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1.发明授权公开(公告)号：US09950806B2
公开(公告)日：2018-04-24
申请号：US15159318
申请日：2016-05-19
CPC分类号： B64D43/00 , B64D45/08 , G01C23/005 , G06T11/00 , G08G5/02
摘要： A method for displaying an outside scene on a cockpit display system. The system comprises two display areas contiguous along a horizontal aircraft axis and a processor to generate the display, on one of the areas, of an initial scene image from data from the aircraft's avionics electronics, the data comprising the aircraft's sideslip angle β. The processor displays, on the scene image, a flight path vector indicating a point on the scene image towards which the aircraft is heading. When the measured angle β exceeds a threshold, the processor displays the initial scene image on a first display area and the display of a supplementary outside scene image, on a second display area, the supplementary scene image representing a lateral extension of the initial scene image. The processor also displays the flight path vector superimposed on one of the two images based on a value of angle β.
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公开(公告)号：US10604270B2
公开(公告)日：2020-03-31
申请号：US15977663
申请日：2018-05-11
摘要： The display system for a cockpit of an aircraft comprises a transparent display device and a display computer. The transparent display device includes a brightness masking device that can be commanded according to at least three predetermined levels of opacity in at least four masking independent zones. The display system includes a brightness sensor. The display computer is configured to determine a level of brightness due to the light source, in display zones corresponding to each of the masking zones, depending on information coming from the brightness sensor; determine an opacity level associated with each of the masking zones, depending on the brightness level determined, such that a higher level of opacity corresponds to a higher level of brightness; and command the opacity level in each of the masking zones of the brightness masking device.
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3.发明申请公开(公告)号：US20160340054A1
公开(公告)日：2016-11-24
申请号：US15159318
申请日：2016-05-19
CPC分类号： B64D43/00 , B64D45/08 , G01C23/005 , G06T11/00 , G08G5/02
摘要： A method for displaying an outside scene on a cockpit display system. The system comprises two display areas contiguous along a horizontal aircraft axis and a processor to generate the display, on one of the areas, of an initial scene image from data from the aircraft's avionics electronics, the data comprising the aircraft's sideslip angle β. The processor displays, on the scene image, a flight path vector indicating a point on the scene image towards which the aircraft is heading. When the measured angle β exceeds a threshold, the processor displays the initial scene image on a first display area and the display of a supplementary outside scene image, on a second display area, the supplementary scene image representing a lateral extension of the initial scene image. The processor also displays the flight path vector superimposed on one of the two images based on a value of angle β.
摘要翻译： 一种用于在驾驶舱显示系统上显示外部场景的方法。 该系统包括沿着水平飞行器轴线连续的两个显示区域和处理器，用于在来自飞行器航空电子设备的数据的一个区域上的一个区域上生成显示器，该数据包括飞行器的侧滑角β。 处理器在场景图像上显示飞行路线矢量，其表示飞机正朝着该方向的场景图像上的点。 当测量角度β超过阈值时，处理器在第一显示区域上显示初始场景图像，并且在第二显示区域上显示辅助场景图像，表示初始场景图像的横向延伸的补充场景图像 。 处理器还基于角度β显示叠加在两个图像之一上的飞行路径向量。
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公开(公告)号：US20130304283A1
公开(公告)日：2013-11-14
申请号：US13886440
申请日：2013-05-03
IPC分类号： B64C19/00
CPC分类号： B64C19/00 , G05D1/0808 , G05D1/101
摘要： A method for controlling the piloting of an aircraft comprising the steps of receiving at least one first instruction for modification of a current velocity vector of the aircraft, determining a target velocity vector of the aircraft, on the basis of said at least one first instruction received, and determining, on the basis at least of said target velocity vector, at least one actuation command intended for at least one actuator of the aircraft in order to modify the movement of the aircraft according to said at least one first instruction received.
