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1. 发明申请

WO2013107944A3 REGULATING OF VORTEX SHEETS 审中-公开
标题翻译： VORTEX表的规定
公开(公告)号：WO2013107944A3
公开(公告)日：2014-07-10
申请号：PCT/FR2012000024
申请日：2012-01-17
申请人： BUENDIA JOSE , RIVIERE GEORGES-MARC , SCHULTZ CHRISTOPHE , PERRICHON CLAUDE ANNIE , PICCALUGA PIERRE , GIRY FRANÇOIS , FOCHESATO BRUNO
发明人： BUENDIA JOSE , RIVIERE GEORGES-MARC , SCHULTZ CHRISTOPHE , PERRICHON CLAUDE ANNIE , PICCALUGA PIERRE , GIRY FRANÇOIS , FOCHESATO BRUNO
IPC分类号： C09D7/00 , B64C23/00
CPC分类号： B64C23/005 , B64C2230/12 , C08K3/04 , C08K3/08 , C08K2003/0812 , C08K2003/085 , C08K2003/2234 , C08K2003/2237 , C09D5/00 , C09D7/61 , C09D7/69 , Y02T50/166
摘要： In the world of aeronautics, the modes of aerodynamic behaviour are complex and come as much from experimentation as computations for modelling the principles of flight. The behaviour of the flight is realized in three dimensions in the actual dynamics of the behaviour of the profiles of aircraft, thereby complicating the intellectual approaches of engineers on the ground. The technical approach is the reducing of drag, this being the most penalizing factor requiring thorough study. Indeed, the drag contributes to the resistance to forward motion, and decreasing it is the fundamental principle by which we afford through the present PCT application, a solution for at least 10%, which is totally new, since it is a novel approach based on fundamental principles of magnetic, electrical and electromagnetic reactivities of structures. These various fluxes around the profile exist through the viscosity of the air, which allows different directions and speeds which impose different voltage constraints on the structure. The method and the product make it possible to limit the counter-reactions identified so as to stabilize the flight in a significant manner in order to improve the operating cost thereof, by attenuating the effects of vortex sheets around the profiles, and especially the effects of phase shift on the structures which electrically polarize the structures. To regulate the phase shifts and electrical polarizations of the structures, we use a quantum product which stops or smoothes, or expunges the voltage deviations.
摘要翻译：在航空世界中，空气动力学行为的模式是复杂的，并且与实验一样多地用于模拟飞行原理的计算。飞行的行为在飞机轮廓行为的实际动态中三维实现，从而使实地工程师的智力方法复杂化。技术方法是减少拖累，这是需要彻底研究的最严厉的因素。事实上，这种拖累有助于抵制前进运动，减少它是我们通过目前的PCT申请提供的基本原则，至少10％的解决方案是全新的，因为它是一种基于结构的磁性，电气和电磁反应性的基本原理。轮廓周围的这些各种助焊剂通过空气的粘度存在，这允许不同的方向和速度对结构施加不同的电压约束。该方法和产品使得可以通过减弱涡轮板在型材周围的影响来限制所确定的反作用以便以显着的方式稳定飞行，从而提高其运行成本，特别是影响在结构电极化的结构上的相移。为了调节结构的相移和电极化，我们使用停止或平滑或消除电压偏差的量子产物。

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