公开(公告)号：US08864081B2

公开(公告)日：2014-10-21

申请号：US13557381

申请日：2012-07-25

申请人： Florian Constans ,  Mickaël Lefebvre

发明人： Florian Constans ,  Mickaël Lefebvre

IPC分类号： G05D1/00 ,  G05D1/12 ,  G05D1/06

CPC分类号： G05D1/0676

摘要： A method is described for optimized energy management of an aircraft upon a flight along a trajectory. The method allows the aircraft to join a given point of the trajectory in a given energy state, with a given position of the slats and flaps, and with a given position of the landing gear. The method includes determining current parameter values of the aircraft. The method also includes determining optimized command orders based on the current parameter values by performing a sequence of operations in an iterative way. The method further includes applying the optimized command orders to an automatic slats and flaps command device and an automatic landing gear command device for automatic control of the slats and flaps and the landing gear, respectively.

摘要翻译： 描述了一种在沿着轨迹的飞行中优化飞行器的能量管理的方法。 该方法允许飞行器以给定的能量状态，具有板条和翼片的给定位置以及起落架的给定位置加入轨迹的给定点。 该方法包括确定飞行器的当前参数值。 该方法还包括通过以迭代方式执行一系列操作来基于当前参数值来确定优化的命令顺序。 该方法还包括将优化的命令命令应用于自动板条和襟翼指令装置以及分别用于自动控制板条和襟翼和起落架的自动起落架指令装置。

公开(公告)号：US20130026299A1

公开(公告)日：2013-01-31

申请号：US13557381

申请日：2012-07-25

申请人： Florian Constans ,  Mickaël Lefebvre

发明人： Florian Constans ,  Mickaël Lefebvre

IPC分类号： B64C13/16

CPC分类号： G05D1/0676

摘要： Method and device for an optimal management of the slats, the flaps and the landing gear of an aircraft.The device (1) includes means (5) for determining, in an iterative manner, according to a predicted energy state, optimal commands of means (10, 11) for controlling the slats, the flaps and the landing gear of the aircraft, which allow the aircraft to reach a given point of a trajectory in a given energy state with a given aerodynamic configuration and a given position of the landing gear.

摘要翻译： 用于飞机的板条，襟翼和起落架的最佳管理的方法和装置。 装置（1）包括用于根据预测的能量状态以迭代方式确定用于控制飞机的板条，翼片和起落架的装置（10,11）的最佳命令的装置（5），其中 允许飞机在给定的能量状态下达到具有给定空气动力学构型和起落架的给定位置的轨迹的给定点。

公开(公告)号：US08249792B2

公开(公告)日：2012-08-21

申请号：US12575286

申请日：2009-10-07

申请人： Emmanuel Blanvillain ,  Florian Constans ,  David Chabe

发明人： Emmanuel Blanvillain ,  Florian Constans ,  David Chabe

IPC分类号： G06F19/00

CPC分类号： B64D31/06 ,  G05D1/0072

摘要： Disclosed is a method and device for protecting an aircraft comprising at least one wing-mounted engine arranged on each of its wings against at least one of a low-energy situation and a high-energy situation during flight in which at least one engine is a failed engine. A control unit is triggered to activate a protection function, as a function of the number and position of failed engines. The control unit controls at least one non-failed engine, and the protection function is activated when activation conditions are met. The activation conditions indicate that the aircraft is either in the low-energy situation such that the total current power of the aircraft is less than a predetermined minimum power or that the aircraft is in the high-energy situation such that the total current power of the aircraft is greater than a predetermined maximum total power.

