• 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:
    A method (200) for providing updated data to an aircraft, comprising requesting (204) updated data relating to a route to be followed by the aircraft, receiving (206), in a member of the aircraft, procedural data of flight in updated data, transmitted by a ground station in response to the request and updating (208) of the route to be followed using the flight procedure data in the updated data.
    公开号:FR3035711A1
    申请号:FR1653657
    申请日:2016-04-26
    公开日:2016-11-04
    发明作者:Russell Allen Ramaker；Joachim Karl Ulf Hochwarth
    申请人:GE Aviation Systems LLC；
    IPC主号:
    专利说明:

    [0001] Systems and Methods for Providing Updated Data to an Aircraft In an aircraft, all kinds of useable aeronautical data are available. Flight data may be available from a number of aeronautical data sources. For example, an aircraft navigation system such as the Flight Management System (VMS) currently contains several databases. The database used to plan flights and forecast trajectories is the Navigation Database (NDB), which is stored in the VMS. The NDB is a static database that has a predetermined refresh cycle (eg 28 days) for updating. Currently, maintenance personnel must manually update the NDB in accordance with this cycle. The NDB is used to ensure that, for example, planned runway closures or navigational aids are propagated so that the flight crew or the SGV can not select them for the predetermined time between cycles. discount. The VMS may also contain or access an additional NDB used by the crew to store temporary navigation data. Air Traffic Control (CCA) uses data communications to electronically transmit clearances to aircraft. The VMS can then load the clearance into the VMS where it can be inserted into the flight plan that will guide the aircraft. These clearances are currently limited to data contained in the VMS static NDB. The exception is waypoints, which can also be defined by their position (ie latitude and longitude). Thus, although the CCA may transmit a clearance that contains a flight procedure unavailable in the NDB of the aircraft, the pilot will not be able to load it into the VMS. According to a first aspect, an embodiment of the invention relates to a method for providing updated data to an aircraft, the method comprising requesting updated data for a route taken by the aircraft, receiving updated data, including flight procedure data from a ground station in response to the request; and updating the route to be followed at least in part based on the flight procedure data. In another aspect, an embodiment of the invention provides an aircraft actuation system having a radio communication link and a flight management system that communicates with the communication link, and includes a communication module. update designed to request a remote server, via the communication link, updated data relating to a route to be followed by the aircraft, and update flight procedure data included in the updated data in at least one component forming navigation database, or loaded into a flight plan flight management system. The invention will be better understood from the detailed study of some embodiments taken as non-limiting examples and illustrated by the appended drawings in which: FIG. 1 is a diagrammatic representation of an aircraft and a ground system according to one embodiment of the invention; FIG. 2 is a block diagram of an aeronautical data updating system 30 according to an embodiment of the invention, which is usable with the aircraft and the ground system of FIG. 1; FIG. 3 is a block diagram of an aeronautical data updating system according to one embodiment of the invention, which is usable with the aircraft and the ground system of FIG. 1; FIG. 4 is a flowchart illustrating a method for providing information via an aeronautical data updating system such as that illustrated in FIGS. 2 and 3, according to one embodiment of the invention; and FIG. 5 is a flowchart illustrating another method for providing information via an aeronautical data updating system such as that illustrated in FIGS. 2 and 3, according to one embodiment of the invention.
    [0002] At least some of the following embodiments provide aircraft data update systems and methods for loading information from a Navigation Database (NDB) into the aircraft in such a way that the NDB be dynamic rather than static. Currently, the NDB is usually updated manually during the current manual maintenance corresponding to the predetermined refresh cycle (eg, 28 days). Specifically, maintenance personnel, during routine maintenance, substitute an entirely new set of disks containing the NDB information or load the NDB information over Ethernet, after which this data will be the only data used up to the next cycle. next predetermined update. Figure 1 shows an aircraft 10 which has an environment for embodiments of the invention. The aircraft 10 can fly on a road, 30 from one point to another, and can include one or more propulsion engines 12 mounted on a fuselage 14. A cockpit 16 can be placed in the fuselage 14 and half The airfoils 18 may extend outwardly from the fuselage 14. In addition, a series of on-board systems 20 that allow the aircraft 10 to operate properly may be included, as well as a controller or computer 22. , and a communication system having a communication link 24. It should be understood that "a series" may comprise any number of on-board systems, or even a single onboard system. Although a commercial aircraft has been shown, it is contemplated that embodiments may be used in any type of aircraft, by way of non-limiting examples, fixed-wing, rotary wing, aircraft fires, personal aircraft, drones and military aircraft.
