• 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 present invention relates to a device (1) and a method for assisting the piloting of an aircraft (20). Said device (1) comprises at least one touch screen (3, 3 ', 4.4'), a memory (5) containing a database (41, 42, 43), measurement and detection means (6, ) and analysis means (7). Said measurement and detection means (6) and said analysis means (7) determine a current situation of said aircraft (20). Each touch screen (3,3 ', 4,4') ensures the display of two pages of information, at least one main permanent icon (13) independent of said current situation and at least one main contextual icon (11) relating to an event of said current situation. Each touch screen (3, 3 ', 4,4') allows selection and lateral displacement of a main contextual icon (11) to display an information page attached to an event of said current situation. Said touch screen (3, 3 ', 4,4') also allows a selection of a main permanent icon (13) to display a main page of information.
    公开号:FR3045176A1
    申请号:FR1502591
    申请日:2015-12-15
    公开日:2017-06-16
    发明作者:Pelletier Romain Fourneau；Roland Touati；Valerie Juppet
    申请人:Airbus Helicopters SAS；
    IPC主号:
    专利说明:

    Device and method for assisting the piloting of an aircraft
    The present invention is in the field of devices for assisting the piloting of aircraft.
    The present invention relates to a device for assisting the piloting of an aircraft and a method of assisting the piloting of an aircraft.
    During a flight, the crew of an aircraft needs a lot of information, this information concerning, in particular, the progress of the flight, the state of the aircraft as well as the state of the environment of the aircraft. This information is provided by control means, such as flight instruments, and / or display means, such as screens, present on the dashboard of the aircraft. This crew usually includes at least one pilot and one co-pilot. In fact, this information is provided in duplicate and identically, on the one hand to the pilot and on the other hand to the co-pilot of the aircraft.
    In addition, the features and equipment available on board an aircraft are numerous and their number is steadily increasing on new aircraft. Additional information regarding these features and equipment must then also be provided to the crew of the aircraft.
    However, the surface available on the dashboard or in the cockpit of an aircraft for the implementation of control means and display means is limited in particular to maintain sufficient visibility area to the outside of the aircraft. The implementation of these means of control and display must also allow their legibility and accessibility by the pilot and / or the co-pilot of the aircraft.
    On the other hand, the multiplication of these control and display means is accompanied by an increase in the cost and mass associated with these control and display means.
    In addition, the simultaneous provision of a multitude of information to the crew of an aircraft does not necessarily facilitate the management and use of the aircraft. Indeed, the crew can not take notice and simultaneously take into account this multitude of information while remaining focused on the piloting of the aircraft. In addition, in certain emergency situations, it may then be difficult for the crew to quickly find the relevant information or information needed to manage this emergency situation among the multitude of information available to them. Such an emergency situation can be for example a breakdown or a fire at the aircraft equipment such as an engine.
    In addition, the aeronautical regulations require the permanent display of a certain amount of information considered necessary or even essential for the smooth running of a safe flight of an aircraft. This regulatory imposition also limits the space available for displaying other information. Such information is for example the primary control parameters such as attitude, altitude, and speed of the aircraft as well as information describing the operation of the aircraft engine (s) such as pressure and temperature. engine oil.
    On modern aircraft, the pilot and co-pilot usually have screens for displaying various pages of information, respectively. The pilot and co-pilot can independently change the information pages displayed on their respective screens and thus navigate between different pages of information.
    For the sake of simplification, only the term "pilot" will be used hereinafter to designate both the pilot and the co-pilot, the actions of the pilot and co-pilot being identical in the context of the invention.
    These information pages can replace flight instruments conventionally used on an aircraft and provide information on the state of the aircraft or its environment, such as speed, altitude or the attitude of the aircraft. for example. These information pages can also provide information on the progress of the flight or on the operation of the aircraft and that of its equipment.
    These information pages are linked together according to a simple and predefined primary tree. This primary tree corresponds to an organization and classification of information pages in a logical and hierarchical manner using an algorithmic structure of tree and branches. The information pages are classified from main information pages located at a primary level of the primary tree and secondary pages of information located at secondary levels of that primary tree. Thus, each branch of this primary tree starts with a main page of information and continues on one or more secondary levels with secondary pages of information.
    On each main page of information, one or more secondary icons are displayed, each secondary icon corresponding to a secondary information page located on the first secondary level just below the main level of the primary tree and on the branch of that primary tree. main page of information. Thus, the driver may request the display of a secondary information page by selecting a secondary icon.
    Similarly, on each secondary information page, one or more secondary icons are displayed, each secondary icon corresponding to a secondary information page located on a secondary level of the primary tree just below the secondary level of the secondary page. of information displayed and on the branch of this secondary page of information displayed. Thus, the driver may request the display of a secondary information page by selecting a secondary icon.
    In addition, main icons are displayed on each main page of information and on each secondary page of information. Each main icon corresponds to a main information page of the main level of the primary tree. Thus, the driver can request the display of a main page of information at any time of its navigation in the primary tree by selecting a main icon.
    This primary tree thus allows an effective consultation of the information pages according to the classification and the hierarchy of this primary tree. However, the display of a secondary information page is accessible according to a single path in this primary tree from a single main page of information.
    In fact, the pilot must return by displaying a main page of information to successively consult two secondary pages of information that are not located on the same branch of the primary tree. This operation may require more or less time especially if the secondary information page is at the end of a branch.
    Indeed, this primary tree is defined in order to offer a compromise between the depth of the primary tree, that is to say the number of secondary levels, and the number of links directly available on each main or secondary page. information, that is, the number of secondary permanent icons displayed on each information page. The classification and prioritization of the primary tree and possibly the content of the main and secondary pages of information are defined for example from a vision of the aircraft system, a functional vision of the aircraft or else operational tasks to be performed for this aircraft. This primary tree can hardly take into account all these constraints simultaneously. As a result, the navigation between the main and secondary pages of information can be optimized according to a single use corresponding to the primary tree, for example according to a vision of the aircraft system, but this navigation will be more tedious and more laborious if the pilot wishes to navigate among these information pages according to a functional vision of the aircraft or according to the accomplishment of the operational tasks of this aircraft.
    In particular, many selection actions by the pilot through the primary tree can be imposed when the driver wants to display a secondary information page located on a branch different from the secondary information page displayed. In addition, this risk increases with the increase in the number of secondary pages of information related to the introduction of new functions and / or new equipment into the aircraft.
    In addition, much of the information necessary for the operation of the aircraft and its equipment is present only in flight manuals and / or use of the aircraft and its equipment. These manuals are available today in paper form or in electronic form, but without connection with the display means of the aircraft. As a result, this information can not generally be displayed in the form of information pages on the display means of the aircraft.
