• 专利附录
  • 专利说明
  • 权利要求
  • 类似技术
  • 同族专利
  • 引用文献
  • 法律状态
  • 优先权
    • 专利摘要:
    The display system (20) comprises a plurality of screens (18) in a cockpit (3) of the aircraft (1), as well as a control unit (12) configured to control the display according to: a normal display mode, in which the control unit is configured to control the display such that following the occurrence of an event on board the aircraft causing the display of an interactive element in a interaction window, the control unit controls the display of the interaction window on one of the screens of the plurality of screens at least as long as an action of an operator is required on the interactive element ; and - a reconfigured display mode, in which the control unit is configured to control the display, on a second screen having a signaling area (35, 35c), of a display window normally displayed on a first screen in the normal display mode, and for controlling the display of an indication in the signaling zone if the interaction window is not displayed on a screen of the plurality of screens when an action of an operator is required on the interactive element.
    公开号:FR3037136A1
    申请号:FR1555177
    申请日:2015-06-08
    公开日:2016-12-09
    发明作者:Aymeric Perrin；Christine Charbonnier；Nicolas Antoni；Cedric Descheemaeker
    申请人:Airbus Operations SAS；
    IPC主号:
    专利说明:

    [0001] 1 System and method for displaying an aircraft. The invention relates to a system and a method for displaying an aircraft, and to an aircraft comprising such a system. Aircraft, particularly modern transport aircraft, include a control system display system in the cockpit type CDS ("Control and Display System" in English). The CDS system comprises a plurality of screens in the cockpit of the aircraft and a control unit configured to control the display on these screens. In a normal display mode, corresponding in particular to the absence of a failure of a screen, the control unit is configured to control the display of at least one display window on each of the screens. Each display window is allocated to one or more systems of the aircraft, and it can be of fixed or variable size. When an event occurs on board the aircraft for which an action of an operator is necessary (for example an alert), a computer of the aircraft in charge of monitoring the event, for example a FWS (Flight Warning System) type of alert management calculator sends a request to the control unit of the CDS system to display an interactive element in at least one display window. This display window is called the interaction window in the rest of the document. The control unit controls the display of the interaction window comprising the interactive element on one of the cockpit screens, at least as long as an action of an operator is required on the interactive element. Thus, following the occurrence of the event, an operator such as in particular a pilot of the aircraft can perform an action on board the aircraft by acting on the interactive element by means of a man-machine interface of the cockpit. This action corresponds for example to an acknowledgment of an alert or to a modification of the state of a system of the aircraft (eg extinguishing a motor, opening or closing a valve, etc.). The interactive element corresponds for example to a button displayed in the interaction window on which the operator can click. Generally, the interaction window also includes at least one indication allowing the operator to understand the nature of the event.
    [0002] 3037136 2 In the event of a failure of one or more cockpit screens, the control unit controls the display on the other screens, not broken down, according to a reconfigured display mode. Such a display mode is in particular described by the document FR2.892.092. When a failed screen corresponds to a screen on which is displayed, in the normal display mode, a viewing window considered to be a priority, then the display is reconfigured so that this display window is displayed on another screen, not broken down, instead of a viewing window considered less priority. A human-machine interface, for example a push button, connected to the control unit of the CDS system, allows the pilot to display on this other screen other display window (s). Thus, each pilot support on the push button makes it possible to change the display window displayed on this other screen, in a predefined order. The pilot can thus scroll and display all the display windows normally displayed on the different 15 screens of the cockpit in the normal display mode. The activation of the reconfigured display mode may also correspond, in addition to the case of a screen failure, to a voluntary request from the pilot to display, on one of the cockpit screens, a display window normally displayed on a screen. portable device type EFB ("Electronic 20 Flight Bag" in English). The corresponding display window is then displayed instead of a display window normally displayed on this cockpit screen in the normal display mode. When the display is made according to the reconfigured display mode, the interactive element displayed in the interaction window may not be accessible to a pilot of the aircraft if the interaction window is not displayed on a cockpit screen due to the reconfiguration of the display. Indications are given in the cockpit so as to warn the pilot of the occurrence of the event, generally in the form of a visual and / or audible indication: the pilot must then act on the man-machine interface 30 to visualize the interaction window. If the event occurs at a time when the driver's workload is high, the driver may want to perform actions related to that event at a later time. However, in order not to be disturbed by the visual or audible indication while performing other actions, the pilot may sometimes acknowledge this visual or sound indication: he must then memorize the fact that he has received this visual indication. or 3037136 3 so as not to forget to require later display of the interaction window. In addition, the display of the interaction window may require several actions of the driver on the human-machine interface to scroll through several windows until the display of the interaction window and, in addition, the driver do not know in advance how many actions will be needed on this man-machine interface so that the interaction window is displayed on a screen of the cockpit. Indeed, as indicated above, the different display windows that can be displayed on a screen in reconfigured display mode are displayed in a predefined order during successive pilot actions on the man-machine interface, but the pilot does not know this predefined order, especially since it may depend on the number of failed displays in the cockpit and the position of the screen (s) failed. Successive actions on the man-machine interface create an additional workload for the pilot, especially since the pilot must furthermore monitor the appearance of the display of the interaction window as far as he is concerned. do not know in advance on the one hand how many actions are needed on the human-machine interface to get the display of the interaction window and secondly on which screen will be displayed the interaction window .