    [0003] The series of on-board systems 20 may be in the cockpit 16, inside the compartment (not shown) of equipment and electronic equipment or elsewhere throughout the aircraft 10, the shipboard systems may even be These onboard systems 20 may include, in no way limiting, an electrical system, an oxygen circuit, a hydraulic or pneumatic circuit, a fuel system, a propulsion system, a SGV, flight controls, audio / video systems, an Integrated Vehicle Condition Management System (IVHM) and systems associated with the mechanical structure of the aircraft 10. The computer 22 can cooperate with the series of aircraft. on-board systems 20 and it is envisaged that the computer 22 can facilitate the operation of the on-board systems 20 and can receive information from the series of onboard systems 20. The computer 22 30 can, among other things, automate the tasks The computer 22 may also be connected to other controllers or computers of the aircraft 10. The computer 22 may comprise a memory 26, the memory 26 may comprise a random access memory (RAM), a read only memory (ROM), a flash memory or one or more different types of portable electronic memory such as disks, DVDs, CD-ROMs, etc., or any adequate combination of these types of memories. The computer 22 may comprise one or more processors 28, which may execute any suitable programs. The computer 22 may include or be associated with any appropriate number of individual equipment such as microprocessors, power sources, storage devices, interface cards, automatic flight systems, computers flight management and other common components, and the computer 22 may understand or cooperate with any number of software (eg flight management programs) or instructions designed to implement the various processes, process tasks, calculations and control / display functions necessary for the operation of the aircraft 10. The communication link 24 may communicate with the computer 22 or other processors of the aircraft to transmit information to and from the aircraft 10. It is envisaged that the communication link 24 may be a radio communication link and may be any kind of communication mechanism. it is able to establish a radio link with other systems and devices and may include, in no way limiting, a satellite upstream link, the Internet by SATCOM, a VHF data link (VDL), a network ACARS, broadcast dependent automatic monitoring (ADS-B), wireless fidelity (WiFi), WiMax, a 3G radio signal, a code division multiple access radio (CDMA) signal, the global broadcast system mobile communications (GSM), a 4G radio signal, a long-term evolution (LTE) signal, or any combination thereof. In addition, the particular type or mode of radio communication is not essential for the embodiments of the present invention, and the radio networks developed in the future will certainly come within the scope of embodiments of the present invention. invention. On the other hand, the communication link 24 may communicate with the computer 22 via a radio link without changing the scope of embodiments of the present invention. Although only one communication link 24 has been shown, it is envisaged that the aircraft 10 may have multiple communication links communicating with the computer 22. These multiple communication links may give the aircraft to transmit information in various ways to or from the aircraft 10.