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公开(公告)号：US10326985B2
公开(公告)日：2019-06-18
申请号：US15832963
申请日：2017-12-06
IPC分类号： G02B27/01 , H04N13/373 , B64D45/00 , G06F3/01 , H04N13/344 , G02B27/00
摘要： A display system for a cockpit of an aircraft comprises a display device configured to be secured to a user's head in the cockpit of the aircraft. A display computer is configured to control the display of information on the display device. The display computer is configured to determine a distance between the head of the user and an element of the cockpit intersecting with a direction corresponding to a current orientation of the head of the user, when the user looks inside the cockpit, and to control a virtual display distance of the display device, corresponding to the distance between the head of the user and the element of the cockpit.
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公开(公告)号：US09096309B2
公开(公告)日：2015-08-04
申请号：US13886440
申请日：2013-05-03
CPC分类号： B64C19/00 , G05D1/0808 , G05D1/101
摘要： A method for controlling the piloting of an aircraft comprising the steps of receiving at least one first instruction for modification of a current velocity vector of the aircraft, determining a target velocity vector of the aircraft, on the basis of said at least one first instruction received, and determining, on the basis at least of said target velocity vector, at least one actuation command intended for at least one actuator of the aircraft in order to modify the movement of the aircraft according to said at least one first instruction received.
摘要翻译： 一种用于控制飞行员驾驶的方法，包括以下步骤：接收至少一个用于修改飞行器的当前速度矢量的第一指令，基于接收的所述至少一个第一指令来确定飞行器的目标速度矢量 并且至少基于所述目标速度向量确定旨在用于飞机的至少一个致动器的至少一个致动指令，以便根据接收到的所述至少一个第一指令来修改飞机的运动。
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公开(公告)号：US10235777B2
公开(公告)日：2019-03-19
申请号：US15616614
申请日：2017-06-07
摘要： A display system for an aircraft cockpit comprises a display device configured to be secured to a user's head, a sensor to determine an orientation of the user's head, and a display computer. The computer is configured to control the display of information relating to the flight of the aircraft on the display device, to acquire information on the user's head orientation, to determine an angular offset value between a direction corresponding to the head orientation and a longitudinal axis of the aircraft, to evaluate at least one condition as a function of the angular offset value, and to control the display device display in accordance with a first display mode when the condition is verified, this first display mode corresponding to a display comprising at least one aircraft piloting assistance symbol displayed in a conforming manner, and another display mode when the condition is not verified.
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公开(公告)号：US09239461B2
公开(公告)日：2016-01-19
申请号：US14052902
申请日：2013-10-14
CPC分类号： G02B27/0149 , B64D45/00 , G02B27/01 , G02B2027/015 , G02B2027/0161
摘要： An aircraft cockpit comprises a head-up display device comprising a projector and a screen, the screen being placed facing a pilot along a theoretical line of sight of the pilot. The projector is fixed to a side wall of the cockpit, the screen forming a non-zero angle of inclination relative to a plane perpendicular to the theoretical line of sight of the pilot.
摘要翻译： 飞机驾驶舱包括一个平视显示装置，包括一个投影仪和一个屏幕，该屏幕沿着飞行员的理论视线面向飞行员放置。 投影仪固定在驾驶舱的侧壁上，屏幕相对于垂直于飞行员的理论视线的平面形成非零倾角。
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公开(公告)号：US20140104693A1
公开(公告)日：2014-04-17
申请号：US14052902
申请日：2013-10-14
CPC分类号： G02B27/0149 , B64D45/00 , G02B27/01 , G02B2027/015 , G02B2027/0161
摘要： An aircraft cockpit comprises a head-up display device comprising a projector and a screen, the screen being placed facing a pilot along a theoretical line of sight of the pilot. The projector is fixed to a side wall of the cockpit, the screen forming a non-zero angle of inclination relative to a plane perpendicular to the theoretical line of sight of the pilot.
摘要翻译： 飞机驾驶舱包括一个平视显示装置，包括一个投影仪和一个屏幕，该屏幕沿着飞行员的理论视线面向飞行员放置。 投影仪固定在驾驶舱的侧壁上，屏幕相对于垂直于飞行员的理论视线的平面形成非零倾角。
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