    [0003] SUMMARY OF THE INVENTION The present invention is intended to provide a solution to these problems. It relates to a display system of an aircraft, this display system comprising a plurality of screens in a cockpit of the aircraft, among which at least a first screen and a second screen, the display system comprising also a control unit configured to control the display on the screens of the plurality of screens in a normal display mode or in a reconfigured display mode, such that: in the normal display mode , the control unit is configured to control the display of at least one display window on each of the screens of the plurality of screens, so that following the occurrence of an event aboard the Since the aircraft causes an interactive element to be displayed in an interaction window, the control unit 303 controls the display of the interaction window on one of the screens of the plurality of screens at least as much. that an action of an operator is r equise on the interactive element; and in the reconfigured display mode, the control unit is configured to control the display on the second screen of the plurality of screens of a display window normally displayed on the first screen in the display. normal display mode. This display system is notable in that the second display has a signaling area and in the reconfigured display mode the control unit is configured to control the display of an indication in the signaling area. if the interaction window is not displayed on a screen of the plurality of screens when an action of an operator is required on the interactive element.
    [0004] Thus, thanks to this system, the pilot of the aircraft is informed that an action on his part is required in the interaction window and that he must do an action to display this interaction window. . Advantageously, the display system comprises a man-machine interface connected to the control unit and, in the reconfigured display mode, the control unit is configured to control the display of the window. interaction when it receives information from the human-machine interface corresponding to an action of an operator on the man-machine interface. Thus, the driver can directly display the interaction window by performing this action on the man-machine interface, without scrolling other display windows on the screen. This therefore saves time and reduces the pilot's workload. In one embodiment, the control unit is configured to control the display of the interaction window on the second screen when it receives the information from the human-machine interface corresponding to an action of an operator on the man-machine interface. Displaying the interaction window on the second screen rather than on another screen improves the ergonomics of the system by allowing the driver to directly view the interaction window without having to search for it on another screen.
    [0005] In a particular embodiment, the signaling zone comprises an interactive element operable by means of the man-machine interface. Thus, the action of the operator on the man-machine interface can then correspond to a pilot action on this interactive element of the signaling zone. The pilot can then act directly on this interactive element of the signaling zone to require the display of the interaction window. This further improves the ergonomics of the display system. In one embodiment, the control unit has a memory containing an ordered list of display windows associated with the second screen in the reconfigured display mode and the control unit is configured to change the display of the second display. display, in the reconfigured display mode, during an action of an operator on the man-machine interface: by displaying on the second screen a consecutive display window, in the ordered list, of a current window displayed during the action of the operator on the human-machine interface, when no action of an operator is required on the interactive element of the interaction window; By displaying on the second screen the interaction window, when an action of an operator is required on this interactive element. Preferably, the ordered list of display windows contains the interaction window. In an advantageous embodiment, the second screen 25 comprises a first display area and a second display area each configured to display at least one display window and the signaling area is arranged between the first display area and the second display area. This embodiment is particularly compatible with the use of large screens in the cockpit, each provided to display several display windows. Advantageously, the signaling zone is configurable to be associated with the first display zone and / or the second display zone. This makes it possible to use a common signaling area for the two display areas and, therefore, to limit the screen area used for the signaling area.
