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The application of wings designed based on the theory of inertial support for aircraft and this bike powered

机译:基于机翼惯性支撑理论设计的机翼及其在飞机上的应用

摘要

The application of wings designed based on the theory of inertial support for aircraft and this bike impulsionados.constitui-se application of wings designed to change the direction and auxiliary support aircraft and this motorcycle driven, based on the theory of sustains In the inertial.The theory of inertial support is based on the idea that the support is produced by the inertia force, the strength of the interaction aerodynamics and propulsion system of the aircraft or aeromodelo.as wings designed on the basis of this theory have smaller surface area and profile with C Urvaturas more gentle than the conventional, thereby allowing greater speed, economy and stability of the flight
机译:基于飞机惯性支撑理论设计的机翼的应用以及这种自行车的冲动。基于惯性持续理论,基于飞机惯性支撑设计的机翼的应用改变了飞机的方向和辅助支撑。惯性支撑理论基于这样的思想,即支撑是由惯性力,飞机或空气模型的相互作用空气动力和推进系统的强度产生的。基于该理论设计的机翼具有较小的表面积和轮廓C Urvaturas比常规飞机更柔和,从而可以提高飞行速度,经济性和稳定性

著录项

  • 公开/公告号BR202013023760U2

    专利类型

  • 公开/公告日2015-09-01

    原文格式PDF

  • 申请/专利权人 RODRIGO BARBOSA DA FONSECA;

    申请/专利号BR20132023760U

  • 发明设计人 RODRIGO BARBOSA DA FONSECA;

    申请日2013-09-10

  • 分类号B64C3/14;

  • 国家 BR

  • 入库时间 2022-08-21 15:16:17

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