• 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:
    aircraft avionics system, and tablet interface module. an aircraft avionics system including an aircraft interface device configured to communicate with an aircraft avionics system and a tablet interface module configured to communicate with the aircraft interface device and with one or more tablets. the aircraft avionics system includes a plurality of sensors for an aircraft and the tablet interface module provides the one or more tablets with information received from the aircraft interface device.
    公开号:BR102013023059B1
    申请号:R102013023059-6
    申请日:2013-09-09
    公开日:2021-08-17
    发明作者:William J. Baumgarten；Michael J. Haukom；Thomas J. Horsager；Daniel L. Mcdowell
    申请人:Rosemount Aerospace Inc；
    IPC主号:
    专利说明:

    Fundamentals of the Invention
    [0001] The present disclosure relates to the field of aircraft avionics and more specifically to an aircraft avionics tablet interface module.
    [0002] Aircraft avionics systems include a large number of sensors, communication systems and navigation systems that can be used during aircraft operation and for aircraft maintenance. Currently available avionics systems include one or more dials that can be used by operators for various functions.
    [0003] As the use of tablet computing devices becomes more prevalent, many aircraft operators would like to use these tablet devices to interface with the aircraft avionics system. However, due to reliability, warranty and safety reasons, aircraft avionics systems are typically closed systems which do not allow operators to use non-integrated electronics, such as commercially available tablet devices, to communicate with the avionics system. Also, due to possible interference that may be caused by such tablet devices, the use of tablet devices on the aircraft flight deck has been restricted. Brief Description of the Invention
    [0004] According to an embodiment, an aircraft avionics system includes an aircraft interface device configured to communicate with an aircraft avionics system and a tablet interface module configured to communicate with the aircraft interface device and with one or more tablets. The aircraft avionics system includes a plurality of sensors for an aircraft and the tablet interface module provides the one or more tablets with information received from the aircraft interface device.
    [0005] According to another embodiment, a tablet interface module includes a first transceiver configured to communicate with one or more tablets and a second transceiver configured to communicate with an aircraft interface device. The tablet interface module also includes a user interface module. The tablet interface module is configured to receive information regarding a plurality of sensors for an aircraft from an aircraft interface device and transmit the information to the one or more tablets.
    [0006] Additional advantages and characteristics are achieved by the techniques of the present invention. Other embodiments and other aspects of the invention are described in detail herein and are considered a part of the claimed invention. For a better understanding of the invention with its advantages and characteristics, please refer to the description and drawings. Brief Description of Drawings
    [0007] The subject matter which is considered as the invention is particularly highlighted and distinctly claimed in the claims at the end of the descriptive report. The foregoing and other features and advantages of the invention are apparent from the following detailed description taken in conjunction with the accompanying drawings in which: FIG. 1 is a block diagram of a system including a tablet interface module and an aircraft interface device in accordance with an embodiment of the disclosure; FIG. 2 is a block diagram of the tablet interface module according to an embodiment of the disclosure; and FIG. 3 is a block diagram of an aircraft interface device in accordance with an embodiment of the disclosure. Detailed Description of the Invention
    [0008] Referring now to FIG. 1, a block diagram of a system 100 in accordance with an embodiment of the disclosure is shown. As illustrated, system 100 includes an aircraft avionics system 102, an aircraft interface device 104, a tablet interface module 106, and a tablet 108. In some exemplary embodiments or embodiments, the aircraft avionics system 102 may include, but is not limited to, multiple sensors, communications systems, and navigation systems. Aircraft avionics system 102 provides data to aircraft interface device 104 which acts as a data concentrator for aircraft avionics system 102. In one embodiment, aircraft interface device 104 is configured for connection to one or more operationally approved devices and to act as a partition between the aircraft avionics system 102 and the operationally approved devices. In one embodiment, the tablet interface module 106 is an operationally approved device that can be connected to the aircraft interface device 104. The tablet interface module 106 in such an embodiment is configured to subscribe to application-requested data received from the module. interface module 104. In one embodiment, tablet 108 is configured to communicate, either wired or wireless, with tablet interface module 106 using any suitable communications protocol. As used herein, the term “tablet” refers to any commercially available tablet computing device, smartphone, laptop or other mobile computing device.
    [0009] In one embodiment, the use of the tablet interface module 106 and the aircraft interface device 104 allows aircraft operators to use commercially available tablets 108 to receive data from the aircraft avionics system 102 without requiring the tablets 108 are certified devices. In one embodiment, system 100 can be used for both in-flight operations and maintenance functions. For example, system 100 can be used to store flight log data, pilot reports, aircraft fault isolation applications, aircraft troubleshooting, move map applications and administrative communications functions. In one embodiment, the tablet interface module 106 is configured to be mounted to an interior wall of an aircraft on the flight deck so that aircraft operators on the flight deck can easily access the tablet interface module 106.