    [0004] As illustrated, the computer 22 may communicate with a remote server 30, which may be anywhere, especially in a given ground station 32, via the communication link 24. The ground station 32 may be n ' any type of ground communications station 32 such as a station operated by ANSPs / air traffic controllers (ACCs). The remote server 30 may include a computer searchable information database 34 accessible to a processor 36. The processor 36 may execute a set of executable instructions to access the computer searchable information database 34. . The remote server 30 could include a general-purpose computer device in the form of a computer, comprising a central unit, a system memory and a system bus, which couples to the central unit various system components including system memory. . The system memory may comprise a read-only memory and a random access memory. The computer may also include a magnetic hard disk drive for reading or writing to a removable magnetic hard disk, a magnetic disk drive for reading or writing on a removable magnetic disk, an optical disk drive for reading or writing on a computer. removable optical disk such as a CD-ROM or other optical media. The computer searchable information database can be any suitable database, including a single database containing multiple data sets, multiple, separate data bases in connection with one another, even a simple table of data. It is contemplated that the computer searchable information database may contain a number of databases or that the database may actually be a number of separate databases. During operation of the aircraft 10, the computer 22 may request information from and receive from the remote server 30. In this way, the computer 22 may be part of a system for providing updated data to the aircraft 10. As more clearly illustrated in Figure 2, the system 38 for providing the updated data may include the computer 22. , which has been shown as part of the SGV. In the illustrated example, a database component 40 is shown included in the memory 26. The database component 40 may be any suitable database, including a single data base containing a data base 40. multiple datasets, multiple separate databases in conjunction with one another, or even a simple array of data. It is contemplated that the database component 40 may contain a number of databases or that the database may actually be a number of separate databases. The database component 40 may be a NDB containing information including, but not limited to, airports, runways, air routes, waypoints, terminal areas, navigational aids, route specific routes, and air carriers / companies and procedures such as standardized instrument departure (SID) and standardized terminal approach trajectories (STAR). The database component 40 may also include, in the SGS, a memory containing a flight plan. Furthermore, a refresh module 42 is shown included in the processor 28. The update module 42 may be designed to request the remote server 30 updated data concerning a route to be followed by the aircraft 10. For example, the The update module 42 may include, but not be limited to, a computer program operating in the processor 28 and able to request information from the remote server 30. More particularly, the update module 42 may request updated data from the remote server 30 via The radio communication link 24. It is envisaged that this process may be initiated by the user or may be implemented automatically by the update module 42 when the aircraft 10 is in flight or when the aircraft is at the aircraft. ground. The flight procedure data received in updated data can be loaded into the database component 40. It is contemplated that the database component 40 may contain otherwise static information about flight procedures as well as as the dynamic data received in the updated data. The database component 40 may be a predefined refresh cycle NDB, including but not limited to a 28 day cycle, and the receipt of the flight procedure data in the updated data is manually performed by the maintenance personnel. following a predetermined refresh cycle. Since the refreshing according to a predetermined cycle is done manually by the maintenance personnel following a predetermined refresh cycle, the NDB is considered a static database. 3 represents another possible updating system 138 similar to the system 38 and, unless stated otherwise, the description of the identical parts of the system 38 is for the updating system 138. A difference is that a component forming Additional or additional database 144 is included in the memory 126 and can be used to store in the updated data the data received on the flight procedures. The additional database component 144 may be any suitable database, including a single database containing multiple data sets, multiple, separate databases in connection with one another, or even a simple array. of data. It is contemplated that the additional database component 144 may contain a number of databases or that the database may actually be a number of separate databases. In addition, an integrity module 146 is shown included in the processor 128. The integrity module 146 may be designed to control the integrity of the flight procedure data received in updated data. The term "integrity" used here refers to the verification of data. By way of non-limiting example, the integrity of the flight procedure data can be controlled so as to detect fortuitous changes in raw data. For example, the integrity module may include, but not limited to, a computer program such as a cyclic redundancy check executed in a processor. Although integrity module 146 is shown included in processor 128, it may be included in any part of the SGV. The update module 142 has been shown separate from the processor 128 to illustrate that it can also be included in any part of the SGV. Still further, an autopilot system 120 is specifically shown as cooperating with the computer 122. The computer 122 may provide the flight procedure data received in updated data to other systems present in the aircraft 10 including, but not limited to, the autopilot system shown 120. Similarly, a cockpit electronic organizer 148 may be included in the aircraft 10 and the flight procedure data may also be loaded into the electronic organizer 148 cockpit. By way of non-limiting example, the computer 122 can download the flight procedure data received in the updated data to the electronic crew station organizer 148 via the radio communication link 124. The embodiments described above could also be used for dynamic updating of additional information such as airline or airline specific data. By way of non-limiting example, these company specific data may include commonly used flight plans or routes. This information could also be stored in the database component 140 or the additional database component 144. The embodiments described above may include sufficient security, including, but not limited to, end-to-end encryption for avoid malicious content in the updated data received. For example, the system may include a security module designed to verify the authenticity of the flight procedure data in the updated data. The term "authenticity" as used herein refers to the indisputable character of the communication. As non-limiting examples, the authenticity check may include control of the flight procedure data to avoid malicious content or to prevent identity theft and denial of service attacks. Details of environments capable of implementing embodiments of the invention are presented to provide a complete understanding of the technology described herein.
