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AIRCRAFT AEROBATIC FLIGHT MODEL

机译:飞机特技飞行模型

摘要

FIELD: piloting models.;SUBSTANCE: invention relates to aircraft aerodynamics. Cockpipe aerobatic model of aircraft of "weft" scheme includes made with forward sweep wing 1, fuselage 2, two propulsion units 3. Aerodynamic control surfaces are represented by elevators 4 arranged on wing 1 and all-moving front horizontal tail unit 5. When performing round aerobatics figures, FGTU 5 is not connected to the control system and operates in the weather vane mode, and the model alignment corresponds to the "tailless" scheme. When angles of square and triangular figures are executed, FGTU 5 is connected to a control system and the model has longitudinal instability. In "normal" scheme in weather vane mode wing flaps work, which when making angles of square and triangular figures includes a full-scale control system.;EFFECT: invention is aimed at improvement of operational characteristics of aircraft aerobatic flight model.;1 cl, 2 dwg
机译:技术领域本发明涉及飞机的空气动力学。 “纬线”计划飞机的ock管特技飞行模型包括前掠翼1,机身2,两个推进单元3。气动控制表面由布置在机翼1上的升降机4和全动式前水平尾翼单元5表示。根据特技飞行表演的数字,FGTU 5未连接至控制系统,而是在风向标模式下运行,并且模型对齐方式对应于“无尾”方案。当执行正方形和三角形的角度时,FGTU 5连接到控制系统,并且模型具有纵向不稳定性。在风向标模式下的“正常”方案中,机翼襟翼工作,当使正方形和三角形的角度成角度时,它包括一个全比例的控制系统。效果:本发明旨在改善飞机特技飞行模型的运行特性。 ,2载重吨

著录项

  • 公开/公告号RU2702279C1

    专利类型

  • 公开/公告日2019-10-07

    原文格式PDF

  • 申请/专利权人 MATVEEV VLADISLAV SERGEEVICH;

    申请/专利号RU20190101424

  • 发明设计人 MATVEEV VLADISLAV SERGEEVICH (RU);

    申请日2019-01-18

  • 分类号A63H27/04;B64C39/12;

  • 国家 RU

  • 入库时间 2022-08-21 11:45:57

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