• 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:
    This hybrid avionic information transmission architecture, of the type comprising subscriber stations (2, 3, 4, 5, 6, 7) connected by information transmission means (8), is characterized in that the stations ( 2, 3, 4, 5, 6, 7) are connected on the one hand by first information transmission means (9, 10) to their neighbors to form at least one first closed ring information transmission network. between the stations and secondly by second information transmission means (11) to communication plane central switch means (12) for forming at least one second star information transmission network between the stations and the central plane switch means.
    公开号:FR3032078A1
    申请号:FR1500125
    申请日:2015-01-22
    公开日:2016-07-29
    发明作者:Patrice Georges Paul Toillon；David Jose Faura；Champeaux Paul Marie Boivin；Vincent Christophe Cedric Sollier
    申请人:Thales SA；
    IPC主号:
    专利说明:

    [0001] The present invention relates to a hybrid avionic information transmission architecture and a hybrid transmission system comprising such architectures. The present application is therefore placed in the context of avionics communication networks and in particular, but not only, those based on the concept of integrated modular avionics also called IMA. This concept requires the implementation of shared processing resources supporting one or more application software as well as shared communication resources as well as shared input / output resources. Such a concept then makes use of spatial and temporal partitioning properties allowing independent and deterministic processing and exchanges of information.
    [0002] This is based for example on standards A653 and A664 well known in the state of the art. A corresponding avionics architecture based on the concept of integrated modular avionics IMA, must provide generic computing platforms (computers) where one or more software applications run to ensure the execution of avionics functions, the operational safety and the safety of the aircraft. In addition, this architecture shall provide applications with standardized communication services in the form of an avionics backbone (eg A664 standard), capable of carrying any type and size of data, and one or more avionics secondary networks (of the CAN bus type, A429, etc.) that can serve in particular as a back-up network and / or for conveying so-called critical data. In the case of the main network, the communication service must allow access and sharing of communication resources, through the use of an ES end system, which allows applications of a computer to access the network. , consisting of a set of switches (also called switches in English) interconnected, which deals with routing the messages only to the destination applications. But avionics systems have very real time constraints. The communication architecture must implement mechanisms to ensure that data transmitted between two applications is available, transmitted in a maximum time and integrity.
    [0003] The object of the invention is to propose an architecture that makes it possible to best meet these different requirements. For this purpose, the subject of the invention is a hybrid avionic information transmission architecture, of the type comprising subscriber stations connected by information transmission means, characterized in that the stations are connected on the one hand by first means for transmitting information to their neighbors to form at least a first closed ring information transmission network between the stations and secondly for second information transmission means to central communication plane for forming at least a second star information transmission network between the stations and the central plane switch means. According to other features of the architecture according to the invention, taken alone or in combination - each station comprises means for subscribing to the first and second networks comprising at least four communication ports, one of which is connected to resources of the network. station, two to the neighboring stations in the first ring network and one to the plan switch means in the second star network; the subscription means of the station include means for broadcasting the information produced by the resources of this station, to a port or some of the ports or all the ports of the subscription means of this station; networks are full duplex networks; the ring and star information transmission networks implement identical communication protocols; ring and star networks implement different communication protocols; the ring and star information transmission networks use identical physical layers; the ring and star networks use different physical layers; It comprises at least two star connection switch means of the stations for forming at least one second star network between the stations and each of the switch means; the networks are adapted to transmit information of different natures including critical information; At least one of the networks is a backup network of another; The switch means comprise means for timing the operation of the subscriber stations. According to another aspect, the invention also relates to a hybrid avionics information transmission system, characterized in that it comprises at least two hybrid architectures as described above, associated. According to other features of this system, taken alone or in combination: the architectures are associated with at least one of their switching means; The architectures are associated at the level of at least one of their stations. The invention will be better understood with the aid of the description which follows, given solely by way of example and with reference to the appended drawings, in which; FIG. 1 represents a general view of a hybrid architecture according to the invention; FIG. 2 represents a detailed view of connection means of a station forming part of the constitution of such an architecture; FIG. 3 represents an alternative embodiment of an architecture according to the invention; FIG. 4 illustrates the connection of two architectures as described in a hybrid system according to the invention; and FIGS. 5 and 6 are block diagrams illustrating two alternative embodiments of such a system. The aim of the invention is therefore to propose a scalable hybrid network architecture solution that is both distributed and centralized.
    [0004] It must also allow communication between one or more avionics applications regardless of the location of this or applications in the avionics system. The invention, by virtue of the combination of two communication structures of different types, namely centralized and distributed, which can be applied to similar or dissimilar physical and logical layers, and thanks to these data transmission mechanisms, confers to this hybrid network architecture, both the advantages of centralized type architectures and those of distributed type architectures. This optimally meets the communication needs of avionic systems.
    [0005] FIG. 1 illustrates an exemplary embodiment of such a hybrid architecture. This is designated by the general reference 1 in this figure and it can be seen that it comprises several subscriber stations, designated by the references 2, 3, 4, 5, 6 and 7 respectively. These stations are connected by means of information transmission designated by the general reference 8. In fact and as illustrated, the stations 2 to 7 are connected on the one hand by first information transmission means, their neighboring regions, to form at least a first closed ring information transmission network between the stations and secondly by second information transmission means, to central communication plane switch means, to minus a second star information transmission network between the stations and the central plane switch means.
