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1.发明授权公开(公告)号：US07761193B2
公开(公告)日：2010-07-20
申请号：US11128299
申请日：2005-05-13
申请人： Franck Artini , Jean-Pierre Demortier , Christophe Bouchet , Jacques Espinasse , Edward Strongman
发明人： Franck Artini , Jean-Pierre Demortier , Christophe Bouchet , Jacques Espinasse , Edward Strongman
IPC分类号： G01C23/00 , G05D1/00 , G05D3/00 , G06F7/00 , G06F17/00 , G05D1/08 , G05D1/06 , G01C5/00 , G01C21/00 , G06F19/00 , G06G7/70 , G08B21/00 , G08B23/00
CPC分类号： G05D1/0646 , G01C5/005
摘要： Method and device for ensuring the safety of a low-altitude flight of an aircraft.A device (1) for ensuring the safety of a low-altitude flight comprises information sources (5) able to determine current flight conditions, a monitoring unit (6) for realizing, with the aid of said current flight conditions, a function for global and autonomous monitoring of said low-altitude flight of the aircraft, making it possible to preserve the integrity of said aircraft during said flight, and means (13) for presenting the results of the monitoring function realized by said monitoring unit (6) to an operator.
摘要翻译： 确保飞机低空飞行安全的方法和装置。 一种用于确保低空飞行的安全性的装置（1）包括能够确定当前飞行情况的信息源（5），用于在所述当前飞行条件的帮助下实现全局的功能的监视单元（6） 以及对所述飞机的所述低空飞行进行自主监视，使得能够在所述飞行期间保持所述飞行器的完整性;以及用于将由所述监视单元（6）实现的监视功能的结果呈现给 操作员。
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2.发明申请公开(公告)号：US20050261811A1
公开(公告)日：2005-11-24
申请号：US11128299
申请日：2005-05-13
申请人： Franck Artini , Jean-Pierre Demortier , Christophe Bouchet , Jacques Espinasse , Edward Strongman
发明人： Franck Artini , Jean-Pierre Demortier , Christophe Bouchet , Jacques Espinasse , Edward Strongman
CPC分类号： G05D1/0646 , G01C5/005
摘要： Method and device for ensuring the safety of a low-altitude flight of an aircraft. A device (1) for ensuring the safety of a low-altitude flight comprises information sources (5) able to determine current flight conditions, a monitoring unit (6) for realizing, with the aid of said current flight conditions, a function for global and autonomous monitoring of said low-altitude flight of the aircraft, making it possible to preserve the integrity of said aircraft during said flight, and means (13) for presenting the results of the monitoring function realized by said monitoring unit (6) to an operator.
摘要翻译： 确保飞机低空飞行安全的方法和装置。 一种用于确保低空飞行的安全性的装置（1）包括能够确定当前飞行情况的信息源（5），用于在所述当前飞行条件的帮助下实现全局的功能的监视单元（6） 以及对所述飞行器的所述低空飞行进行自主监视，使得能够在所述飞行期间保持所述飞行器的完整性;以及用于将由所述监视单元（6）实现的监视功能的结果呈现给 操作员。
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公开(公告)号：US20050261810A1
公开(公告)日：2005-11-24
申请号：US11128298
申请日：2005-05-13
CPC分类号： G01D7/08
摘要： Flight control indicator for an aircraft. The flight control indicator (1) comprises a set (2) of information sources, a computation unit (3) which determines, on the basis of information emanating from said set (2) of information sources, at least one item of information regarding actual thrust of at least one engine of the aircraft, and a display device (5) which is a head-up display device and which presents, on a display screen (7), at least one means of indication which indicates said item of information regarding actual thrust, which is associated with a thrust scale, and which is presented, with this thrust scale, superimposed on the environment prevailing in front of the aircraft.
摘要翻译： 飞机的飞行控制指示器。 飞行控制指示器（1）包括一组信息源（2），一个计算单元（3），根据从所述信息源集合（2）发出的信息，确定至少一个关于实际信息的信息 至少一个发动机的推力，以及作为平视显示装置的显示装置（5），其在显示屏幕（7）上呈现至少一个指示装置，其指示所述关于 与推力秤相关的实际推力，与该推力秤一起呈现，叠加在飞机前方的环境中。
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4.发明申请公开(公告)号：US20050273221A1
公开(公告)日：2005-12-08
申请号：US11118314
申请日：2005-05-02
CPC分类号： G05D1/0646 , G01C23/00 , G01D7/08
摘要： The flight control indicator (1) comprises a set (2) of information sources, a computation unit (3) connected to said set (2) of information sources and determining, on the basis of information emanating from said set (2) of information sources, at least one maximum total slope of the aircraft, which corresponds to the maximum thrust and is obtained on the basis of the measurement of the current performance of the aircraft, extrapolated to the condition of maximum slope and anticipating an engine fault, and a head-up display device (5) which presents, on a display screen (7), at least one means of indication (8) which indicates said maximum total slope and which is presented superimposed on the environment existing in front of the aircraft.
摘要翻译： 飞行控制指示符（1）包括一组（2）信息源，连接到所述信息源集合（2）的计算单元（3），并且基于从所述信息集（2）发出的信息 来源，飞机的至少一个最大总斜率，其对应于最大推力，并且是基于飞机的当前性能的测量获得的，外推到最大坡度条件并预期发动机故障，以及 在显示屏幕（7）上呈现指示（8）的指示所述最大总斜率并且叠加在飞机前面的环境上的至少一个指示装置（5）的平视显示装置（5）。
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5.发明授权公开(公告)号：US07962254B2
公开(公告)日：2011-06-14
申请号：US11917310
申请日：2006-06-12
IPC分类号： G05D1/08
CPC分类号： G08G5/0021 , G01C23/00 , G05D1/0646 , G08G5/0086 , G08G5/045
摘要： A system determines a limit angle of climb corresponding to a climb angle of an aircraft for flying over the ground along an avoidance path and displays a characteristic sign representing the limit angle of climb on a display screen.
