US20030003872A1 - Methods and apparatus for wireless upload and download of aircraft data - Google Patents

Methods and apparatus for wireless upload and download of aircraft data Download PDF

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Publication number
US20030003872A1
US20030003872A1 US10075083 US7508302A US2003003872A1 US 20030003872 A1 US20030003872 A1 US 20030003872A1 US 10075083 US10075083 US 10075083 US 7508302 A US7508302 A US 7508302A US 2003003872 A1 US2003003872 A1 US 2003003872A1
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data
aircraft
communication
avionics
arinc
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US10075083
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Roger Brinkley
Timothy Mitchell
Jerry Price
David Lee
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Boeing Co
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Boeing Co
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    • HELECTRICITY
    • H04ELECTRIC COMMUNICATION TECHNIQUE
    • H04LTRANSMISSION OF DIGITAL INFORMATION, e.g. TELEGRAPHIC COMMUNICATION
    • H04L67/00Network-specific arrangements or communication protocols supporting networked applications
    • H04L67/06Network-specific arrangements or communication protocols supporting networked applications adapted for file transfer, e.g. file transfer protocol [FTP]
    • GPHYSICS
    • G06COMPUTING; CALCULATING; COUNTING
    • G06FELECTRIC DIGITAL DATA PROCESSING
    • G06F8/00Arrangements for software engineering
    • G06F8/60Software deployment
    • G06F8/61Installation
    • HELECTRICITY
    • H04ELECTRIC COMMUNICATION TECHNIQUE
    • H04BTRANSMISSION
    • H04B7/00Radio transmission systems, i.e. using radiation field
    • H04B7/14Relay systems
    • H04B7/15Active relay systems
    • H04B7/185Space-based or airborne stations; Stations for satellite systems
    • H04B7/18502Airborne stations
    • H04B7/18506Communications with or from aircraft, i.e. aeronautical mobile service
    • HELECTRICITY
    • H04ELECTRIC COMMUNICATION TECHNIQUE
    • H04LTRANSMISSION OF DIGITAL INFORMATION, e.g. TELEGRAPHIC COMMUNICATION
    • H04L67/00Network-specific arrangements or communication protocols supporting networked applications
    • H04L67/04Network-specific arrangements or communication protocols supporting networked applications adapted for terminals or networks with limited resources or for terminal portability, e.g. wireless application protocol [WAP]
    • HELECTRICITY
    • H04ELECTRIC COMMUNICATION TECHNIQUE
    • H04LTRANSMISSION OF DIGITAL INFORMATION, e.g. TELEGRAPHIC COMMUNICATION
    • H04L67/00Network-specific arrangements or communication protocols supporting networked applications
    • H04L67/12Network-specific arrangements or communication protocols supporting networked applications adapted for proprietary or special purpose networking environments, e.g. medical networks, sensor networks, networks in a car or remote metering networks
    • HELECTRICITY
    • H04ELECTRIC COMMUNICATION TECHNIQUE
    • H04LTRANSMISSION OF DIGITAL INFORMATION, e.g. TELEGRAPHIC COMMUNICATION
    • H04L67/00Network-specific arrangements or communication protocols supporting networked applications
    • H04L67/34Network-specific arrangements or communication protocols supporting networked applications involving the movement of software or configuration parameters
    • HELECTRICITY
    • H04ELECTRIC COMMUNICATION TECHNIQUE
    • H04LTRANSMISSION OF DIGITAL INFORMATION, e.g. TELEGRAPHIC COMMUNICATION
    • H04L12/00Data switching networks
    • H04L12/28Data switching networks characterised by path configuration, e.g. local area networks [LAN], wide area networks [WAN]
    • H04L12/40Bus networks
    • H04L2012/40267Bus for use in transportation systems
    • H04L2012/4028Bus for use in transportation systems the transportation system being an aircraft
    • HELECTRICITY
    • H04ELECTRIC COMMUNICATION TECHNIQUE
    • H04WWIRELESS COMMUNICATIONS NETWORKS
    • H04W84/00Network topologies
    • H04W84/005Moving wireless networks
    • HELECTRICITY
    • H04ELECTRIC COMMUNICATION TECHNIQUE
    • H04WWIRELESS COMMUNICATIONS NETWORKS
    • H04W84/00Network topologies
    • H04W84/02Hierarchically pre-organised networks, e.g. paging networks, cellular networks, WLAN [Wireless Local Area Network] or WLL [Wireless Local Loop]
    • H04W84/04Large scale networks; Deep hierarchical networks
    • H04W84/06Airborne or Satellite Networks

Abstract

A method for wirelessly communicating data between a plurality of avionics units on an aircraft and a data communication apparatus. The method includes wirelessly communicating download data for one avionics unit from the data communication apparatus from an aircraft data services link in the aircraft; electronically switching a communication path from the aircraft data services link to the avionics unit responsive to the download data; and electronically communicating the download data from the data communication apparatus to the avionics unit via the electronically switched communication path.