    [0006] In this FIG. 1, the stations, such as the station 2, are connected to their neighbors, such as the stations 3 and 7, by first information transmission means designated by the general references 9 and 10 respectively. for example, to form at least a first closed ring (or loop) information transmission network between the different interconnected stations. Furthermore, the stations, such as the station 2, are also connected by second information transmission means designated for example by the general reference 11, to means forming a central communication plane switch, one of which is designated by the general reference numeral 12 in this FIG. 1, to form at least a second star information transmission network between the stations 2 to 7 and these communication plane central switch means, designated by the general reference 12. L The combination of these two communication domains, namely the ring peripheral domain and the star central domain, thus forms an avionic communication plane to which each subscriber station or avionics equipment is connected. Each area of communication is independent of the other and has its own autonomy and its own mathematical temporal model. The central communication domain is based, for example, on a frame switch based communication technology, using one or more dedicated switch-type avionics (or switches in English) or one or more avionics subassemblies. distributed switch type, providing the function of centralized intermediate systems. The topology of the domains is therefore centralized or in a star and the central communication domain is for example based on a standard of the ARINC 664 or Ethernet 5 IEEE 802.3 type. This central area of communication is based on the controlled propagation of the frames. According to the availability objectives of the supported avionic systems, the central communication domain may be redundant, the central domain providing direct interconnection between the subscriber stations. The peripheral domain, constituted by the closed ring network, is based for example on a frame circulation communication technology using mechanisms of the type circulators or elementary switches distributed and installed in each of the subscriber avionics equipment.
    [0007] This peripheral communication domain is based on a closed topology, such as for example a loop or a ring, and on the systematic and controlled propagation of frames with a strong dissociation between each of the two domains (transmission, filtering principles, etc.) leading to a mathematical temporal model different from that of the central domain.
    [0008] The peripheral communication domain may be based on a standard of the ARINC 664 or Ethernet IEEE 802.3 type, allowing a direct and controlled association, without modification of the frame within a communication plane, resulting in end-to-end exchanges, without frame modification for supported systems.
    [0009] But in a desire to increase the dissymmetry between the two communication domains, the peripheral domain could be, for example, of another type (point-to-point serial link, etc.). The communication between the various avionics communication plans located or not in different physical zones of the aircraft is performed at the level of the frames. The association between the various avionic communication plans is achieved by direct links between the switches of each of the communication plans via physical communication ports having complementary mechanisms and capabilities. The communication between central switches is carried out without changing the frame, from one communication plane to the other, and this on a principle of controlled propagation of the frame.
    [0010] Thus, these mechanisms and capabilities implement, for example, more substantial means for intermediate storage of frames in the two directions of circulation, as well as control / filtering mechanisms ensuring the monitoring / isolation at the passage of a communication plane. avionics to other avionics communication planes in both directions. In case of no authorization or in case of excessive aging, the associated frame is not inserted in the other communication plane with the indication of such a situation. As illustrated in FIG. 2, each station has means for subscribing to the first and second networks. These subscription means comprise for example at least four communication ports. In this FIG. 2, the station is, for example, the station designated by the general reference 2 in FIG. 1 and the latter comprises, for example, subscription means 15 designated by the general reference 15. As indicated previously, the station comprises resources such as for example a calculator 16 (or any other resource) and one of the communication ports of the subscription means, constituted for example by the port designated by the general reference 17, is associated with this calculator or any other resource from this station. Two other ports respectively 18 and 19, are associated with the neighboring stations in the first ring network, thanks to the connecting means for example 20 and 21 Finally another port such as for example the port 22, is associated with the means 25 forming plan switch in the second star network. It is conceivable that such a structure has a certain number of advantages and that different modes of operation of these different elements can be envisaged. Thus, for example, the subscription means of the station may include means for broadcasting the information produced by the resources of this station to a port or some of the ports or all the ports of these subscription means of this station. Thus the distribution of the frames can be perfectly controlled and managed. It should be noted that the networks may be Full Duplex (Duplex) networks and that these ring or star data transmission networks may implement identical or different communication protocols and use identical or different physical layers. It is thus possible, for example, to find wired or non-wired connection means, etc. It is then conceivable that these networks may be adapted to transmit information of different natures, including for example critical information, and that at least one of one of the networks can be for example a back-up network of another of these networks. As indicated above, the timing of the operation of the different stations can be controlled.
    [0011] This control can for example be carried out at the central plane switch means, which can then comprise means for generating timing signals for the operation of the subscriber stations. These signals are thus for example transmitted to the stations from these switch means.
    [0012] As illustrated in FIG. 3, it is also possible to use at least two means for forming a star connection of the stations. These two switch means are then adapted to form at least a second star network between the stations and each of these switch means in parallel with the first star network.