    These flight manuals and / or use contain for example descriptive cards of the equipment of the aircraft and their operation. These flight and / or use manuals also contain information relating to the management of certain flight situations or in the event of incidents, for example a breakdown or a fire of one or more equipment, this information containing inter alia procedures to be followed and / or lists of tasks to be performed.
    In fact, if the pilot has any doubt or hesitation about the operation of an equipment or the procedure to be followed and the tasks to be performed in the event of a flight situation or an incident, the pilot must consult, for example, the manual of the aircraft during the flight to find relevant information regarding this situation or incident. This search can be long and tedious among the many pages of the manual and delay for example the establishment of an emergency procedure. This search can be made easier and faster on an electronic version of the flight manual, without all relevant information being found immediately.
    However, document EP 0580474 describes a method and a device that provide the crew of an aircraft with information adapted to the current situation of the aircraft. This information comes from a database that contains a large amount of information contained in documents generally present in paper form in the aircraft. These documents are for example flight manuals, the maintenance manual and maps.
    This method and this device ensures the acquisition in real time of an event relating to the current situation of the aircraft, the preselection of the information of the database most adapted to this current situation of the aircraft and their possible classification in order of relevance. The pilot can then use this adapted and relevant information vis-à-vis the current situation of the aircraft on a screen.
    The object of the present invention is to overcome the limitations mentioned above and to propose a device for assisting the piloting of an aircraft and a method for assisting the piloting of an aircraft making it possible to navigate in quick, efficient ways. and relevant between the main and secondary pages of information available in a database according to the current situation of the aircraft.
    In this context, the present invention relates to a device for assisting the piloting of an aircraft comprising: at least one processor, at least one display means, a selection means for each display means, at least one memory containing at least one database, means for measuring and detecting, and at least one means of analysis.
    This device for assisting the piloting of an aircraft according to the invention is intended for aircraft and in particular for rotary wing aircraft.
    The measuring and detection means are elements usually present in an aircraft to determine in particular the operating state of the aircraft and that of its equipment. The measurement and detection means are for example sensors for determining the speed relative to the air, the altitude or the attitude of the aircraft. The measurement and detection means can also be sensors measuring the temperature at the level of a motor or that of a mechanical power transmission of the aircraft as well as the consumption of electric current or the hydraulic pressure of the engine. 'an equipment. The measuring and detection means may also include a satellite receiver for determining the speed relative to the ground and the position of the aircraft in a terrestrial reference.
    These measurement and detection means may be dedicated to the device for assisting the piloting of an aircraft according to the invention and form part of this device for assisting the piloting of an aircraft. This device for assisting the piloting of an aircraft may also use measurement and detection means present in the aircraft and then share them with other aircraft equipment such as avionics equipment.
    The device for assisting the piloting of an aircraft according to the invention may comprise one or more memories storing one or more databases. A first database is for example main and secondary pages of information that can be displayed on one of the display means. These main and secondary pages of information can be classified and prioritized according to a primary tree. Another database may be the flight plan of the aircraft containing in particular the coordinates of navigation points of the planned route and the planned landing point. Another database may also be constituted by maps of the areas overflown by the aircraft including, for example, the terrain, the potential obstacles as well as the lands or landing platforms available.
    Each display means may be a screen positioned on the dashboard of the aircraft. Preferably, each display means is a touch screen advantageously integrating the selection means relative to this display means. However, the selection means may be a computer mouse or a touchpad. A pointer is then displayed on the display means, and then moved according to the movements of the computer mouse or the pilot's finger on the touchpad, this display and displacement of the pointer being defined in a known manner via the processor. .
    This device for assisting the piloting of an aircraft according to the invention is remarkable in that: the measurement and detection means and at least one analysis means determine a current situation of the aircraft, at least one display means displays two pages of information and at least one main contextual icon, each main contextual icon corresponding to an event of the current situation of the aircraft, and the selection means relating to the display means on which at least one main contextual icon is displayed allows selection and lateral displacement of a main contextual icon on the display means to display on this display means an information page related to the main contextual icon selected and attached to an event the current situation of the aircraft.
    Each analysis means uses in real time the measurements and / or the information provided by the measurement and detection means in order to determine a current situation of the aircraft.
    An analysis means can thus determine the flight phase of the aircraft using, for example, the speed, the altitude and the attitude of the aircraft. The flight phase of the aircraft, such as a take-off phase, a cruise flight, a hover or a landing phase, thus constitute an event of the current situation of the aircraft. An event of the current situation of the aircraft may also be a change of flight phase.
    An analysis means may also use the flight plan stored in a memory of the device according to the invention in order to define the progress of the flight of the aircraft with respect to this flight plan. An event of the current situation of the aircraft can thus be a passage to a navigation point of this flight plan or a spacing of the aircraft a significant distance from the route provided by the flight plan.
    An analysis means can also determine, by means of the measurements and information provided by the measuring and detection means, an abnormal evolution of the current situation of the aircraft, in particular in the event of an incident or breakdown of a aircraft equipment. An event of the current situation of the aircraft may for example be an abnormal variation such as a drop in the hydraulic pressure or the power consumption of an equipment. An event of the current situation of the aircraft may also be a fault detected on aircraft equipment or a fire on an area of the aircraft such as an engine compartment.
    Each analysis means may use at least one database stored in a memory of the device according to the invention and compare the measurements and the information provided by the measurement and detection means with the contents of a database to determine the current situation of the aircraft and the appearance of an event of this current situation of the aircraft.
    The device for assisting the piloting of an aircraft may comprise a single means of analysis.
    The device for assisting the piloting of an aircraft can comprise several identical analysis means and used in parallel in order to overcome a failure of one of these analysis means.
    The device for assisting the piloting of an aircraft may comprise several different and complementary means of analysis, each analysis means being dedicated to specific situations. A first analysis means for example determines the flight phase of the aircraft and a second analysis means is dedicated to the detection of incidents and failures.
    This device for assisting the piloting of an aircraft makes it possible for at least one display means to display two pages of information and at least one main contextual icon. The two pages of information are derived from the first database stored in a memory of the device for assisting the piloting of an aircraft according to the invention.
    Advantageously, each main contextual icon corresponds to an event of the current situation of the aircraft determined in real time by an analysis means.
    A main contextual icon can be displayed for each event of the current situation detected according to a pre-established list of events.
    A main contextual icon may be a main contextual operating icon when the event to which it is attached relates to the normal flight of the aircraft. A main contextual operating icon is for example attached to the progress of the aircraft on the route provided by the flight plan or to a change of flight phase for example to enter a landing phase. A main contextual operating icon can also be attached to aircraft equipment whose availability depends on the flight phase of the aircraft. For example, when an event of the current situation of the aircraft is the hovering of the aircraft and the aircraft comprises a hoist equipment, a main contextual operating icon corresponding to the hoist function is displayed on the display means, this function being usable only in hovering.