    [00010] Referring now to FIG. 2, a block diagram of a tablet interface module 200 in accordance with an embodiment of the disclosure is shown. As illustrated, tablet interface module 200 can include a wireless transceiver 202, a wired transceiver 204, a user interface 206, and a processor 208. The wireless transceiver 202 is configured to communicate with one or more tablets and can be configured to use a variety of known wireless communications protocols. For example, the wireless transceiver 202 can be configured to communicate with tablets via Wi-Fi, Bluetooth or something similar. Wired transceiver 204 is configured to communicate with the tablet and aircraft interface device and can be configured to use a variety of known wired communications protocols. For example, the wired transceiver 204 can be configured to communicate with tablets via Ethernet (using TCP/IP, UDP or similar), a serial connection (using SSP, SIP or something similar) (ie 232/422/485 ), or something like this. In exemplary embodiments, wired transceiver 204 can also be configured to communicate with one or more tablets. The tablet interface module 200 also includes a processor 208 which can be any custom or commercially available processor, a central processing unit (CPU), an auxiliary processor among multiple processors, a microprocessor-based semiconductor (in the form of a microchip or chip assembly), a macroprocessor, or generally any device for executing instructions.
    [00011] In one embodiment, the tablet interface module 200 includes a user interface 206 that is configured to enable a user to connect the tablet interface module 200 to a tablet, such as, in a non-limiting example, the tablet 108 shown in FIG. 1. In addition, user interface 206 may include an indicator which is configured to indicate whether tablet interface module 200 is connected to a tablet. In one example, the wireless transceiver 202 is configured to use Bluetooth to communicate with the tablet and the user interface 206 includes a pair button which allows the tablet user to connect the tablet to the tablet interface module 200. user interface indicator 206 may be a light indicating that a tablet is connected to tablet interface module 206. In one embodiment, tablet interface module 200 may be configured to connect to multiple tablets and user interface 206 may include a plurality of pair buttons and indicator lights.
    [00012] In one embodiment, the tablet interface module 200 may also include a battery 212 and/or power source 210. In one embodiment, the tablet interface module 200 may include a power source 210 that is configured to conditioning power received from the aircraft interface device and isolating the tablet interface module 200 from the aircraft power system. In one embodiment, the tablet interface module 200 can be configured to operate exclusively without power received from battery 212 and can have a low power design. In one embodiment, the tablet interface module 200 can be configured to connect to multiple tablet devices and can include a physical connection port for connecting to tablet devices to provide charging and communications between the tablet interface module 200 and the tablet. For example, the tablet interface module 200 can include one or more universal serial bus (USB) connectors for connecting to tablet devices.
    [00013] In one embodiment, the wireless transceiver 202 of the tablet interface module 200 can be selected or designed to provide a low-power, low-visibility communications link for the tablet. For example, the wireless transceiver 202 can be selected to be a Bluetooth 4.0, IEEE 802 or similar capable device. The wireless transceiver 202 is designed so that it is able to communicate with tablets in close proximity to the tablet interface module 200 and so that the signals it emits do not interfere with the aircraft's electronics. In one embodiment, the tablet interface module 200 is configured to provide multiple layers of security to prevent unauthorized access to the tablet interface module 200. Physical access to the tablet interface module 200 is limited to individuals authorized to access the deck flight where the tablet 200 interface module is located. Also, the tablet interface module 200 is configured so that pairing or connection to the tablet interface module 200 can only be initiated from the tablet interface module 200 and not a tablet device. In addition, the tablet interface module 200 wireless transceiver 202 can be configured to encrypt data that is transmitted.
    [00014] Referring now to FIG. 3, a block diagram of an aircraft interface device 300 in accordance with an embodiment of the disclosure is shown. As illustrated, the aircraft interface device 300 includes a communications port 302, a storage device 304, and a processor 306. The communications port 302 is configured to connect the aircraft interface device 300 to both the tablet interface module. as for the aircraft avionics system. In one embodiment, storage device 304 is configured to store data received from the aircraft avionics system. Storage device 304 may include, but is not limited to, any one or a combination of volatile memory elements (e.g., random access memory (RAM, such as DRAM, SRAM, SDRAM, etc.) and memory elements non-volatile (eg ROM, erasable programmable read-only memory (EPROM), electronically erasable programmable read-only memory (EEPROM), programmable read-only memory (PROM), tape, compact disk read-only memory (CD- ROM), disk, floppy disk, cartridge, cassette or the like, etc.) In addition, the storage device 304 may incorporate electronic, magnetic, optical and/or other types of storage media. aircraft 300 also includes a processor 306 which can be any custom or commercially available processor, a central processing unit (CPU), an auxiliary processor among multiple processors, a microprocessor semiconductor-based (in the form of a microchip or chip assembly), a macroprocessor, or generally any device for executing instructions.