    [0013] In this FIG. 3, the two switch means are designated by references 25 and 26 respectively and the stations are then connected to each of these two switch means in a configuration of two second star networks. FIGS. 4, 5 and 6 show various possible embodiments of hybrid avionic information transmission systems, which comprise at least two hybrid architectures as described above, associated with each other. 4, 5 and 6, hybrid architectures designated by the references 30 and 31 in FIG. 4, 32 and 33 in FIG. 5 and 34 and 35 respectively in FIG. the hybrid architectures 30 and 31 are associated at their central plane switch means, as designated by references 36 and 37. In FIG. 5 and FIG. 6, two embodiments are shown in FIG. which hybrid architectures are associated at at least one of their stations and at at least one of their stations and their communication plane switch means, respectively. In these figures, examples of embodiments of multiple communication plane architectures have also been illustrated, for example for what is called a cabinet in the avionics field. It will be understood that such an architecture and system structure is of particular interest, insofar as this is a hybrid structure which can for example be a multi-plane communication structure, both robust and scalable. It is possible to implement asymmetric or different or, on the contrary, symmetrical or identical structures, in the two networks, and an avionic system 10 implementing this design, may for example have an integrated backup network. The communication plan also simplifies the organization of communications and their association and increases the availability of information over any other conventional network.
    [0014] Of course, still other embodiments of this architecture can be envisaged.
    权利要求:
    Claims (15)
    [0001]
    CLAIMS1.- Hybrid avionic information transmission architecture, of the type comprising subscriber stations (2, 3, 4, 5, 6, 7) connected by information transmission means (8), characterized in that the stations (2, 3, 4, 5, 6, 7) are connected on the one hand by first information transmission means (9, 10) to their neighbors to form at least one first ring information transmission network closed between the stations and secondly by second information transmission means (11) to central communication plane switch means (12) for forming at least one second star information transmission network between stations and means forming a central plane switch.
    [0002]
    2. Architecture according to claim 1, characterized in that each station (2) comprises means for subscribing (15) to the first and second networks comprising at least four communication ports of which one (17) is connected to resources ( 16) of the station, two (18, 19) to the neighboring stations in the first ring network and one (22) to the plan switch means in the second star network.
    [0003]
    3. Architecture according to claim 2, characterized in that the subscription means of the station comprise means for broadcasting the information produced by the resources of this station to a port or some of the ports or all ports (17, 18, 19, 22) of the subscription means (15) of this station.
    [0004]
    4. Architecture according to any one of the preceding claims, characterized in that the networks are full duplex networks.
    [0005]
    5. Architecture according to any one of the preceding claims, characterized in that the ring and star information transmission networks implement identical communication protocols.
    [0006]
    6. Architecture according to any one of claims 1 to 5, characterized in that the ring and star networks implement different communication protocols.
    [0007]
    7. Architecture according to any one of the preceding claims, characterized in that the ring and star information transmission networks implement identical physical layers.
    [0008]
    8. Architecture according to any one of claims 1 to 6, characterized in that the ring and star networks implement different physical layers. 3032078 10
    [0009]
    9. Architecture according to any one of the preceding claims, characterized in that it comprises at least two means forming a switch (25, 26) star connection stations to form at least a second star network between the stations and each of the switch means. 5
    [0010]
    10. Architecture according to any one of the preceding claims, characterized in that the networks are adapted to transmit information of different natures including critical information.
    [0011]
    11. Architecture according to any one of the preceding claims, characterized in that at least one of the networks is a backup network of another. 10
    [0012]
    12. Architecture according to any one of the preceding claims, characterized in that the switch means comprise means for timing the operation of the subscriber stations.
    [0013]
    13. Hybrid avionic information transmission system, characterized in that it comprises at least two hybrid architectures (30, 31; 32, 33; 34, 35) according to any one of the preceding claims, associated.
    [0014]
    14.- System according to claim 13, characterized in that the architectures are associated at the level of at least one of their means forming a switch.
    [0015]
    15.- System according to claim 13 or 14, characterized in that the architectures are associated at the level of at least one of their stations.
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    引用文献:
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    法律状态:
    2016-02-01| PLFP| Fee payment|Year of fee payment: 2 |
    2016-07-29| PLSC| Publication of the preliminary search report|Effective date: 20160729 |
    2017-01-31| PLFP| Fee payment|Year of fee payment: 3 |
    2018-01-31| PLFP| Fee payment|Year of fee payment: 4 |
    2020-01-30| PLFP| Fee payment|Year of fee payment: 6 |
    2021-01-28| PLFP| Fee payment|Year of fee payment: 7 |
    2022-01-31| PLFP| Fee payment|Year of fee payment: 8 |
    优先权:
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    FR1500125A|FR3032078B1|2015-01-22|2015-01-22|HYBRID AVIONIC INFORMATION TRANSMISSION ARCHITECTURE AND CORRESPONDING SYSTEM|FR1500125A| FR3032078B1|2015-01-22|2015-01-22|HYBRID AVIONIC INFORMATION TRANSMISSION ARCHITECTURE AND CORRESPONDING SYSTEM|
    US15/003,603| US10469323B2|2015-01-22|2016-01-21|Hybrid architecture for avionics data transmission and corresponding system|
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