    A main contextual icon may also be a main contextual alert icon when the event to which it is attached relates to an incident or a failure of essential equipment of the aircraft. Equipment is considered essential if a failure of this equipment may jeopardize the safety of the flight of the aircraft. Essential equipment is for example a motor, the main rotor or the retractable landing gear. A main alert popup icon may be represented in a particular form or with a particular color in order to be easily identifiable by the pilot of the aircraft.
    The pilot can then through the selection means relating to this display means, then select and laterally move a main contextual icon. The pilot in fact selects this main contextual icon via the selection means and uses the selection means to move this main contextual icon on the display means. This main contextual icon is actually moved on the display means in a known manner via the processor according to the action of the driver on the selection means. If the display means and the selection means are grouped together to form a touch screen, the pilot presses the touch screen on the main contextual icon with one finger and then moves his finger on the touch screen to move the context icon. main.
    The pilot thus moves the main contextual icon laterally on one of the information pages displayed and the device for assisting the piloting of an aircraft according to the invention then displays a new information page linked to the main contextual icon selected. . This new information page related to the main contextual icon selected is displayed instead of the information page previously displayed on the display means.
    This new information page comes from the first database. Advantageously, this new information page is linked to the main contextual icon selected and is therefore attached to the event attached to this main contextual icon selected. The pilot can thus easily and quickly consult an information page relating to an event of the current situation of the aircraft.
    In addition, after the selection of a main contextual icon and the display of the new information page related to the selected main contextual icon, this device for assisting the piloting of an aircraft allows this display means to display at least one secondary popup icon. Each secondary contextual icon also corresponds to the event of the current situation of the aircraft to which the selected main contextual icon is attached.
    The driver can then through the selection means relating to this display means, select a secondary context icon. The device for assisting the piloting of an aircraft according to the invention then displays an information page linked to the selected secondary contextual icon. This information page related to the selected secondary contextual icon is displayed instead of the previously displayed information page related to the previously selected main contextual icon. In addition, each of the other secondary contextual icons previously displayed are also displayed simultaneously with the information page.
    The main and secondary contextual icons preferably make it possible to display secondary pages of information in order to check, for example, the state, the characteristics or the operation of an equipment of the aircraft relating to an event of the current situation of the aircraft. the aircraft. Several contextual links have been previously created to secondary pages of information, each contextual link being linked to a contextual icon and therefore attached to an event of the current situation of the aircraft.
    Thus, for a predetermined event of the current situation of the aircraft, a main contextual link is established to a secondary page of information. This secondary page of information is considered as the most relevant information page to communicate first to the pilot of the aircraft to take into account and / or treat this event. A main contextual icon is then linked to this main contextual link.
    Then one or more secondary contextual links are established between this secondary page of information related to the main contextual link and one or more secondary pages of information. These secondary information pages are also relevant to allow the pilot to take into account and / or treat this event. A secondary contextual icon is then linked to each secondary contextual link.
    In this way, an event of the current situation of the aircraft is associated with only one main contextual icon and at least one secondary contextual icon.
    The secondary information pages are derived from the first database and contain information that is traditionally displayed on the aircraft screens. This information relates in particular to the progress of the flight, the state of the aircraft and the state of the environment of the aircraft.
    Advantageously, the secondary information pages may also be complementary information from another database. This additional information is for example the content of flight manuals and use of the aircraft and its equipment. This additional information can also be derived from aircraft maintenance manuals, for example to check the date and the content of the last maintenance operation performed on a piece of equipment.
    This additional information may also be the list of tasks to be performed and / or procedures to be followed depending on an event of the current situation of the aircraft. For example, the procedure to follow and the list of tasks to be performed in the event of a fire in the engine compartment during a flight of the aircraft.
    In addition, this additional information can also be added to the first database.
    The main and secondary contextual icons allow the pilot of the aircraft to display very quickly and at the right moment the appropriate and relevant information necessary for the management of the events of the current situation of the aircraft among the multitude of information provided. at his disposal. These events of the current situation of the aircraft can be ben ben the appearance of abnormal events such as a breakdown or an incident on an aircraft equipment or a change of operational phases of the flight of the aircraft.
    In addition, the display means may also display at least one main permanent icon regardless of the current situation of the aircraft. Each main permanent icon is for example relative to a state, measurements or the position of the aircraft. The selection means relating to this display means then allows selection and lateral displacement of a main permanent icon to display on the display means a main page of information related to the main permanent icon selected.
    The pilot thus moves the main contextual icon on one of the information pages previously displayed and the device for assisting the piloting of an aircraft according to the invention then displays the main information page linked to the main permanent icon selected. . This main page of information related to the main permanent icon selected is displayed instead of the information page previously displayed on the display means.
    In addition, the display means may display at least one secondary permanent icon regardless of the current situation of the aircraft. The selection means relating to this display means then makes it possible to select a secondary permanent icon in order to display a secondary information page corresponding to the selected secondary permanent icon as well as possibly at least one secondary permanent icon. Each secondary permanent icon is relative to the main information page or to the displayed secondary information page The secondary information page related to the selected secondary permanent icon is displayed instead of the previously displayed information page.
    The primary and secondary permanent icons are in fact linked to permanent links of a primary tree of the main and secondary pages of information.
    This simple and predefined primary tree corresponds to an organization and classification of the main and secondary information pages in a logical and hierarchical manner as traditionally used in an aircraft. The information pages are classified from main information pages located at a primary level of the primary tree and secondary pages of information located at secondary levels of that primary tree.
    Permanent main links provide access to the main pages of information. A main permanent link is linked to a single main page of information and a main page of information is linked to a single main permanent link. Secondary permanent links connect the main pages of information to secondary pages of information as well as secondary pages of information between them.
    On the other hand, a main page of information can be linked by several permanent links secondary to several secondary pages of information whereas a secondary page of information is connected by a single secondary permanent link to a single main information page. Similarly, a secondary information page located at a secondary level n can be connected by several secondary links secondary to other secondary pages of information located at an upper secondary level n + 1. Conversely, a secondary information page located at a secondary level is connected by a single secondary permanent link to a single secondary information page located at a lower secondary level n-1.
    Two pages of information can therefore be linked to each other on the one hand by a main permanent or secondary link and on the other hand by a main or secondary contextual link. However, the permanent and contextual links are independent.
    A main permanent link necessarily links to a main page of information at the origin of the tree. A secondary permanent link can link on the one hand a main page of information to a secondary information page located at the first secondary level and secondly two secondary pages of information located at two successive secondary levels.