    [0005] However, it will be apparent to those skilled in the art that the exemplary embodiments may be implemented without these specific details. Examples of embodiments are described with reference to the drawings. These drawings illustrate certain details of specific embodiments that involve a module or method, or a computer program product described herein. However, the drawings should not be interpreted as imposing any potential limitations on the drawings. The method and computer program can be run on any computer-readable medium to run properly. Embodiments may be implemented using an existing processor or by a specific processor incorporated for that purpose or another, for a wired system. As noted above, the embodiments described herein may include a computer program product comprising computer-readable media carrying or on which computer-readable instructions or data structures are stored. These computer-readable media may be any existing media accessible to a versatile or specific computer or other processor machine. By way of example, such computer-readable mediums may comprise a random access memory, a read-only memory, an EPROM, an EEPROM, a CD-ROM or other optical disc storage, magnetic disk storage or other magnetic storage devices. or any other medium that can be used to carry or store desired program code in the form of computer-readable instructions or data structures that is accessible to a versatile or specific computer or other machine. processor. When information is transmitted or delivered via a network or other communication link (wired or radio or both wired and wireless) to a machine, the machine rightly sees the link as a computer-readable medium. Thus, any link such as this is rightly called a computer-readable medium.
    [0006] Combinations of the above link means also fall within the definition of computer readable media. The computer executable instructions include, but are not limited to, instructions and data that cause a versatile computer, a specific computer, or specific processors to perform a certain function or group of functions. Embodiments will be described in the general context of steps of a method that may be implemented in one embodiment by a program product comprising computer executable instructions such as program codes, for example, under the form of program modules run by machines in networked environments. Overall, the program modules include routines, programs, objects, components, data structures, and so on. which have the technical effect of performing particular tasks or of implementing particular abstract data types. Computer executable instructions, associated data structures, and program modules are examples of program codes for performing steps of the method presented here. The particular order of these executable instructions or associated data structures are examples of corresponding acts to implement the functions described in these steps.
    [0007] Embodiments may be practiced in a networked environment using logical connections to one or more remote computers having processors. The logical connections may include a local area network (LAN) and a wide area network (WAN) presented here by way of non-limiting example. These networked environments are common in office-wide or enterprise-wide computer networks, intranets, and the Internet and can use a variety of different communication protocols. It will be understood by those skilled in the art that these networked computer environments typically encompass many types of computer system configurations, including personal computers, portable devices, multiprocessor systems, microprocessor-based or programmable consumer electronic equipment. , networked PCs, minicomputers, mainframes and others. Embodiments may also be practiced in distributed computing environments where tasks are performed by related local and remote processing devices (either by cable links, radio links, or by a combination of hard-wired or wireless links). In a distributed computing environment, the program modules may be in both local and remote storage devices. In accordance with one embodiment of the invention, Fig. 4 illustrates a method 200 for providing up-to-date data. to an aircraft such as the aircraft 10. The method may start with an optional trigger event 202. Such a triggering event may include a predetermined period of time out of the predefined refresh cycle or a change of conditions in the flight plan. In this way, flight procedures can be updated daily or all hours or may take into account weather conditions such as winds or violent disturbances. As other non-limiting examples, the triggering event at 202 may include a predetermined portion of the flight plan. For example, these triggering events may include, without limitation, the preliminaries of the departure of the flight or the beginning of the cruise phase. In 204, the method 200 includes updating data relating to a route to be followed by the aircraft 10. The route to be followed may comprise a route defined before the flight of the aircraft 3035711 or defined during the flight of the aircraft . This request can be made by the updating module 42, 142 of the updating system 38, 138. More particularly, the updating module 42, 142, via the radio communication link 24, 124, can request this update. from the remote server 30. The request can be made automatically by the update module 42, 142 according to the trigger event in 202. For example, it is envisaged that the request is made automatically on the current route. defined and received by the computer 22, 122 constituting at least a portion of the SGV. In another example, in the event that the triggering event is part of the flight's preliminary preliminaries, the request may occur automatically during the departure preliminaries. According to another possibility, the request may be made periodically by the updating module, in particular every hour during the flight of the aircraft 10. As another non-limiting example, a crew member may manually request a updating of data. Flight procedure data may be received upon data refresh in 206. This flight data data in the updated data may be any amount of data provided by any suitable system or equipment. of which the remote server 30. By way of non-limiting example, the flight procedure data in the updated data can include any information on an airport, information on tracks including, but not limited to, track closures. , information on air corridors including, but not limited to, spaces for special activities, information on waypoints, information relating to aids to navigation including, but not limited to, closures of aids to navigation. or information on a specific route of an airline or procedures involving terminals, such as SIDs, STARs or approaches.
