公开(公告)号：US20130001362A1

公开(公告)日：2013-01-03

申请号：US13588276

申请日：2012-08-17

申请人： Peter Kreuzer ,  Sven Schaber ,  Iris Goldhahn

发明人： Peter Kreuzer ,  Sven Schaber ,  Iris Goldhahn

IPC分类号： B64C23/06

CPC分类号： B64C23/06 ,  B64C21/10 ,  Y02T50/162

摘要： An arrangement of aerodynamic auxiliary surfaces is configured for being arranged on the underside of an aircraft and furthermore includes a longitudinal axis and at least one aerodynamic auxiliary surface, wherein the aerodynamic auxiliary surface is laterally offset referred to the longitudinal axis, and wherein the aerodynamic auxiliary surface is configured for generating vortices when it is subjected to an oncoming air flow. This makes it possible to compensate vortices caused by the shape of the aircraft such that the directional stability of the aircraft can be improved and the aerodynamic drag may be reduced.

摘要翻译： 空气动力辅助表面的布置被配置为布置在飞行器的下侧，并且还包括纵向轴线和至少一个空气动力学辅助表面，其中空气动力辅助表面以纵向轴线横向偏移，并且其中空气动力辅助 表面被配置为在受到迎面而来的气流时产生涡流。 这使得可以补偿由飞行器的形状引起的旋涡，从而可以提高飞机的方向稳定性并且可以减小空气动力学阻力。

公开(公告)号：US09038950B2

公开(公告)日：2015-05-26

申请号：US13588276

申请日：2012-08-17

申请人： Peter Kreuzer ,  Sven Schaber ,  Iris Goldhahn

发明人： Peter Kreuzer ,  Sven Schaber ,  Iris Goldhahn

IPC分类号： B64C1/38 ,  B64C23/06 ,  B64C21/10

CPC分类号： B64C23/06 ,  B64C21/10 ,  Y02T50/162

摘要： An arrangement of aerodynamic auxiliary surfaces is configured for being arranged on the underside of an aircraft and furthermore includes a longitudinal axis and at least one aerodynamic auxiliary surface, wherein the aerodynamic auxiliary surface is laterally offset referred to the longitudinal axis, and wherein the aerodynamic auxiliary surface is configured for generating vortices when it is subjected to an oncoming air flow. This makes it possible to compensate vortices caused by the shape of the aircraft such that the directional stability of the aircraft can be improved and the aerodynamic drag may be reduced.

摘要翻译： 空气动力辅助表面的布置被配置为布置在飞行器的下侧，并且还包括纵向轴线和至少一个空气动力学辅助表面，其中空气动力辅助表面以纵向轴线横向偏移，并且其中空气动力辅助 表面被配置为在受到迎面而来的气流时产生涡流。 这使得可以补偿由飞行器的形状引起的旋涡，从而可以提高飞机的方向稳定性并且可以减小空气动力学阻力。