    On the other hand, a main contextual link and a secondary contextual link connect two pages of information, preferably two secondary pages of information, whatever their secondary levels. These two secondary pages of information can in particular be on the same secondary level or on two non-successive secondary levels.
    Primary and secondary permanent links as well as primary and secondary contextual links can be stored with the information pages in the first database.
    Preferably, the primary and secondary permanent links are grouped together in a first library while the main and secondary contextual links are grouped in a plurality of second libraries. Advantageously, each second library of contextual links is thus attached to an event of the current situation of the aircraft and an event is attached to a single second library. In this way, each second library has a single main contextual link and one or more secondary contextual links.
    The first library may also include the main permanent icons and secondary permanent icons that are attached to these primary and secondary permanent links. Thus, the permanent links of the first library allow a structured and hierarchical navigation on the one hand between each main permanent icon and each main page of information and secondly between each secondary permanent icon and each secondary page of information.
    Similarly, the second libraries may also include the main contextual icons and secondary contextual icons that are attached to these primary and secondary contextual links. Thus, the contextual links of each second library allow a quick and relevant navigation on the one hand between each main contextual icon and a relevant information page and secondly between each secondary contextual icon and a relevant information page depending events of the current situation of the aircraft.
    A memory of the device for assisting the piloting of an aircraft according to the invention thus contains the first permanent link library and the second contextual link libraries, the first library and the second libraries that can be stored in the same database or well in two dedicated databases.
    The main and secondary permanent links as well as the main and secondary contextual links are preferably created when the pages of information are placed in the memory of the aircraft flight assistance device according to the invention. These contextual permanent links can also be modified during an update of the information pages or during modifications of the equipment of the aircraft.
    Moreover, a display means may be allocated to several users, namely the pilot and the co-pilot, advantageously allowing this visualization means to be shared between these users. In this case, the use of a tactile visualization means makes it possible to use the device for assisting the piloting of an aircraft according to the invention as well by the pilot or the co-pilot without having to exchange means. selection means, this selection means being integrated with the display means.
    In this way, the information pages are shared by the pilot and the co-pilot, thus limiting the number of visualization means necessary for the efficient and safe management of the flight of the aircraft by the pilot and the co-pilot.
    In addition, the main contextual icons and, if appropriate, the main permanent icons are preferably displayed on the display means in a column located between the two information pages. This arrangement advantageously allows the pilot and co-pilot to easily select these icons while limiting their surface on the display means, each icon being displayed uniquely. As a result, most of the surface of the display means can be used for displaying the two pages of information.
    Each secondary permanent icon is displayed preferably on a main page of information and / or on a secondary page of information. Likewise, each secondary contextual icon is preferably displayed on a secondary information page. Thus, this column groups only the main permanent and contextual icons while the secondary and secondary contextual icons are displayed directly on an information page. The distinction is thus well defined without risk of error between on the one hand the main permanent and contextual icons and secondly the secondary permanent and contextual icons.
    When displaying an information page relating to an event of the current situation of the aircraft, a selection of this column followed by a lateral displacement of this column by means of the selection means allows the side-by-side display of two pages of information related to this event. The pilot can advantageously consult simultaneously two pages of information relating to this event.
    In addition, the display of certain pages of information can be enlarged by selecting and then moving the column laterally. This is particularly the case when the information page is displayed following the selection of a main or secondary permanent icon or when the information page represents the position of the aircraft on a map or a representation of the environment of the aircraft. This can also be the case when the information page is a view of a camera outside the aircraft.
    The present invention also relates to a method of assisting the piloting of an aircraft. This aircraft comprises in particular at least one processor, at least one display means, a selection means for each display means, at least one memory containing at least one database, measurement and detection means, and at least one means of analysis.
    This method of assisting the piloting of an aircraft according to the invention can also be implemented by the device for assisting the piloting of an aircraft previously described which then comprises this aircraft.
    This method of assisting the piloting of an aircraft comprises the following steps enabling: the display of two pages of information on a display means, the determination of a current situation of the aircraft, the display on the means for displaying at least one main contextual icon relating to the current situation of the aircraft, each main contextual icon being relative to an event of this current situation of the aircraft, -the selection and the lateral displacement of a main contextual icon, -the display on the display means of an information page corresponding to the event attached to the selected main contextual icon.
    The method of assisting the piloting of an aircraft according to the invention may also comprise the following complementary steps allowing: displaying on the display means at least one secondary contextual icon, each secondary contextual icon corresponding to the event of the current situation of the aircraft to which is attached the main contextual icon selected, -the selection of a secondary contextual icon and -the display on the display means of an information page corresponding to the icon secondary context selected as well as at least one of the secondary contextual icons.
    The method of assisting the piloting of an aircraft according to the invention may also comprise the following complementary steps allowing: displaying on the display means at least one main permanent icon regardless of the current situation of the aircraft , the selection of a main permanent icon, and the display on the display means of a main page of information related to the main permanent icon selected.
    The method of assisting the piloting of an aircraft according to the invention may also include the following complementary steps enabling: the display on the display means of at least one secondary permanent icon regardless of the current situation of the aircraft each secondary permanent icon being relative to the main information page or to the displayed secondary information page, -selecting a secondary permanent icon and -displaying on the display means of a secondary page of information corresponding to the selected secondary permanent icon as well as possibly at least one of the other secondary permanent icons.
    The method of assisting the piloting of an aircraft according to the invention may also include a preliminary step of creating primary and secondary contextual links and permanent main and secondary links. The primary and secondary permanent links are grouped into a first library and the main and secondary contextual links are grouped into a plurality of second libraries. Each second library of contextual links is attached to an event that may be encountered by the aircraft.
    The main and secondary contextual links are attached to events of the current situation of the aircraft while the main and secondary permanent links are independent of these events of the current situation of the aircraft. In addition, the primary and secondary permanent links are linked to the information pages according to a primary tree while the main and secondary contextual links are linked to these pages of information independently of this primary tree. In addition, each information page is linked to at least one main or secondary permanent link while only certain pages of information may be linked to one or more main and / or secondary contextual links. The invention and its advantages will appear in more detail in the context of the description which follows with exemplary embodiments given by way of illustration with reference to the appended figures which represent: FIG. 1, an aircraft equipped with a device for pilot assistance, FIG. 2, a representation of the information pages according to a primary tree structure, FIG. 3, a representation of the information pages according to a primary tree structure and with contextual links, and FIGS. two schematic diagrams of a method of assisting the piloting of an aircraft, FIGS. 6 to 9, views of the display of a display means.
    The elements present in several separate figures are assigned a single reference.
