡轮喷气发动机或活塞发动机以及喷气式尾舵组成的联合飞行综合体。涡轮风扇发动机可用作气体发生器。效果:减少了阻力和起降运行时间; 6厘升,4载重吨

著录项

  • 公开/公告号RU2401771C2

    专利类型

  • 公开/公告日2010-10-20

    原文格式PDF

  • 申请/专利权人 GOROBTSOV VENIAMIN MIKHAJLOVICH;

    申请/专利号RU20080142889

  • 发明设计人 GOROBTSOV VENIAMIN MIKHAJLOVICH;

    申请日2008-10-30

  • 分类号B64C15/00;B64C29/00;

  • 国家 RU

  • 入库时间 2022-08-21 18:29:26

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