首页> 外国专利> 'MAXINIO' STANDARD TECHNOLOGY OF VEHICLE MANUFACTURING AND OPERATION, NO-RUN TAKE-OFF AND LANDING ELECTRIC AIRCRAFT (VERSIONS), LIFTING DEVICE, TURBO-ROTARY ENGINE (VERSIONS), MULTISTEP COMPRESSOR, FAN COWLING, TURBO-ROTARY ENGINE OPERATION METHOD AND METHOD OF ELECTRIC AIRCRAFT LIFTING FORCE CREATION METHOD

'MAXINIO' STANDARD TECHNOLOGY OF VEHICLE MANUFACTURING AND OPERATION, NO-RUN TAKE-OFF AND LANDING ELECTRIC AIRCRAFT (VERSIONS), LIFTING DEVICE, TURBO-ROTARY ENGINE (VERSIONS), MULTISTEP COMPRESSOR, FAN COWLING, TURBO-ROTARY ENGINE OPERATION METHOD AND METHOD OF ELECTRIC AIRCRAFT LIFTING FORCE CREATION METHOD

机译:车辆制造和操作,空转起飞和着陆电动飞机(版本),起升装置,涡轮增压发动机(版本),多级压缩机,风扇冷却,涡轮增压和发动机运行方法的“ MAXINIO”标准技术飞机起升力建立方法的研究

摘要

FIELD: transport.;SUBSTANCE: set of invention relates to aircraft engineering. In the first version, no-run take-off and landing electric aircraft contains fuselage (1) with pillars (3) and helical fan in cowlings (2), lifting planes and chassis. Turbo-rotary engines (4) have generator units of the first and the second screws connected by electric circuit with electric motors (12,13) of the first (23) and the second (28) screw respectively of screw fan (11) installed on the front upper pillar (10). In the second version, no-run take-off and landing electric aircraft contains fuselage with upper and lateral pillars with fork at the end. In the fork of front upper pillar (10), turbo-rotary engine (4) with generator units having rotors on shafts of screw fan screws is installed, and in forks of front lateral pillars (48), electric motors (50) driven fans (49) are installed. Invention also covers lifting device, turbo-rotary engine, multistep compressor, fan cowling, turbo-rotary engine operation method and lifting force creation method.;EFFECT: improved flight safety and comfort as well as increased elevating capacity.;14 cl, 15 dwg
机译:技术领域本发明涉及飞机工程。在第一个版本中,空跑起降电动飞机包含带有支柱(3)的机身(1)和位于整流罩(2)中的螺旋形风扇,起升飞机和底盘。涡轮转子发动机(4)具有通过电路与分别安装有螺旋风扇(11)的第一(23)和第二(28)的电动机(12,13)的电动机连接的第一和第二螺钉的发电机单元。在前上部支柱(10)上。在第二版中,空跑起降电动飞机包含机身,机身上部和侧面均带有叉形末端。在前上支柱(10)的前叉中,安装了涡轮发电机(4),该发电机的发电机单元在风扇螺杆的轴上具有转子,在前侧支柱(48)的前叉中,电动机(50)驱动了风扇。 (49)已安装。发明还涉及起重装置,涡轮旋转式发动机,多级压缩机,风扇整流罩,涡轮旋转式发动机的操作方法和产生升力的方法。效果:提高了飞行安全性和舒适性,并提高了起重量。14 cl,15 dwg

著录项

  • 公开/公告号RU2457153C2

    专利类型

  • 公开/公告日2012-07-27

    原文格式PDF

  • 申请/专利权人 MAKSIMOV NIKOLAJ IVANOVICH;

    申请/专利号RU20100130447

  • 发明设计人 MAKSIMOV NIKOLAJ IVANOVICH;

    申请日2010-07-20

  • 分类号B64C29;B64C39/08;B64C3;F02K3/04;F04D19/02;B64D33/02;

  • 国家 RU

  • 入库时间 2022-08-21 17:05:58

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