摘要翻译： 系统确定对应于飞行器沿着回避路径飞越地面的爬升角度的极限爬升角度，并且在显示屏幕上显示表示爬升极限角度的特征符号。
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公开(公告)号：US07467030B2
公开(公告)日：2008-12-16
申请号：US11121053
申请日：2005-05-04
IPC分类号： G01C23/00
CPC分类号： G01C23/00
摘要： A flight control indicator for an aircraft includes a central unit that determines a change of vertical or lateral trajectory. A display, which may present a first indicator of a next vertical change and a second indicator of a next lateral change, presents the one of the first and second indicators indicating the change of trajectory which is closest from the current position of the aircraft.
摘要翻译： 飞行器的飞行控制指示器包括确定垂直或横向轨迹变化的中央单元。 可以呈现下一垂直变化的第一指示符和下一横向变化的第二指示符的显示器呈现指示与飞行器当前位置最接近的轨迹变化的第一和第二指示中的一个。
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公开(公告)号：US20050273222A1
公开(公告)日：2005-12-08
申请号：US11121053
申请日：2005-05-04
CPC分类号： G01C23/00
摘要： The flight control indicator (1) comprises a central unit (3) able to determine any change of trajectory corresponding to a vertical change which represents a change of vertical segment or a lateral change which represents a change of lateral branch, and means of display (5) which are able to present, on a viewing screen (7), a first means of indication indicating a next vertical change and a second means of indication indicating a next lateral change, and which are formed in such a way as to present at least one of said first and second means of indication, namely the one indicating the change of trajectory which is closest, from the current position of the aircraft.
摘要翻译： 飞行控制指示器（1）包括中央单元（3），其能够确定对应于垂直变化的任何轨迹变化，所述垂直变化表示垂直段的变化或表示横向分支变化的横向变化，以及显示装置 5），其能够在观察屏幕（7）上呈现指示下一个垂直变化的第一指示装置和指示下一个横向变化的第二指示装置，并且以这样的方式形成： 所述第一和第二指示装置中的至少一个，即指示与飞行器的当前位置最接近的轨迹的变化的指示。
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公开(公告)号：US20080208400A1
公开(公告)日：2008-08-28
申请号：US11917310
申请日：2006-06-12
IPC分类号： G08G5/04
CPC分类号： G08G5/0021 , G01C23/00 , G05D1/0646 , G08G5/0086 , G08G5/045
摘要： The system (1) comprises means (6) for determining a limit angle of climb corresponding to a climb angle of the aircraft for flying over the ground along an avoidance path and means (8) for displaying a characteristic sign representing said limit angle of climb on a display screen (9).
摘要翻译： 系统（1）包括用于确定对应于飞行器沿着回避路径在地面上飞行的爬升角的爬升极限角度的装置（6）和用于显示表示所述极限爬升角度的特征符号的装置（8） 在显示屏幕（9）上。
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公开(公告)号：US07636617B2
公开(公告)日：2009-12-22
申请号：US11128298
申请日：2005-05-13
CPC分类号： G01D7/08
摘要： A flight control indicator for an aircraft has a set of information sources, a computation unit which determines, on the basis of information emanating from the set of information sources, an item of information regarding actual thrust of an engine of the aircraft, and a display device which is a head-up display device and which presents, on a display screen, an indication of the item of information regarding actual thrust. The item of information regarding actual thrust is associated with a thrust scale and both are presented superimposed on the environment prevailing in front of the aircraft.
摘要翻译： 飞行器的飞行控制指示器具有一组信息源，计算单元基于从该组信息源发出的信息，确定关于飞行器的发动机的实际推力的信息项，以及显示器 装置，其是平视显示装置，并且在显示屏幕上呈现关于实际推力的信息项的指示。 关于实际推力的信息项目与推力秤相关联，并且两者都叠加在飞机前面的环境中。
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10.发明授权公开(公告)号：US07089090B2
公开(公告)日：2006-08-08
申请号：US11118314
申请日：2005-05-02
IPC分类号： G01C23/00
CPC分类号： G05D1/0646 , G01C23/00 , G01D7/08
摘要： The flight control indicator may include a set of information sources, a computation unit connected to said set of information sources, and a head-up display device. The computation unit determines, on the basis of information emanating from the set of information sources, at least one maximum total slope of the aircraft. The maximum total slope corresponds to the maximum thrust and is obtained on the basis of the measurement of the current performance of the aircraft, extrapolated to the condition of maximum slope and in anticipation of an engine fault. The head-up display device presents, on a display screen, at least one indicator which indicates the maximum total slope and which is presented superimposed on the environment existing in front of the aircraft.
摘要翻译： 飞行控制指示器可以包括一组信息源，连接到所述一组信息源的计算单元和平视显示装置。 计算单元基于从该组信息源发出的信息确定飞行器的至少一个最大总斜率。 最大总斜率对应于最大推力，并且是基于飞机当前性能的测量，外推到最大坡度条件并预期发动机故障而获得的。 平视显示装置在显示屏幕上呈现至少一个指示器，其指示最大总斜率并且叠加在存在于飞机前面的环境上。
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