摘要翻译： 公开了一种用于保护飞行器的方法和装置，其包括布置在其每个翼上的至少一个机翼安装的发动机，以抵抗飞行中的低能量情况和高能量情况中的至少一个，其中至少一个发动机是 发动机失效 触发控制单元以根据故障发动机的数量和位置来激活保护功能。 控制单元控制至少一个非故障发动机，并且当满足激活条件时激活保护功能。 激活条件表明飞机处于低能量状态，使得飞机的总电流功率小于预定的最小功率，或者飞机处于高能量状态，使得飞行器的总电流功率 飞机大于预定的最大总功率。

公开(公告)号：US20100100262A1

公开(公告)日：2010-04-22

申请号：US12575286

申请日：2009-10-07

申请人： Emmanuel Blanvillain ,  Florian Constans ,  David Chabe

发明人： Emmanuel Blanvillain ,  Florian Constans ,  David Chabe

IPC分类号： G06F19/00

CPC分类号： B64D31/06 ,  G05D1/0072

摘要： According to the invention, an aircraft speed threshold is computed in order to calculate a total power to apply to aircraft engines. When conditions of activation are fulfilled, the current individual power of each aircraft engine in operation controlled by a protection function is gradually modified.

摘要翻译： 根据本发明，计算飞行器速度阈值以计算应用于飞机发动机的总功率。 当满足激活条件时，由保护功能控制的每个飞机发动机的当前单独功率逐渐改变。

公开(公告)号：US08892275B2

公开(公告)日：2014-11-18

申请号：US13559295

申请日：2012-07-26

申请人： Florian Constans ,  Mickael Lefebvre

发明人： Florian Constans ,  Mickael Lefebvre

IPC分类号： G05D1/00 ,  G05D1/08 ,  G05D3/00 ,  G05F7/00 ,  G06F17/00 ,  G05D1/06 ,  G08G5/02

CPC分类号： G08G5/025 ,  G05D1/0005 ,  G05D1/0676

摘要： A method and device optimize the vertical trajectory of an aircraft in flight along a predetermined approach trajectory. The method and device include the use of a calculator, which is structured to predict a predicted stabilization altitude at which the aircraft will reach a setpoint approach speed as a function of the current aircraft parameter values, a theoretical vertical trajectory, and predetermined models of aerodynamic efficiency of the aircraft. A comparator is structured to determine absolute value differences between the predicted stabilization altitude and the setpoint stabilization altitude and to compare the differences against a predetermined altitude threshold. A vertical trajectory determination unit is structured to determine an optimized vertical trajectory as a function of the current aircraft parameter values, auxiliary parameter values corresponding to a final approach axis, and the absolute value differences between the predicted stabilization altitude and the setpoint stabilization altitude.

摘要翻译： 一种方法和装置沿着预定的进场轨迹优化飞行中飞行器的垂直轨迹。 该方法和装置包括使用计算器，其被构造为预测飞机将达到设定点进近速度的预测的稳定高度，作为当前飞行器参数值，理论垂直轨迹和预定的空气动力学模型的函数 飞机的效率。 结构化比较器以确定预测的稳定高度和设定点稳定高度之间的绝对值差异，并将差异与预定高度阈值进行比较。 垂直轨迹确定单元被构造为根据当前飞机参数值，对应于最终进近轴的辅助参数值以及预测的稳定高度和设定点稳定高度之间的绝对值差来确定优化的垂直轨迹。

公开(公告)号：US08165735B2

公开(公告)日：2012-04-24

申请号：US12062073

申请日：2008-04-03

申请人： Florian Constans

发明人： Florian Constans

IPC分类号： G60G7/70

CPC分类号： G08G5/025 ,  G05D1/0676

摘要： A method to assist in the landing of an airplane in its final flight phase, following a current approach path toward a runway, includes determining at a given flight point, a landing delay margin, called MRAmax, corresponding to an estimated delay during which the braking actions must be undertaken, after the wheels touch down, to enable the airplane to stop on the runway. A device includes equipment for acquiring parameters necessary to perform the method of assisting the landing of the airplane, a computer to determine the landing delay margin MRAmax from the parameters, and a display for presenting the information to alert the crew.