    [0006] In a particular embodiment, the control unit is configured to receive status information from the screens of the plurality of screens and to detect an eventual failure of a screen according to said status information. the control unit is further configured to control the display of the plurality of screens according to the normal display mode in the absence of a display failure and to control the display on the display screens. the plurality of screens according to the reconfigured display mode in case of failure of at least one screen of the plurality of screens. The display system according to the invention is then particularly advantageous in the event of failure of one of the plurality of screens. The invention also relates to an aircraft comprising a display system as mentioned above.
    [0007] The invention also relates to a method of displaying an aircraft whose display system comprises a plurality of screens in a cockpit of the aircraft, among which at least a first screen and a second screen, the a display system also comprising a control unit, wherein the control unit controls the display on the screens of the plurality of screens in a normal display mode or in a reconfigured display mode; such that: in the normal display mode, the control unit controls the display of at least one display window on each of the screens of the plurality of screens, so that following the occurrence of an event on board the aircraft causing the display of an interactive element in an interaction window, the control unit controls the display of the interaction window on one of the screens of the aircraft. plurality of screens at least as long as an acti an operator is required on the interactive element; and in the reconfigured display mode, the control unit controls the display, on the second screen of the plurality of screens, of a display window normally displayed on the first screen in the first mode. normal display. The display method is remarkable in that, the second screen having a signaling area, in the reconfigured display mode the control unit controls the display of an indication in the signaling area if the Interaction window is not displayed on a screen of the plurality of screens when an action of an operator is required on the interactive element.
    [0008] The invention will be better understood on reading the description which follows and on examining the appended figures. Figure 1 schematically illustrates an aircraft with a cockpit. Fig. 2 shows a display system according to an embodiment of the invention. Figures 3 and 4 each illustrate a cockpit screen of the aircraft displaying a signaling area according to embodiments of the invention. FIG. 5 illustrates an example of display on cockpit screens 15 of the aircraft, in a normal display mode. Figure 6 illustrates an example of display on cockpit screens of the aircraft, in a reconfigured display mode. FIG. 7 illustrates an example of successive display of several windows on a cockpit screen of the aircraft, in a reconfigured display mode. FIGS. 8A to 8E illustrate various examples of display in the signaling zone of a cockpit screen, in the reconfigured display mode.
    [0009] The aircraft 1 shown in FIG. 1 comprises a display system 20 as shown in FIG. 2. The display system 20 comprises a display management system 28, for example of the CDS ("Cockpit Display") type. System "). The display management system comprises a control unit 12 and a plurality of display screens 18 (DU for "Display Unit" in English) located in the cockpit 3 of the aircraft. These display screens are connected to the control unit by a set of links 22. The control unit 12 is also connected to a human machine interface device (HMI) 14 by a link 24. The control unit 12 is also connected to a set of avionic computers, including an FWS (Flight Warning System) type of management computer 16 by a link 26. The control unit 12 may for example be located in an avionics bay 2 of the aircraft. It corresponds to an avionics computer or to a function implemented on a modular avionics computer.
    [0010] The plurality of cockpit display screens 18 comprise at least a first display screen and a second display screen. According to one embodiment of the invention, at least the second display screen comprises a display surface 30 in which the display is distributed between a first display area 31 and a signaling area 10 35, such as shown in FIG. 3. In a variant shown in FIG. 4, the display is distributed, in the display surface 30, between the first display area 31, a second display area 32 and the signaling area. 35, the signaling zone 35 being located between the first display area and the second display area.