    [0008] The reception at 206 may be automatic in response to the request submitted at 204. The flight procedure may be received from the remote server 30 by the update system 38, 138 via the radio communication link 24, 124. More particularly, the flight procedures in the updated data can be received in the database component 40, 140 or in the additional database component 144. It is envisaged that the flight procedure data in the updated data can be directly synchronized in the database component 40, 140 or in the additional database component 144 and that no formatting is necessary to synchronize the flight procedure data in the database component 40, 140 or in the additional database component 144. It is also envisaged that the updated data could be 20 directly loaded into the SGV flight plan. By way of non-limiting example, the flight procedure data in the updated data may contain procedures represented in ARINC 424 format and coded in binary format that may include, but not limited to, binary XML. The computer 22, 122 constituting at least a portion of the SGV can take the flight procedure data into the updated data and include it in its database component 40, 140 or its additional database component 144. The Transport of the flight procedure data in the updated data between the remote server 30 and the aircraft 10 could be performed in the air of a data link protocol such as the Williamsburg (II) protocol. For example, data in ARINC format 424 could be sent using a Williamsburg (II) cover or an Aeronautical Telecommunications Network (ATN). Alternatively, the processor 28, 128 may be adapted to format the flight procedure data in the updated data to be compatible with the database component 40, 140 or the additional database component. 144. For example, the processor 28 can convert the binary data into packets in an exclusive format. In addition, the flight procedures in the updated data can be received in the active flight plan of the SGV. In particular, the updated data can be received in the flight plan after being reviewed and approved by the pilot. The information received at 206 can then be used to create a route to be followed by 208. More particularly, the flight procedure data in the updated data can be used by the VMS in the manner in which the aircraft 10 is made to fly. on the road. Updated flight procedure data does not indicate which route to fly; on the other hand, they cover how the road should be followed. Both the computer 22, 122 constituting at least a portion of the SGV and the crew may use the flight procedure data received in the updated data to include them in the flight plan allowing the aircraft 10 to fly according to the flight procedure. The computer 22, 122 constituting at least a portion of the SGV may also provide the information received in the updated data to other systems present in the aircraft 10, including the autopilot system or an electronic postman 3035711 In this way, the updated flight procedure can be included in the route to be followed and the aircraft can be stolen accordingly. In addition, additional data associated with the flight procedures can be received. For example, these additional data may reflect atmospheric conditions, including winds and violent disturbances. Also, additional data such as a Notice to Aviators (NOTAM) may be received and may contain information relating to potential hazards on an air route. In this way, the update module can be used to synchronize additional data. The method 200 is flexible and is presented for illustrative purposes only. For example, the order of the steps described is purely illustrative and is in no way intended to limit the method 200, it being understood that the steps may take place in a different logical order or that additional or intermediate steps may be included without There is no departure from embodiments of the invention. By way of non-limiting example, an alert inside the aircraft 10 can be issued when an update is available for a procedure loaded into the computer 22, 122 constituting at least a part of the SGV. In this way, the flight crew can be alerted if a procedure has been modified and lapses in the database component 40, 140 or the additional database component 144 of the SGV. It is contemplated that the computer 22, 122 may communicate and interact with the remote server 30 to determine when one of the updated data is available. The computer 22, 122 could then automatically update itself or request the crew to request updating, whether or not the outdated information is concerned with the route to be followed. Still further, the computer 22, 122 could provide an ANSP or CCA with information about the version of the procedure loaded into the computer 22, 122 so that appropriate route clearances can be received from the CCA. In yet another example, the computer 22, 122 may automatically request flight procedure data referenced in route clearances transmitted by CCA but absent in the database component 40, 140 or the base component of 144. In this way, the provision of updated data to the aircraft can be triggered when an updated route is received as illustrated in the method 300 of Figure 5. The method 300 is similar to the method 200 and, unless otherwise specified On the contrary, the description of the identical parts of the process applies to the method 300. In 302, before or during a flight, the computer 22, 122 can receive an updated route. The updated route can be received from any appropriate source, including a CCA. Still further, the computer 22, 122 may request a subscription to a procedure so that any updating of this procedure is automatically sent by the remote server 30. In this way, once the update module 42, 142 will have requested the subscription, data can be transmitted adequately by the station on the ground.