    FIG. 1 represents an aircraft 20 comprising a fuselage 21, a main rotor 22, a rear rotor 23, a mechanical power transmission box 24 and a motor 25. This aircraft 1 also comprises a dashboard 8 and a device 1 of piloting assistance. This pilot assistance device 1 comprises a processor 2, two touch screens 3,3 'positioned on the dashboard 8 and each incorporating a selection means 4,4', a memory 5, measurement and detection means 6 and an analysis means 7. The memory 5 stores several databases 41,42,43.
    This device 1 to assist the piloting of an aircraft is capable of implementing a method of assisting the piloting of the aircraft 20. Two block diagrams of such methods are shown in FIGS. 2 and 3.
    According to FIG. 2, this method of assisting the piloting of the aircraft 20 comprises five steps taking place sequentially.
    During a first step 51 of displaying two main pages 101-104 and / or secondary 111-139 information, two main pages 101-104 and / or secondary 111-139 information are displayed on one of the two touch screens 3,3 'as shown in Figures 6 and 7. In Figure 6, two main pages of information 101-104 are respectively displayed in a window 16 and in a window 17. In Figure 7, a page 101-104 is displayed in the window 16 and a secondary information page 111-139 is displayed in the window 17.
    The touch screens 3,3 'are preferably positioned in the center of the dashboard 8 and can thus be shared between the pilot and the co-pilot of the aircraft 20. The pilot and the co-pilot can thus take cognizance simultaneously of these main pages 101 -104 and / or secondary 111-139 information.
    These main pages 101-104 and 111-139 of information are located in a first database 41 stored in the memory 5. These main pages 101-104 and 111-139 secondary information contain many information necessary for the management of the flight of the aircraft 20 and the operation of its equipment 21-25. These information pages 101-104, 111-139 may in particular replace flight instruments conventionally used and provide information on the state of the aircraft 20, its equipment 21-25 or its environment.
    Moreover, this information is used traditionally in aircraft and displayed on the screens of the dashboard of these aircraft. This information is classically classified and prioritized according to a simple and predefined primary tree.
    In addition, as part of this method of assisting the piloting of the aircraft 20, the secondary information pages 111-139 also include additional information such as the contents of the flight manual and the user manual of the aircraft. aircraft 20 and its equipment 21-25. This additional information may also be the list of tasks to be performed and / or procedures to be followed according to an event of the current situation of the aircraft 20.
    These main pages 101-104 and secondary 111-139 information are thus linked together in a primary tree by main permanent links 201-204 and secondary 211-239 in the form of a tree and branches as shown on the figure 4.
    According to this primary tree, the first database 41 has four main pages 101-104 information and twenty-seven sub pages 111-139 information. The four main information pages 101-104 are located at a main level 31 of the primary tree and are respectively linked by four main permanent links 201-204 to the original 100 of this primary tree. The twenty-seven secondary pages 111-139 of information are located on three secondary levels 32,33,34.
    Thus, each main information page 101-104 is connected by one or more secondary permanent links 211-219 to one or more secondary information pages 111-119 located on the first secondary level 32. Likewise, a secondary page of 111-119 located on the first secondary level 32 is connected by one or more secondary permanent links 221-229 to one or more secondary pages of information 111-129 located on the second secondary level 33. Finally, a secondary page of information 121-129 located on the second secondary level 33 is connected by one or more secondary permanent links 231-239 to one or more secondary information pages 131-139 located on the third secondary level 34. However, some secondary pages of information 113,117,118,122,125,126,129 are not linked to any secondary information page of an upper secondary level. On the other hand, a secondary information page 111-139 is connected to a single secondary information page 111-139 of a lower secondary level or to a single main information page 101-104.
    The memory 5 thus stores the first database 41 comprising the main pages 101-104 and secondary 111-139 of information and a second database 42 comprising a first library grouping the main permanent links 201-204 and the links secondary permanent 211-239.
    Then, during a second step 52 of determining a current situation of the aircraft 20, the analysis means 7 uses in real time the measurements and / or the information provided by the measurement and detection means 6 to determine this current situation of the aircraft 20.
    The measurement and detection means 6 are constituted inter alia by different sensors 61-64 to determine in particular the operating state of the aircraft 20 such as its air speed and altitude. These sensors 61-64 also make it possible to determine the operating state of equipment of the aircraft 20, such as the main rotor 22, the rear rotor 23, the mechanical power transmission 24 and the engine 25. measurement and detection 6 also include a satellite receiver 65 for determining the speed and position of the aircraft 20 in a terrestrial reference.
    The analysis means 7 may for example determine the flight phase of the aircraft 20 or an abnormal change in the current situation of the aircraft 20. The current situation of the aircraft 20 is composed of events such as the maintaining a flight phase or the change of flight phase during the normal flight of the aircraft 20 or an incident or failure of a 21-25 equipment in the case of an abnormal development of the situation current of the aircraft 20.
    Main contextual links 301-305 and secondary links 311-319 are attached to some of these events of the current situation of the aircraft 20. These main contextual links 301-305 and secondary links 311-319 are linked to secondary pages 111-139 information as shown in Figure 5.
    These secondary pages 111-139 of information related to a main contextual link 301-305 or secondary link 311-319 contain information relevant to the event of the current situation of the aircraft 20 to which this link is attached. main contextual 301-305 or secondary 311-319. These main contextual links 301-305 and secondary 311-319 are linked to these secondary information pages 111-139 regardless of the primary tree. In fact, a main contextual link 301-305 and a secondary contextual link 311-319 connect two secondary pages of information regardless of their secondary levels. In contrast, the main permanent links 201-204 and secondary 211-239 link the main pages 101-104 and secondary 111-139 information according to the primary tree and regardless of these events of the current situation of the aircraft 20.
    Moreover, an event of the current situation of the aircraft 20 is associated with a single main contextual link 301-305 and generally one or more secondary contextual links 311-319. However, it is possible that only a main context link 305 is attached to an event and no secondary context link is attached to this event, as is the case for the secondary page of information 119. In addition, a main contextual link 301-305 or a secondary contextual link 311-319 can also be linked to a main information page 101-104.
    The main contextual link 301-305 is set to a secondary information page 311-339 which is considered as the most relevant information page necessary for the pilot to take into account and / or treat the event to which this link is attached. main contextual 301-305. This most relevant secondary information page 111-139 may be linked by at least one secondary contextual link 311-319 to at least one other secondary information page which is also relevant to that event.
    The memory 5 stores a third database 43 comprising second libraries grouping these main contextual links 301-305 and these secondary contextual links 311-223. Each second library is attached to an event of the current situation of the aircraft 20.
    The main permanent 201-204 and secondary links 211-239 as well as the main contextual links 301-305 and secondary links 311-319 can be created independently of the method of assisting the piloting of the aircraft 20 during the setting up of the pages. information in the first database 41.
