公开(公告)号：US20110040534A1

公开(公告)日：2011-02-17

申请号：US12673670

申请日：2007-08-16

申请人： Miguel Gonzalez Cuadrado

发明人： Miguel Gonzalez Cuadrado

IPC分类号： G06F17/14 ,  G06G7/48

CPC分类号： G09B9/46

摘要： This procedure proposes the appropriate equations that determine the rotor movement in order to obtain the aerodynamic actions for each blade in each iteration (the forces that are transmitted to the helicopter and the moments with respect to the articulations), and they are resolved by discretizations made in the rotor disc, such that that the blade elements of the partition are connected to the disc, which does not rotate, instead of to each blade. The blades pass through an azimuth range in each iteration, making a division of each blade longitudinally into ne elements, and the rotor disc into na sectors, corresponding to divisions of the range of azimuth angles. Therefore, partitions are made on ne·na blade elements, identifying each blade element by means of its distance to the rotor axis and its azimuth angle.

摘要翻译： 该过程提出了确定转子运动的适当方程，以便在每次迭代中获得每个叶片的空气动力学动作（传递到直升机的力和相对于关节的力矩），并且它们通过离散化来解决 在转子盘中，使得分隔件的叶片元件连接到不旋转的盘而不是每个叶片。 叶片在每次迭代中通过方位角范围，使得每个叶片纵向分割成ne元素，并且转子盘分成与扇形方位角范围的分割相对应的na个扇区。 因此，分隔是在ne·na叶片元件上制成的，通过其与转子轴的距离及其方位角来识别每个叶片元件。

公开(公告)号：US08589131B2

公开(公告)日：2013-11-19

申请号：US12673670

申请日：2007-08-16

申请人： Miguel Gonzalez Cuadrado

发明人： Miguel Gonzalez Cuadrado

IPC分类号： G06F17/50 ,  G06F7/60 ,  G06G7/48

CPC分类号： G09B9/46

摘要： This procedure proposes the appropriate equations that determine the rotor movement in order to obtain the aerodynamic actions for each blade in each iteration (the forces that are transmitted to the helicopter and the moments with respect to the articulations), and they are resolved by discretizations made in the rotor disc, such that that the blade elements of the partition are connected to the disc, which does not rotate, instead of to each blade. The blades pass through an azimuth range in each iteration, making a division of each blade longitudinally into ne elements, and the rotor disc into na sectors, corresponding to divisions of the range of azimuth angles. Therefore, partitions are made on ne·na blade elements, identifying each blade element by means of its distance to the rotor axis and its azimuth angle.

摘要翻译： 该过程提出了确定转子运动的适当方程，以便在每次迭代中获得每个叶片的空气动力学动作（传递到直升机的力和相对于关节的力矩），并且它们通过离散化来解决 在转子盘中，使得分隔件的叶片元件连接到不旋转的盘而不是每个叶片。 叶片在每次迭代中通过方位角范围，使得每个叶片纵向分割成ne元素，并且转子盘分成与扇形方位角范围的分割相对应的na个扇区。 因此，分隔是在ne·na叶片元件上制成的，通过其与转子轴的距离及其方位角来识别每个叶片元件。