    [0009] In 304, the update module 42, 142 may request updated data regarding the updated route. In this way, the reception of the updated route can automatically cause the update system to request a refresh of data. At 306, the computer 22, 122 can then automatically receive, via the radio communication link 24, 124, flight procedure data in up-to-date data. The flight procedure data in the updated data can be synchronized in the database component 40, 140 or the additional database component 144. The flight procedure data in the updated data can also be loaded directly into the data stream. a flight plan of a data link after confirmation by the pilot. The flight plan of a data link or the modified / secondary flight plan is the non-active / primary flight plan that the pilot can examine before accepting it. The flight procedure data in the updated data relates to the updated route. The verb "relate" used herein means that the flight procedure data is relative to the vicinity of the updated route. The neighborhood could be defined as a tunnel delimiting a band around a position, including but not limited to latitude and longitude, altitude or time. The neighborhood could also include a predetermined area around the destination airport or a predetermined area around a range of other possible airports. The information received in the updated data can then be used, in 308, to create a route to follow on the updated route. In particular, the VMS or the crew may use the flight procedure data received in the updated data to establish the flight conditions of the aircraft on the updated route. The VMS may also provide the information received in the updated data to other systems present in the aircraft 10, including the autopilot system or an electronic cockpit organizer on board. Thus, in the case where a CCA electronically transmits route clearances or waypoints to the aircraft 3035711 21, the computer 22, 122 constituting at least a portion of the SBV can then charge the clearance or clearance. waypoint in the VMS where he / she can be inserted into the flight plan that will be used to guide the aircraft 10 during the flight. The method 300 is flexible and is presented for illustrative purposes only. For example, the order of the steps described is purely illustrative and is in no way intended to limit the process 300, it being understood that the steps may take place in a different logical order or that additional or intermediate steps may be included without There is no departure from embodiments of the invention. By way of non-limiting example, it is envisaged that the VMS can determine if the updated route contains procedures that are not present in the database and the VMS can issue an alert in the aircraft 10 that the updated route contains missing procedures in the database. This may include the fact that an alert can be communicated to the crew in the cockpit of the aircraft 10. Whatever the trigger event, the flight procedure data received in the updated data does not enter as part of the routine maintenance of the database component 40, 140 or the additional database component 144 of the SGV. Among the technical effects of the embodiments described above, information may be provided to an otherwise static database including, but not limited to, the navigation database of an aircraft, which currently has a refresh cycle. predetermined rigid (e.g. 28 days), where it is currently not possible to update the database 30 other than in the context of the cycle. In this way, up-to-date procedures can be dynamically transmitted to the aircraft's VMS and can be updated automatically based on route clearances communicated by a CCA, daily or hourly, to reflect changes. 5 of procedures, or on the basis of changing atmospheric conditions, including strong winds or disturbances. In this way, the flight crew can select in the flight plan newly loaded procedures by allowing the aircraft to fly according to a procedure. Still further, the embodiments described above may allow optimized procedures depending on weather conditions. In addition, the embodiments described above can update the database using a format already included in the database. The embodiments described above provide savings on maintenance activities, since the databases can be dynamically updated instead of being updated in a rigid manner. Since they have not already been described, the various details and structures of the various embodiments can, if desired, be used in combination with each other. The fact that a detail may not be illustrated in all of the embodiments is not intended to be interpreted as meaning that it can not be, it is only intended for a greater conciseness of the description. Thus, the various details of the various embodiments can be mixed and adapted as desired to create new embodiments, whether the new embodiments are expressly described or not. All combinations or permutations of details described herein are covered by this disclosure.
