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    Method and system for improving the performance of an aircraft upon take off
    1.
    发明授权
    Method and system for improving the performance of an aircraft upon take off 有权
    起飞时提高飞机性能的方法和系统

    公开(公告)号：US08437894B2

    公开(公告)日：2013-05-07

    申请号：US12881692

    申请日：2010-09-14

    申请人： Mathieu Berthereau

    发明人： Mathieu Berthereau

    IPC分类号： G06F19/00 ,  G06F17/10

    CPC分类号： B64C13/16 ,  G05D1/0661

    摘要： A method and system for improving aircraft performances during take-off is described. The system (1) can include means (4, 6, 7) for determining an optimised take-off position of the control surfaces (S1-Sn) of the aircraft, in the case where a regulatory safety criterion relating to the minimum gradient of climb with a breakdown engine is predominant.

    摘要翻译： 描述了用于提高起飞时飞机性能的方法和系统。 在系统（1）可以包括用于确定飞行器的控制表面（S1-Sn）的优化的起飞位置的装置（4,6,7），在与最小梯度 以击穿引擎为主。

    METHOD AND SYSTEM FOR IMPROVING THE PERFORMANCE OF AN AIRCRAFT UPON TAKE OFF
    3.
    发明申请
    METHOD AND SYSTEM FOR IMPROVING THE PERFORMANCE OF AN AIRCRAFT UPON TAKE OFF 有权
    改善飞机性能的方法和系统

    公开(公告)号：US20110066306A1

    公开(公告)日：2011-03-17

    申请号：US12881692

    申请日：2010-09-14

    申请人： Mathieu Berthereau

    发明人： Mathieu Berthereau

    IPC分类号： G05D1/00

    CPC分类号： B64C13/16 ,  G05D1/0661

    摘要： A method and system for improving aircraft performances during take-off is described. The system (1) can include means (4, 6, 7) for determining an optimised take-off position of the control surfaces (S1-Sn) of the aircraft, in the case where a regulatory safety criterion relating to the minimum gradient of climb with a breakdown engine is predominant.

    摘要翻译： 描述了用于提高起飞时飞机性能的方法和系统。 在系统（1）可以包括用于确定飞行器的控制表面（S1-Sn）的优化的起飞位置的装置（4,6,7），在与最小梯度 以击穿引擎为主。

    Method and device for an aircraft buffet reduction
    4.
    发明授权
    Method and device for an aircraft buffet reduction 有权
    飞机自动降低的方法和装置

    公开(公告)号：US08191832B2

    公开(公告)日：2012-06-05

    申请号：US12413986

    申请日：2009-03-30

    申请人： Mathieu Berthereau ,  Michel Mazet

    发明人： Mathieu Berthereau ,  Michel Mazet

    IPC分类号： G05D1/00

    CPC分类号： B64C9/16 ,  B64C13/16

    摘要： A method and device of dynamically reducing the buffeting of an airplane. The method is carried out by detecting a risk of buffeting of the airplane in flight by a monitor. At least one control surface is turned by an actuator arranged at a trailing edge of each wing of the airplane. The control surface is turned, at a predetermined respective rate of turn, into a predetermined respective position to modify lift profile of the wing along a wingspan length to reduce lift in at least one buffeting-generating region of each wing.

    摘要翻译： 一种动态减少飞机缓冲的方法和装置。 该方法是通过用监视器检测在飞行中飞行器的缓冲的风险来进行的。 至少一个控制表面由布置在飞机每翼的后缘处的致动器转动。 控制表面以预定的相应的转弯速度转动到预定的相应位置，以沿着翼展长度改变机翼的升力曲线，以减少每个机翼的至少一个缓冲产生区域中的升力。