    [00015] In one embodiment, the communications port 302 may include multiple interfaces to receive information from various components of the aircraft avionics system and to communicate with the tablet interface module. For example, aircraft interface device 300 may include, but is not limited to, an Ethernet interface, an ARINC 429 interface, an ARINC 717 interface, a USB interface, an RS-232 interface, an RS-422 interface, an RS-485 interface, an SPI interface, an I2C interface or the like to communicate with the aircraft avionics system and/or the tablet interface module. In one embodiment, by connecting a tablet to the aircraft interface device via the tablet interface module, the tablet is able to access information regarding the entire aircraft avionics system.
    [00016] In one embodiment, aircraft interface device 300 may include a power source 308 that is configured to condition power received from an aircraft power system and provide power to the tablet interface module. The 308 power supply is also configured to isolate the tablet interface module from the aircraft power system.
    [00017] Although the invention has been described in detail with respect to only a limited number of embodiments, it should be readily understood that the invention is not limited to such disclosed embodiments. Rather, the invention may be modified to incorporate any number of variations, alterations, substitutions or equivalent arrangements not heretofore described, but which are compatible with the spirit and scope of the invention. Furthermore, although various embodiments of the invention have been described it will be understood that aspects of the invention may include only some of the described embodiments. Therefore, the invention is not to be seen as limited by the above description, but it is only limited by the scope of the appended claims.
    权利要求:
    Claims (7)
    [0001]
    1. Aircraft avionics system (102), the system comprising: a plurality of sensors for an aircraft; an aircraft interface device (104, 300) configured to communicate with the aircraft avionics system (102); and a tablet interface module (106, 200) configured to communicate with the aircraft interface device (104, 300) and with one or more tablets (108), wherein the tablet interface module (106, 200) provides the one or more tablets (108) with information received from the aircraft interface device (104, 300), which tablet interface module comprises: a wireless transceiver (202) configured to communicate with the one or more tablets (108 ); a transceiver (204) configured to communicate with the aircraft interface device (104, 300); and a user interface (206) configured to establish a communication channel between the tablet interface module (200) and the one or more tablets (108) via the wireless transceiver (202), characterized in that: a user interface includes a configured indicator to indicate whether the tablet interface module is connected to a tablet, the tablet interface is configured so that the communication channel can be established only by initiation from the tablet interface module and not from one or more tablets, and the communication channel is encrypted by the wireless transceiver.
    [0002]
    2. Aircraft avionics system (102) according to claim 1, characterized in that the aircraft interface device (104, 300) is configured to store data received from the aircraft avionics system (102).
    [0003]
    3. Aircraft avionics system (102) according to any one of claims 1 or 2, characterized in that the aircraft interface device (104, 300) acts as a divider between the aircraft avionics system ( 102) and the tablet interface module (106, 200).
    [0004]
    4. Aircraft avionics system (102) according to any one of claims 1 to 3, characterized in that the aircraft interface device (104, 300) is configured to condition energy received from a power system. an aircraft and isolate the tablet interface module (106, 200) from the aircraft power system.
    [0005]
    5. Aircraft avionics system (102) according to claim 1, characterized in that the wireless transceiver (202) is a low-power, low-visibility radio frequency transceiver.
    [0006]
    6. Aircraft avionics system according to claim 5, characterized in that the tablet interface module (200) further comprises a power source (210) configured to connect to an aircraft power system and to supply power to the one or more tablet devices (108).
    [0007]
    7. Aircraft avionics system (102) according to any one of claims 5 or 6, characterized in that the power source (210) is configured to condition energy received from the aircraft power system and isolate the ones. or more tablets (108) from the aircraft power system.
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    法律状态:
    2015-08-11| B03A| Publication of a patent application or of a certificate of addition of invention [chapter 3.1 patent gazette]|
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    2021-08-17| B16A| Patent or certificate of addition of invention granted [chapter 16.1 patent gazette]|Free format text: PRAZO DE VALIDADE: 20 (VINTE) ANOS CONTADOS A PARTIR DE 09/09/2013, OBSERVADAS AS CONDICOES LEGAIS. |
    优先权:
    申请号 | 申请日 | 专利标题
    US13/608,100|US9334063B2|2012-09-10|2012-09-10|Aircraft avionics tablet interface module|
    US13/608,100|2012-09-10|
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