    [0010] 30 3035711 23 List of marks 10 Aircraft 12 Engine 5 14 Fuselage 16 Cockpit 18 Wing wings 20 On-board systems 22 Computer 10 24 Communication link 26 Memory 28 Processor 30 Remote server 32 Ground station 15 34 Database 36 Processor 38 SGV 40 Database component 42 Update module 20 120 Autopilot system 122 Computer 124 Radio communication link 126 Memory 128 Processor 25 138 SGV 140 Database component 142 Update module 144 Additional database component 146 Integrity Module 30 148 Electronic Cockpit Organizer 3035711 24 200 Method 202 Possible trigger event 204 Request updated data for a route to follow 5 206 Receipt of flight procedure data in updated data 208 Creation of a route to track using flight procedure data in the updated data 300 Method 10 302 Receiving an updated route 304 Requesting updated data for an updated route 306 Receiving flight procedure data in updated data 15 308 Creating a route to follow on the updated route using the data of flight procedures in the updated data
    权利要求:
    Claims (10)
    [0001]
    REVENDICATIONS1. A method (200) for providing updated data to an aircraft (10), the method comprising: requesting (204), by an update module (42, 142) of the aircraft (10), updated data for an route to be followed by the aircraft (10); receiving (206), by a member of the aircraft (10), via a communication link (24,124), updated data including flight procedure data transmitted from a ground station (32), response to the request; and updating (208) the route to be followed, at least in part based on the flight procedure data.
    [0002]
    2. The method of claim 1, wherein the member is a flight management system (38, 138) of the aircraft (10).
    [0003]
    The method of claim 2, further comprising issuing an alert in the aircraft (10) when one of the updated data is available for a flight procedure maintained in the flight management system.
    [0004]
    The method of claim 1, wherein the route comprises a route defined during the flight of the aircraft (10) and the request is made in response to the definition of the route.
    [0005]
    The method of claim 1, wherein the request (204) comprises the request for a subscription to a procedure so that updated data on the procedure is sent automatically.
    [0006]
    The method of claim 1, wherein the route is a predefined route established prior to the flight of the aircraft (10). 3035711 26
    [0007]
    The method of claim 1, wherein receiving (206) the flight procedure data includes inserting the flight procedure data into a flight plan of the aircraft.
    [0008]
    The method of claim 1, wherein the request (204) is automatically submitted during departure preliminaries or during the flight.
    [0009]
    The method of claim 1, wherein the received flight procedure data is synchronized directly into a database. 10
    [0010]
    The method of claim 1, wherein the request (204) for the updated data is automatically submitted after a trigger event (202).
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    FR3026214A1|2016-03-25|METHOD FOR MANAGING ALERTS
    FR3038751A1|2017-01-13|METHOD FOR INTEGRATING A CONSTRAINED ROAD OPTIMIZATION APPLICATION IN AN OPEN ARCHITECTURE AIRCRAFT SYSTEM OF CLIENT-TYPE SERVER
    WO2006106206A1|2006-10-12|Method and device for displaying part of an airport on a viewing screen
    FR3076679A1|2019-07-12|Systems and methods for autonomous distress locating in air vehicles
    CA3020086A1|2019-04-20|Control process for alert restitution and/or system reconfiguration procedures, associated computer program and control systems
    同族专利:
    公开号 | 公开日
    GB2540010B|2020-01-22|
    GB2540010A|2017-01-04|
    GB201911633D0|2019-09-25|
    US20160328978A1|2016-11-10|
    FR3035711B1|2021-09-24|
    GB2573718B|2020-03-04|
    GB2573718A|2019-11-13|
    US10068488B2|2018-09-04|
    GB201607486D0|2016-06-15|
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    法律状态:
    2017-04-26| PLFP| Fee payment|Year of fee payment: 2 |
    2018-04-25| PLFP| Fee payment|Year of fee payment: 3 |
    2018-11-02| PLSC| Search report ready|Effective date: 20181102 |
    2019-03-25| PLFP| Fee payment|Year of fee payment: 4 |
    2020-03-19| PLFP| Fee payment|Year of fee payment: 5 |
    2021-03-23| PLFP| Fee payment|Year of fee payment: 6 |
    优先权:
    申请号 | 申请日 | 专利标题
    US14/700,485|US10068488B2|2015-04-30|2015-04-30|Systems and methods of providing a data update to an aircraft|
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