    However, the method of assisting the piloting of the aircraft 20 may include a preliminary stage 50 of creating these main permanent links 201-204 and secondary links 211-239 as well as these main contextual links 301-305 and secondary links 311-319. . This preliminary step 50 is performed upstream of the first step 51.
    During a third step 53 of displaying at least one main contextual icon 11, several main contextual icons 11 may be displayed on a touch screen 3,3 'as shown in FIGS. 6 and 7. These main contextual icons 11 are displayed in a column 15 located between the two information pages, these two pages of information being displayed respectively in the windows 16, 17 located on either side of the column 15.
    Each main contextual icon 11 displayed is linked to a main contextual link 301-305 of the second library and is therefore attached to an event of the current situation of the aircraft 20. In fact, a main contextual icon 11 is displayed as soon as an event of the current situation of the aircraft 20, to which a main contextual link is attached, is detected.
    The main contextual icons 11 displayed at the bottom of the column 15 are main contextual operating icons and are attached to events relating to a normal flight of the aircraft 20. These main contextual operating icons correspond for example to the phase of the aircraft and its position on the route provided for in the flight plan.
    The main contextual icons 11 displayed at the top of column 15 are main alerting contextual icons and are attached to events relating to an incident or to a breakdown of an essential equipment of the aircraft 20. The main alert icons 11 are displayed at the top of column 15 in order to be more easily visible and identifiable by the pilot. Each main contextual icon 11 may be associated with a text or an abbreviation characterizing the event to which this main contextual icon 11 is attached.
    During a fourth step 54 for selection and lateral displacement of a main contextual icon 11, the pilot selects via the selection means 4,4 'a main contextual icon 11 on a touch screen 3,3' . The selection means 4,4 'being integrated in the touch screen 3,3', the driver presses with a finger directly on the main contextual icon 11 on the touch screen 3,3 '. The pilot then moves laterally the main contextual icon 11 by moving his finger without taking off the touch screen 3,3 '. The selected main contextual icon 11 is moved from the column 15 to one of the windows 16, 17.
    Then, during a fifth step 55 of displaying a secondary information page 111-139, a new information subpage 111-139 is displayed in place of the information page previously displayed in the window 16,17 on which has been moved the main contextual icon 11 selected. This new information subpage 111-139 displayed is in fact linked to the selected main contextual icon 11 and, consequently, to the main contextual link 301-305 to which this selected main contextual icon 11 is linked. Consequently, this new information subpage 111-139 displayed is also linked to the event of the current situation of the aircraft 20 to which this main contextual link 301-305 is attached. This new secondary information page 111-139 is finally the most relevant information page for this event.
    The pilot of the aircraft 20 can thus easily and quickly consult, after having selected and moved a main contextual icon 11, the most relevant information page relating to the event corresponding to the appearance of this main contextual icon 11.
    The method of assisting the piloting of the aircraft 20 may comprise complementary steps according to the block diagram of FIG. 3. These complementary steps may be grouped into three stages occurring simultaneously at the third, fourth and fifth stages 53,54,55 .
    First, the method of assisting the piloting of an aircraft 20 may include the following complementary steps.
    During a sixth step 63 of displaying at least one secondary contextual icon 12, several secondary contextual icons 12 may be displayed on the touch screen 3,3 'as shown in FIG. 7. These secondary contextual icons 12 are displayed at the top of a secondary information page 111-139 displayed in the window 17 and correspond to an event of the current situation of the aircraft 20. This secondary information page 111-139 has for example been displayed more selecting a main contextual icon 11 during the third step 53.
    Each secondary contextual icon 12 displayed is linked to a secondary contextual link 311-319 which is itself attached to the event of the current situation of the aircraft 20 to which is linked the secondary information page 111-139 displayed in FIG. window 17.
    As for the main contextual icons 11, each secondary contextual icon 12 can be associated with a text or an abbreviation.
    Then, during a seventh step 64 of selecting a secondary contextual icon 12, the driver selects via the selection means 4,4 'a secondary contextual icon 12 on the touch screen 3,3'.
    During an eighth step 65 of displaying a secondary information page 111-139, a new information subpage 111-139 is displayed instead of the information subpage 111-139 above. displayed in the window 17 t. This new information subpage 111-139 displayed is related to the secondary contextual icon 12 selected in the previous step and, consequently, to the secondary contextual link 311-319 to which this secondary context icon 12 selected is linked. Consequently, this new information subpage 111-139 displayed is also linked to the event of the current situation of the aircraft 20 linked to the secondary information page 111-139 previously displayed in the window 17. Secondary page 111-139 information is also relevant to this event to allow the pilot to treat this event.
    The method of assisting the piloting of an aircraft 20 may also include the following complementary steps.
    During a ninth step 73 of displaying at least one main permanent icon 13, several main permanent icons 13 may be displayed on the touch screen 3,3 'as shown in FIGS. 6 and 7. These permanent icons main 13 are displayed in the column 15 substantially vertically centered in this column 15 while the main contextual icons 11 are displayed at the top and / or bottom of the column 15. Moreover, these main permanent icons 13 have a shape substantially square while the main contextual icons 11 have an elongated rectangular shape. The pilot can thus easily differentiate the main permanent icons 13 and the main contextual icons 11.
    Each main permanent icon 13 displayed is linked to a main permanent link 201-204 of the first library and is therefore linked to the primary tree of the main pages 101-104 and secondary information 111-139. By cons, this main permanent icon 13 is independent of any event of the current situation of the aircraft 20. In fact, these main permanent icons 13 are displayed permanently regardless of the current situation of the aircraft 20.
    During a tenth step 74 of selection of a main permanent icon 13, the pilot selects via the selection means 4,4 'a main permanent icon 13 on the touch screen 3,3' and moves laterally this main permanent icon 13 selected from the column 15 to one of the windows 16,17.
    During an eleventh step 75 of displaying an information main page 101-104, a main information page 101-104 is displayed in place of the information page previously displayed in the window 16 , 17 on which has been moved the main permanent icon 13 selected. This displayed main page 101-104 is in fact related to the selected main permanent icon 13 and hence to the main permanent link 201-204 to which this selected main context icon 11 is linked.
    The pilot of the aircraft 20 can thus easily and quickly consult, after having selected and moved a main permanent icon 11, one of the main information pages 101-104 of the main level 31 of the primary tree.
    The method of assisting the piloting of an aircraft 20 may finally comprise the following complementary steps.
    During a twelfth step 83 for displaying at least one secondary permanent icon 14, several secondary permanent icons 14 may be displayed on the touch screen 3,3 'as shown in FIGS. 6 and 7. These permanent icons 14 are displayed on the side of a main page 101-104 information displayed in the window 17 as shown in Figure 6 or that of a secondary page information 111-139 displayed in the window 17 as shown in Figure 7.