    [0011] In operation, the control unit 12 controls the display on the screens 18 of the cockpit as a function of information that it receives in particular from avionic computers and as a function of interactions of crew members of the aircraft on the aircraft. 14. The control unit 12 also monitors the operation of the screens 18 via the links 22, so as to detect a possible failure of one of the screens. For this, it is configured to receive status information of the screens of the plurality of screens, via the links 22, and to detect a possible failure of a screen according to said status information. In the absence of a failure of a screen, the control unit controls the display on the screens 18 of the cockpit in a display mode called "normal display mode". In the event of failure of at least the first display screen of the plurality of screens 18 of the cockpit, the control unit controls the display on the other non-faulty screens of the cockpit, according to a display mode called "mode reconfigured display ". In addition to the case of failure of at least one screen, the reconfigured display mode can also be activated following a voluntary request from the pilot, for example to display on one of the cockpit screens, a display window normally displayed on a portable EFB-type device, the corresponding display window then being displayed instead of a display window normally displayed on this cockpit screen in the normal display mode.
    [0012] In the normal display mode, the control unit 12 controls the display of at least one display window on each screen of the plurality of screens 18 of the cockpit. More particularly, when this screen is similar to the second screen and has a first display area 31 and possibly a second display area 32, the control unit 12 controls the display of at least one display window in the first display area 31 and at least one display window in the second display area 32 (when the display includes said second display area). When the alert management computer 16 detects the occurrence of an event on board the aircraft, if the flight procedures provide that this event must be reported to the crew members of the aircraft and requires action by the From a crew member, then the alert management computer 16 sends information relating to this event via the link 26 to the control unit 12. The control unit 12 then controls the display. of an interactive element in an interaction window and it controls the display of the interaction window on one of the screens of the plurality of screens 18 at least as long as an action of an operator is required on the interactive element. Thus, a crew member, for example a pilot of the aircraft, can use the man-machine interface 14 to act on the interactive element so as to perform the required action. The interaction window being displayed on one of the cockpit screens, the pilot can act on the interactive element in this window following the occurrence of the event, without having to make an action to cause the display of the 25 interaction window. In the example shown in FIG. 5, the cockpit of the aircraft comprises four screens 18 whose respective display surfaces 30a, 30b, 30c and 30d each comprise a first display zone (on the left), a second zone display (right) and a signaling area between the first display area and the second display area. In the normal display mode, the control unit 12 controls the display of display windows in the different display areas of the four screens such that: in the display surface 30a, a window of The display displayed in the first display area 35 comprises two sub-windows corresponding to displays of PFD type 3037136 10 ("Primary Flight Display" in English) and SFT ("Slat Flaps and Trim indicator" in English) and, a window the display area displayed in the second display area comprises two sub-windows corresponding to ND ("Navigation Display") and VD ("Vertical 5 Display") type displays; in the display surface 30b, a display window displayed in the first display area comprises two sub-windows corresponding to displays of the ED ("Engine Display") and SD ("System Display") types. ) and, a display window displayed in the second display area comprises two sub-windows 10 corresponding to displays of types MB ("Mail Box" in English) and WD ("Warning Display" in English); in the display surface 30c, a display window displayed in the first display area comprises two sub-windows corresponding to displays of ND ("Navigation Display") and VD ("Vertical Display") types. ) and, a display window displayed in the second display area comprises two sub-windows corresponding to PFD ("Primary Flight Display") and SFT ("Slat Flaps and Trim indicator") displays. ); in the display surface 30d, a display window displayed in the first display area and a display window displayed in the second display area both correspond to MFD displays ("Multi Function Display"). " in English). When an event occurs on board the aircraft, this event is indicated in the WD type sub-window and the interactive element is displayed in this sub-window which then corresponds to the window interaction. In the reconfigured display mode, the control unit 12 is configured to control the display on the second screen of the plurality of screens of a display window normally displayed on the first screen in the mode of operation. normal display. This display window is then displayed on the second screen instead of another display window normally displayed on the second screen in normal display mode. More particularly, the control unit controls the display of said window in the first display area 31 or in the second display area 32 of the second screen. According to a first alternative, the control