摘要翻译： 一种辅助飞机在其最终飞行阶段着陆的方法，在当前进入跑道的路径之后，包括在给定的飞行点确定称为MRAmax的着陆延迟余量，对应于估计的延迟，其中制动 在轮子碰到后，必须采取行动，使飞机停在跑道上。 装置包括用于获取执行辅助飞机着陆的方法所必需的参数的设备，计算机根据参数确定着陆延迟余量MRAmax，以及用于呈现提醒机组人员的信息的显示器。

公开(公告)号：US08224506B2

公开(公告)日：2012-07-17

申请号：US12021252

申请日：2008-01-28

申请人： Florian Constans

发明人： Florian Constans

IPC分类号： G06F7/70 ,  G01C19/00

CPC分类号： G08G5/025 ,  G01C23/00

摘要： A method of determining and utilizing a maximum stabilization height of a moving airplane includes: determining a nominal total height at any point of the nominal path of the airplane, determining a total height of the airplane, determining a nominal maximum total height that the airplane is able to reach from its current position corresponding to a nominal total height and according to an optimum total height variation law, determining the maximum stabilization height corresponding to the nominal maximum total height that the airplane is able to reach, and determining whether to continue or to interrupt a landing procedure during the final flight phase of the airplane based on the determined maximum stabilization height.

摘要翻译： 确定和利用移动飞机的最大稳定高度的方法包括：确定在飞机的标称路径的任何点的标称总高度，确定飞机的总高度，确定飞机的标称最大总高度 能够从对应于标称总高度的当前位置到达，并且根据最佳总高度变化规律，确定对应于飞机能够到达的标称最大总高度的最大稳定高度，以及确定是否继续 基于确定的最大稳定高度，在飞机的最终飞行阶段期间中断着陆程序。

公开(公告)号：US08948937B2

公开(公告)日：2015-02-03

申请号：US13559325

申请日：2012-07-26

申请人： Florian Constans ,  Mickael Lefebvre

发明人： Florian Constans ,  Mickael Lefebvre

IPC分类号： G06F7/70 ,  G05D1/10 ,  G08G5/00 ,  G05D1/00 ,  G01C23/00

CPC分类号： G05D1/101 ,  G01C23/00 ,  G01C23/005 ,  G05D1/0005 ,  G05D1/0077 ,  G08G5/0013 ,  G08G5/0021

摘要： Method and device for an optimal management of the energy of an aircraft.The device (1) includes means (5) for determining, in an iterative manner, according to a predicted energy state and according to a management strategy, optimal commands of means (S1,S2, S3, S4, S5, S6) for controlling the energy of the aircraft, which allow the aircraft to reach a given point of a trajectory in a given operational state.

摘要翻译： 用于飞机能量的最佳管理的方法和装置。 装置（1）包括用于根据预测能量状态和根据管理策略以迭代方式确定用于控制的装置（S1，S2，S3，S4，S5，S6）的最佳命令的装置（5） 飞机的能量，使得飞机能够达到给定操作状态下轨迹的给定点。

公开(公告)号：US07952492B2

公开(公告)日：2011-05-31

申请号：US12304451

申请日：2007-06-07

申请人： Florian Constans

发明人： Florian Constans

IPC分类号： G01C23/00 ,  G05D1/12

CPC分类号： G05D1/0676

摘要： A landing assistance device and method for an aircraft according to the invention, based on the landing procedure rules attached to the runway, a lower threshold and an upper threshold of total energy acceptable for the aircraft are determined and the current total energy of the latter is compared with the thresholds.

摘要翻译： 根据本发明的飞机的着陆辅助装置和方法，基于附接到跑道的着陆程序规则，确定飞行器可接受的总能量的下阈值和上限阈值，并且后者的当前总能量 与门槛相比。

公开(公告)号：US20090195413A1

公开(公告)日：2009-08-06

申请号：US12304451

申请日：2007-06-07

申请人： Florian Constans

发明人： Florian Constans

IPC分类号： G01C23/00

CPC分类号： G05D1/0676

摘要： A landing assistance device and method for an aircraft. According to the invention, based on the landing procedure rules attached to the runway (2), a lower threshold and an upper threshold of total energy acceptable for the aircraft (1) are determined and the current total energy of the latter is compared with said thresholds.

摘要翻译： 飞机的着陆辅助装置和方法。 根据本发明，基于附接到跑道（2）的着陆程序规则，确定飞机（1）可接受的总能量的下阈值和上限阈值，并将后者的当前总能量与所述 阈值。