    Each secondary permanent icon 14 displayed is linked to a secondary permanent link 211-239 of the first library and is therefore linked to the primary tree of the main pages 101-104 and secondary information 111-139. This secondary permanent icon 14 is therefore independent of any event of the current situation of the aircraft 20.
    During a thirteenth step 84 for selecting a secondary permanent icon 14, the pilot selects via the selection means 4,4 'a secondary permanent icon 14 on the touch screen 3,3'.
    During a fourteenth step 85 of displaying a secondary information page 111-139, a new information subpage 111-139 is displayed in place of the information page previously displayed in the window. 17 which may be a main information page 101-104 or a secondary information page 111-139. This new information subpage 111-139 displayed is linked to the selected secondary permanent icon 14 and, consequently, to the secondary permanent link 211-239 to which this selected secondary context icon 14 is linked.
    The pilot of the aircraft 20 can thus easily and quickly consult, after having selected a secondary permanent icon 14, a secondary information page 111-139 of the first secondary level 32 of the primary tree when the previously displayed information page is a main information page 101-104 or a secondary level 33,34 higher than the secondary level of the previously displayed information page when this previously displayed information page is a secondary information page 111-139 .
    In addition, it is possible to display side by side two secondary pages 111-139 information relating to the same event of the current situation of the aircraft 20, as shown in Figure 8. For this purpose, when a Information secondary page 111-139 relating to an event of the current situation of the aircraft 20 is displayed for example in the window 17, the pilot selects the column and then laterally moves the column to this window 17. The two windows 16,17 are then displayed side by side and the column 17 is displayed on one side of the touch screen 3,3 '. One of the two windows 16, 17 contains the secondary page information 111-139 previously displayed and relating to this event while the other window 16,17 contains another secondary page of information 111-139 related to this same event. The driver can of course request the display of another secondary information page 111-139 relating to this same event by selecting a secondary contextual icon 12.
    Moreover, the display of certain information pages 101-104, 111-139 can be enlarged as shown in FIG. 9 by selecting and laterally moving column 15. This is particularly the case when the information page 101 -104, 111-139 is displayed following the selection of a main permanent icon 201-204 or secondary 211-239, for example to display the position of the aircraft 20 on a map.
    Naturally, the present invention is subject to many variations as to its implementation. Although several embodiments have been described, it is well understood that it is not conceivable to exhaustively identify all the possible modes. It is of course conceivable to replace a means described by equivalent means without departing from the scope of the present invention.
    权利要求:
    Claims (15)
    [1" id="c-fr-0001]
    1. Device (1) for assisting the piloting of an aircraft (20) comprising: at least one processor (2), at least one display means (3,3 ', 3'), a means of selecting (4,4 ') for each display means (3,3'), -at least one memory (5) containing at least one database (41,42,43), -measuring and detection means (6), and -at least one means of analysis (7), characterized in that -said measurement and detection means (6) and at least one analysis means (7) determine a current situation of said aircraft ( 20), at least one display means (3,3 ') displays two pages of information, at least one main contextual icon (11), each main contextual icon (11) corresponding to an event of said current situation of said aircraft (20), and said selection means (4,4 ') relating to said display means (3,3') on which at least one main contextual icon (11) is displayed allows a selection then a lateral displacement of a main contextual icon (11) to display on said display means (3,3 ') an information page linked to said main contextual icon (11) selected and attached to an event of said current situation.
    [2" id="c-fr-0002]
    2. Device (1) according to claim 1, characterized in that -said visualization means (3,3 ') displays at least one secondary contextual icon (12) on said information page related to said main contextual icon (11). ) selected, each secondary contextual icon (12) corresponding to said event of said current situation to which said selected main contextual icon (11) is attached, and - said selection means (4,4 ') relative to said visualization means (3,3) ') allows selection of a secondary contextual icon (12) to display on said display means (3,3') an information page corresponding to said selected secondary context icon (12) and each of said other icons secondary contextual (12).
    [3" id="c-fr-0003]
    3. Device (1) according to any one of claims 1 to 2, characterized in that -at least one display means (3,3 ') displays at least one main permanent icon (13) independently of said current situation and said selection means (4,4 ') relating to said display means (3,3') ensures selection of a main permanent icon (13) in order to display on said display means (3,3 ') a corresponding main page of information related to said selected main permanent icon (13).
    [4" id="c-fr-0004]
    4. Device (1) according to any one of claims 1 to 3, characterized in that -at least one display means (3,3 ') displays on a page of information at least one secondary permanent icon (14) regardless of said current situation, each secondary permanent icon (14) being relative to said information page, -said selection means (4,4 ') relating to said display means (3,3') on which at least one icon permanent secondary (14) is displayed allows selection of a secondary permanent icon (14) to display a secondary information page corresponding to said selected secondary permanent icon (14) and optionally at least one of said secondary permanent icons (14).
    [5" id="c-fr-0005]
    5. Device (1) according to any one of claims 1 to 4, characterized in that said memory (5) contains a first library of main and secondary permanent links and a plurality of second libraries of main and secondary contextual links, each second library of contextual links being attached to an event of said current situation of said aircraft (20), said primary and secondary permanent links of said first library being respectively linked to said main and secondary permanent icons (13, 14) and allowing structured navigation and hierarchy on the one hand between each main permanent icon (13) and each main page of information and secondly between each secondary permanent icon (14) and each secondary page of information, said main and secondary contextual links of each second library being respectively linked to said icons contextual and secondary context (11,12) and allowing a fast and relevant navigation on the one hand between each main contextual icon (11) and each information page and secondly between each secondary contextual icon (12) and each page information according to said current situation.
    [6" id="c-fr-0006]
    6. Device (1) according to any one of claims 1 to 5, characterized in that at least one display means (3,3 ') is a touch screen thus integrating said selection means (4,4') relative visualization means audit (3,3 ').
    [7" id="c-fr-0007]
    7. Method (1) for assisting the piloting of an aircraft (20), said aircraft (20) comprising: at least one processor (2), at least one visualization means (3,3 '), selection means (4,4 ') for each display means (3,3'), -at least one memory (5) containing at least one database (41,42,43), -measuring means and detection (6), and -at least one means of analysis (7), characterized in that said method comprises various steps comprising -displaying two pages of information on a display means (3,3 ' ), -determining a current situation of said aircraft (20), -displaying on said display means (3,3 ') at least one main contextual icon (11) relating to said current situation, each icon contextual context (11) relating to an event of said current situation of said aircraft (20), -selecting and laterally moving a contextual icon main (11), and -the display on said display means (3,3 ') of an information page corresponding to said event attached to said selected main contextual icon (11).