unit automatically controls the display of said display window 3037136 11 on the second screen following the failure of the first screen. This first alternative corresponds in particular to a case in which this display window is set in the control unit 12 as a priority over the other display window normally displayed on the second screen in normal display mode. According to a second alternative, the control unit controls the display of said display window on the second screen following an action of an operator on the man-machine interface 14 after the failure of the first screen. This second alternative corresponds in particular to a case in which this display window is set in the control unit 12 as less priority compared to the other display window normally displayed on the second screen in normal display mode. . This second alternative is illustrated by the example shown in FIG. 6. This example corresponds to the display illustrated in FIG. 5, when the two central screens are out of order. Therefore, the corresponding display surfaces 30b and 30d are no longer functional and displays of the ED, SD, MB, WD and MFD type are therefore not available. Displays ND, VD, PFD and SFT are set in the control unit 12 as priority over the above types of displays. Consequently, the display windows 20 displayed in the display surfaces 30a and 30c of the non-failed screens remain unchanged after the failure of the two central screens, as long as no action in this direction is performed on the interface. machine man 14 by an operator such as a pilot of the aircraft. In the following description, it is considered that the second screen corresponds to the screen shown on the right in Figure 6, which corresponds to the display surface 30c. When the control unit 12 receives, via the link 24, information from the human machine interface 14 relating to an action of an operator on the man-machine interface 14, the control unit 12 controls a change of the display window displayed in the first display area 31c of the second screen. Successive actions of the operator on the man-machine interface 14 make it possible to control the successive display of the display windows normally displayed on the two central screens in the normal display mode, as represented in FIG. control unit 12 comprises a memory containing an ordered list of display windows 310, 311, 312 and 313 whose display it controls in the first display area 31c, during the successive actions of the operator on Thus, prior to an operator action on the man-machine interface, the display window 310 corresponding to the ND and VD type displays remains displayed in the display area 31c. A first action on the human-machine interface has the effect of replacing the display window 310 by the display window 311 corresponding to the display types ED and SD, as illustrated by the arrow F1. A second action on the man-machine interface has the effect of replacing the display window 311 with the display window 312 corresponding to the display type MFD, as illustrated by the arrow F2. A third action on the human-machine interface has the effect of replacing the display window 312 with the display window 313 corresponding to the display types MB and WD, as illustrated by the arrow F3. A fourth action on the man-machine interface returns to the display of the display window 310 as illustrated by the arrow F4. Following the occurrence of an event on board the aircraft, the control unit 12 controls the display of an indication in the signaling zone 35c of the second screen if the interaction window is not displayed on the screen. a screen of the plurality of screens 18 when an action of an operator is required on the interactive element. FIG. 8B illustrates the display, in the signaling zone 35c, of an ALERT warning indication associated with the display area 31c of the second screen. The operator, in particular a pilot of the aircraft, is thus informed that an event has occurred on board the aircraft and that he must make an action in the interaction window. An action of the operator on the man-machine interface 14 then makes it possible to directly display the display window 313 in the first display area 31c of the second screen, in place of the display window 310. display window 313 contains the WD type display pane corresponding to the interaction window. Consequently, following the occurrence of an event on board the aircraft, it suffices for a single action of the operator to access the display of the interaction window, instead of the three successive actions as illustrated by the arrows F1, F2 and F3 in the example of FIG. 7. The operator can then take note of the event in the interaction window and perform the required action by acting on the interactive element of the interaction window by means of the man-machine interface 14. The action required on the interactive element corresponds, for example, to an acknowledgment of an alert or to a modification of the state of a control system. aircraft (eg extinguishing a motor, opening or closing a valve, etc.). Advantageously, the display attributes of the ALERT warning indication, such as its color or the type of display (fixed or flashing, etc.) depend on an importance of the event parameterized in the control unit 12. For example, the indication may be displayed in red for the most important events and in yellow for the less important events.
    [0013] Various variants are possible for the man-machine interface 14. This may for example correspond to a push button, to a pointing device such as in particular a trackball, to a touch screen, etc. Advantageously, the signaling zone 35c comprises an interactive element operable by means of the man-machine interface 14.