    [8" id="c-fr-0008]
    8. Method (1) for assisting the piloting of an aircraft (20) according to claim 7, characterized in that said method comprises various complementary steps comprising: the display on said display means (3,3 ') at least one secondary contextual icon (12) corresponding to said event of said current situation to which said selected main contextual icon (11) is attached -the selection of a secondary contextual icon (12) and -the display on said viewing (3,3 ') an information page corresponding to said selected secondary contextual icon (12) and at least one of said secondary contextual icons (12).
    [9" id="c-fr-0009]
    9. A method (1) for assisting the piloting of an aircraft (20) according to any one of claims 7 to 8, characterized in that said method comprises different complementary steps comprising: -the display on said display means (3,3 ') at least one main permanent icon (13) independently of said current situation, -the selection of a main permanent icon (13), and -the display on said display means (3,3) ') a corresponding main information page related to said selected main permanent icon (13).
    [10" id="c-fr-0010]
    10. A method (1) for assisting the piloting of an aircraft (20) according to any one of claims 7 to 9, characterized in that said method comprises different complementary steps comprising: -the display on said display means (3,3 ') on an information page of at least one secondary permanent icon (14) independently of said current situation of said aircraft (20), each secondary permanent icon (14) being relative to said information page, the selection of a secondary permanent icon (14) and the display on said display means (3,3 ') of a secondary page of information corresponding to said selected secondary permanent icon (14) as well as optionally at least one of said secondary permanent icons (14).
    [11" id="c-fr-0011]
    11. A method (1) for assisting the piloting of an aircraft (20) according to any one of claims 7 to 10, characterized in that said main contextual icons (11) and if appropriate said main permanent icons (13). ) are displayed on said display means (3,3 ') in a column (15) located between said two pages of information.
    [12" id="c-fr-0012]
    12. A method (1) for assisting the piloting of an aircraft (20) according to claim 11, characterized in that two secondary pages are displayed side by side on said display means (3,3 '). information relating to said event attached to said main contextual icon (11) selected by selecting and then moving said column (15) laterally.
    [13" id="c-fr-0013]
    13. Method (1) for assisting the piloting of an aircraft (20) according to claim 11, characterized in that the display of an information page is enlarged on said display means (3,3 '). selecting and then moving said column (15) laterally.
    [14" id="c-fr-0014]
    14. Method (1) for assisting the piloting of an aircraft (20) according to any one of claims 7 to 13, characterized in that said method comprises a preliminary step of creating on the one hand main contextual links and secondary events attached to events of said current situation of said aircraft (20) and linked to said information pages, and secondly of primary and secondary permanent links independent of said events of said current situation of said aircraft (20) and linked to said pages of information according to a primary tree, said primary and secondary permanent links being grouped together in a first library and said primary and secondary contextual links being grouped into a plurality of second libraries, each second library of contextual links being attached to an event that may be encountered aircraft (20).
    [15" id="c-fr-0015]
    15. A method (1) for assisting the piloting of an aircraft (20) according to any one of claims 7 to 14, characterized in that said display means (3,3 ') is a touch screen thus integrating said selection means (4,4 ') relating to said display means (3,3').
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    同族专利:
    公开号 | 公开日
    FR3045176B1|2019-10-11|
    US20170168680A1|2017-06-15|
    引用文献:
    公开号 | 申请日 | 公开日 | 申请人 | 专利标题
    EP0580474A1|1992-07-24|1994-01-26|Sextant Avionique|Method and device for assisting the steering of an aircraft using a great number of documents stored in a memory|
    FR3012599A1|2013-10-31|2015-05-01|Gulfstream Aerospace Corp|
    US7579966B2|2006-05-30|2009-08-25|Calspan Corporation|Dual-axis loadmeter|
    FR2935179B1|2008-08-20|2010-12-03|Airbus France|METHOD AND DEVICE FOR ASSISTANCE IN CONTROLLING ON-AIR SYSTEMS IN AN AIRCRAFT|
    KR101640460B1|2009-03-25|2016-07-18|삼성전자 주식회사|Operation Method of Split Window And Portable Device supporting the same|
    US8589069B1|2009-11-12|2013-11-19|Google Inc.|Enhanced identification of interesting points-of-interest|
    US8903655B2|2009-11-30|2014-12-02|Honeywell International Inc.|Method and system for displaying emphasized aircraft taxi landmarks|
    US8723693B1|2011-06-30|2014-05-13|Rockwell Collins, Inc.|System for and method of indicating predictive windshear transmitter status|
    US9014879B2|2013-09-17|2015-04-21|Honeywell International Inc.|Messaging and data entry validation system and method for aircraft|
    US10042456B2|2014-03-11|2018-08-07|Textron Innovations Inc.|User interface for an aircraft|
    US9811954B2|2014-12-02|2017-11-07|Honeywell International, Inc.|Near-to-eye display systems and methods for verifying aircraft components|
    US10426393B2|2017-09-22|2019-10-01|Aurora Flight Sciences Corporation|Systems and methods for monitoring pilot health|US20190276158A1|2018-03-08|2019-09-12|Bell Helicopter Textron Inc.|Active cooling system|
    US11010940B2|2018-12-19|2021-05-18|EffectiveTalent Office LLC|Matched array alignment system and method|
    US11010941B1|2018-12-19|2021-05-18|EffectiveTalent Office LLC|Matched array general talent architecture system and method|
    US11016988B1|2018-12-19|2021-05-25|Airspeed Systems LLC|Matched array flight alignment system and method|
    法律状态:
    2016-12-22| PLFP| Fee payment|Year of fee payment: 2 |
    2017-06-16| PLSC| Publication of the preliminary search report|Effective date: 20170616 |
    2017-12-21| PLFP| Fee payment|Year of fee payment: 3 |
    2018-12-19| PLFP| Fee payment|Year of fee payment: 4 |
    2019-12-19| PLFP| Fee payment|Year of fee payment: 5 |
    2020-12-23| PLFP| Fee payment|Year of fee payment: 6 |
    2021-12-24| PLFP| Fee payment|Year of fee payment: 7 |
    优先权:
    申请号 | 申请日 | 专利标题
    FR1502591|2015-12-15|
    FR1502591A|FR3045176B1|2015-12-15|2015-12-15|DEVICE AND METHOD FOR ASSISTING THE CONTROL OF AN AIRCRAFT|FR1502591A| FR3045176B1|2015-12-15|2015-12-15|DEVICE AND METHOD FOR ASSISTING THE CONTROL OF AN AIRCRAFT|
    US15/376,017| US20170168680A1|2015-12-15|2016-12-12|Device and a method for assisting the piloting of an aircraft|
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