    [0014] When the human machine interface 14 corresponds to a pointing device, this interactive element corresponds to a portion of the signaling area in which an operator can click. When the human machine interface 14 corresponds to a touch screen, the interactive element corresponds to a sensitive surface of the touch screen, this sensitive surface 20 being defined in the signaling zone. As the case may be, the action of the operator on the man-machine interface 14 following which the control unit 12 controls the display of the interaction window then corresponds to an action of clicking on the interactive element or touching the sensitive surface of the interactive element. Acting directly on the interactive element located in the signaling zone to control the display of the interaction window improves ergonomics and reduces the workload of the operator. In an advantageous embodiment, when the control unit 12 controls the display on the cockpit screens according to the reconfigured display mode, the control unit controls the display of an indication in the control zone. signaling 35c, even when an action of an operator is not required on the interactive element. The display of such an indication is illustrated in FIGS. 6, 7 and 8A by the STACK indication intended to inform an operator that a stack of unposted display windows 35 is available for display, these display windows which can be displayed by actions on the man-machine interface 14, as discussed with reference to FIG. 7. This allows the operator to become more aware of the fact that the reconfigured display mode is enabled and that it can request viewing of other display windows by actions on the man-machine interface. In a particular embodiment, the control unit 12 also controls the display of a specific indication in the signaling zone 35c when an unread message, for example from the air traffic control, is displayed in the sub window display type MB when this window is not displayed. This particular embodiment is illustrated in FIG. 8C by the display of the indication MSG in the signaling zone 35c. Preferably, during an action of an operator on the man-machine interface 14 while this MSG indication is displayed, the control unit 12 directly controls the display of the display window 313 comprising the sub-display. MB type display window, to reduce the operator's workload. Advantageously, the MSG indication is displayed in a specific color, for example in blue. When the signaling area is common to two display areas of the same screen, as in the examples shown in FIGS. 4, 5, 6, 7, 8A ...
    [0015] 8E, when it controls the display of an indication in the signaling zone, the control unit also controls the display of a symbol associated with this indication. This symbol is shaped to enable an operator to understand which of the two display areas corresponds to the indication. This symbol may for example correspond to an arrow or triangle pointing to the corresponding display area. Thus, in FIGS. 6, 7, 8A, 8B and 8C, this symbol corresponds to a triangle pointing to the first display area (on the left of the screen) so as to inform an operator that an action on his part on the man-machine interface 14 will have the effect of modifying the display window 30 displayed in the first display area. In FIG. 8D, this symbol corresponds to a triangle pointing to the second display area (on the right of the screen) so as to inform an operator that an action on his part on the man-machine interface 14 will have effect of changing the display window displayed in the second display area.
    [0016] In a particular embodiment shown in FIG. 8E, the signaling zone is provided to allow the simultaneous display of a first indication MSG and a second indication ALERT respectively corresponding to the first display area and to the second display area. A first symbol, corresponding to a triangle pointing to the left, is associated with the first indication and a second symbol, corresponding to a triangle pointing to the right, is associated with the second indication. Advantageously, a first interactive element operable by means of the man-machine interface 14 is associated with the first indication 10 and a second interactive element operable by means of the man-machine interface 14 is associated with the second indication. Thus, an action of an operator on the first interactive element makes it possible to display the MB type display sub-window in the first display area and an action of an operator on the second interactive element allows the display of the interaction window in the second display area.
    权利要求:
    Claims (11)
    [0001]
    CLAIMS1- A display system (20) of an aircraft (1), this display system comprising a plurality of screens (18) in a cockpit (3) of the aircraft, among which at least a first screen and a second screen, the display system also comprising a control unit (12) configured to control the display on the screens of the plurality of screens in a normal display mode or in a reconfigured display mode; such that: in the normal display mode, the control unit is configured to control the display of at least one display window on each of the screens of the plurality of screens, so that following on the occurrence of an event on board the aircraft causing the display of an interactive element in an interaction window, the control unit controls the display of the interaction window on one of the screens of the plurality of screens at least as long as an action of an operator e st required on the interactive element; and in the reconfigured display mode, the control unit is configured to control the display, on the second screen of the plurality of screens, of a display window normally displayed on the first screen in the normal display, the display system being characterized in that the second screen has a signaling area (35, 35c) and in the reconfigured display mode the control unit is configured to control the display an indication in the signaling zone if the interaction window is not displayed on a screen of the plurality of screens when an action of an operator is required on the interactive element.
    [0002]
    2- Display system according to claim 1, characterized in that it comprises a man-machine interface (14) connected to the control unit (12) and, in the reconfigured display mode, the unit of control is configured to control the display of the interaction window when it receives information from the man-machine interface corresponding to an action of an operator on the man-machine interface. 3037136 17
    [0003]
    3- Display system according to claim 2, characterized in that the control unit is configured to control the display of the interaction window on the second screen when it receives the information from the human-machine interface corresponding to an action of an operator on the human-machine interface.
    [0004]
    4- Display system according to any one of claims 2 or 3, characterized in that the signaling area (35, 35c) comprises an interactive element operable by means of the man-machine interface.
    [0005]
    Display system according to one of claims 2 to 4, characterized in that the control unit comprises a memory containing an ordered list of display windows (310, 311, 312, 313) associated with the display. second screen in the reconfigured display mode and the control unit is configured to change the display of the second screen, in the reconfigured display mode, during an action of an operator on the human-machine interface by displaying on the second screen a consecutive display window, in the ordered list, of a current window displayed during the action of the operator on the human-machine interface, when no action of a operator is not required on the interactive element; - by displaying on the second screen the interaction window, when an action of an operator is required on the interactive element. 25
    [0006]
    6. Display system according to claim 5, characterized in that the ordered list of display windows contains the interaction window.
    [0007]
    7- Display system according to any one of the preceding claims, characterized in that the second screen comprises a first display area (31) and a second display area (32) each configured to display at least one display window and the signaling area (35) is arranged between the first display area and the second display area. 35 3037136 18
    [0008]
    8- A display system according to claim 7, characterized in that the signaling area is configurable to be associated with the first display area and / or the second display area. 5
    [0009]
    9- Display system according to any one of the preceding claims, characterized in that the control unit (12) is configured to receive status information from the screens of the plurality of screens (18) and to detect a possible failure of a screen according to said status information, the control unit being further configured to control the display on the screens of the plurality of screens according to the normal display mode in the absence of a screen failure and to control the display on the screens of the plurality of screens according to the reconfigured display mode in case of failure of at least one screen of the plurality of screens. 15
    [0010]
    Aircraft (1) having a display system (20) according to any one of the preceding claims.
    [0011]
    11- A method of displaying an aircraft (1) having a display system (20) comprising a plurality of screens (18) in a cockpit (3) of the aircraft, among which at least one first screen and a second screen, the display system also having a control unit (12), wherein the control unit controls display on the screens of the plurality of screens in a normal display mode or according to a reconfigured display mode, such that: in the normal display mode, the control unit controls the display of at least one display window on each of the screens of the plurality of screens , so that following the occurrence of an event on board the aircraft causing the display of an interactive element in an interaction window, the control unit controls the display of the window 30 of interaction on one of the screens of the plurality of screens at least as long as an action of an operation eur is required on the interactive element; and in the reconfigured display mode, the control unit controls the display, on the second screen of the plurality of screens, of a display window normally displayed on the first screen in the display mode. normal display, the display method being characterized in that, the second screen having a signaling area (35, 35c), in the reconfigured display mode the control unit controls the display of an indication in the signaling zone if the interaction window is not displayed on one of the plurality of screens when an action of an operator is required on the interactive element.
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    同族专利:
    公开号 | 公开日
    CN106249984A|2016-12-21|
    US20160357492A1|2016-12-08|
    FR3037136B1|2017-05-19|
    引用文献:
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    法律状态:
    2016-06-27| PLFP| Fee payment|Year of fee payment: 2 |
    2016-12-09| PLSC| Search report ready|Effective date: 20161209 |
    2017-06-21| PLFP| Fee payment|Year of fee payment: 3 |
    2018-06-26| PLFP| Fee payment|Year of fee payment: 4 |
    2019-06-19| PLFP| Fee payment|Year of fee payment: 5 |
    2021-03-12| ST| Notification of lapse|Effective date: 20210205 |
    优先权:
    申请号 | 申请日 | 专利标题
    FR1555177A|FR3037136B1|2015-06-08|2015-06-08|SYSTEM AND METHOD FOR DISPLAYING AN AIRCRAFT|FR1555177A| FR3037136B1|2015-06-08|2015-06-08|SYSTEM AND METHOD FOR DISPLAYING AN AIRCRAFT|
    US15/167,541| US20160357492A1|2015-06-08|2016-05-27|Display system and method for an aircraft|
    CN201610392272.XA| CN106249984A|2015-06-08|2016-06-06|Display system and method for aircraft|
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