Description

    CROSS-REFERENCE TO RELATED APPLICATIONS
  • [0001]
    This application claims the benefit of U.S. Provisional application Ser. No. 60/268,085, filed Feb. 13, 2001, which is hereby incorporated by reference in its entirety. This application is also related to a commonly-assigned U.S. Patent Application of the same inventors entitled “METHOD AND APPARATUS FOR REMOTE INITIATION OF ARINC 615 DOWNLOADS”, Attorney Docket No. 7784-000338, filed on even date herewith, which is also incorporated by reference in its entirety.
  • FIELD OF THE INVENTION
  • [0002]
    The present invention relates to communications systems, and more particularly to methods and apparatus to facilitate loading and acquisition of data relating to aircraft loadable computers
  • BACKGROUND OF THE INVENTION
  • [0003]
    Digital computers on recent airplane models require frequent software updates. Flight management computers (FMCS) were among the first of these computers to have periodic updates performed. Originally, these updates were performed according to a tape loading standard (ARINC 603) that required the use of a portable device having one ARINC 429 output and two inputs. The loading was performed by attaching a cable and a portable tape loader to a 32-pin data loader connector located in the cockpit of the airplane. The location of this connector was chosen in different model airplanes to avoid having a mechanic crawl around an electrical equipment (EE) bay each time he was required to perform a software update. Nevertheless, it was soon recognized that portable tape loaders were slow, large and cumbersome. Thus, a new data loading standard, ARINC 615-1, was developed to utilize standard 3 ½″ floppy disks.
  • [0004]
    To accommodate new ARINC 615-1 loaders, the 32-pin data loader connector was replaced with a new 53-pin connector. In addition, some airlines preferred that loaders be configured for permanent mounting on primary long haul aircraft. As a result, the ARINC 615 specification was upgraded to accommodate additional busses in an attempt to anticipate a maximum number of loadable units that would require an interface with an ARINC 615 loader. Today, as many as 24 loadable Line Replaceable Units (LRUS) may be found on a single aircraft. However, only eight LRUs can be accommodated by the ARINC 615-3 specification.
  • [0005]
    One solution to the increasing number of LRUs on an aircraft has been to provide a Portable Data Loader (PDL) connector with a multiple position rotary switch. In some cases, approximately 200 wires populate four circular connectors located on the data loader switch installed on a maintenance panel.
  • [0006]
    Data communication between aircraft and ground began using existing HF and VHF radios to transmit character data stored in a few avionics line replaceable units (LRUs). The routing of information such as central maintenance computer and aircraft condition monitoring system reports in one known data communication system is under control of a management unit (MU) based on ARINC 724 specifications. The interfaces through which data has been routed from aircraft systems are traditional analog discrete and ARINC 429 data bus interfaces.
  • [0007]
    As the complexity of aircraft communication and reporting systems (ACARS) have increased, production aircraft have been provisioned with more advanced versions of such systems based on ARINC 758 specifications. One such communication management unit (CMU) is capable of handling protocol layers beyond those specified by ARINC 724B. One known CMU is also intended to accommodate interfaces to Ethernet-based systems, adding an additional, non-traditional physical layer. Digital link radios currently in development would further improve transmission between ground stations and aircraft. However, bandwidth for this technology still lags that provided by broadband satellite data communications.
  • [0008]
    ARINC 758 CMU functionality manages the routing of data for aircraft avionics systems over data link radios and satellite communication systems (SATCOM), with expandability to Ethernet-compatible systems. Sources and end users for communication with a ground station include satellite data units (SDUs), ACMS, central maintenance computers (CMCs), and optional cabin terminals via HF, VHF, SATCOM, and new data link radios. Aircraft information to the CMU comes from many avionics sources, such as display systems, flight management computers (FMCs), DFDAU digital discretes, ACMS, DFDAU ARINC 753 data, out/off/on/in (OOOI) discretes and transponders. Two-way communication is also established between multifunction control and display units (MCDUs), printers, data loaders, and aircraft programmable modules (APMs). CMUs are also capable of driving up to two sets of alert output discretes.
  • [0009]
    The aircraft industry is currently developing ARINC 763 Network Server Systems (NSS), which will have management capability for routing information over IEEE 802.11 transceivers utilizing wireless spread spectrum technology as well as Ethernet interface capability. The primary avionics data sources that ARINC 763 systems require are aircraft parametric information and 2-way ARINC 429 communication directly between avionics LRUs and a server interface unit (SIU).
  • [0010]
    As currently envisioned, ARINC 763 NSS will acquire parametric data and status via an ARINC 573/717 serial output of a digital flight data acquisition unit (DFDAU). To update software in avionics LRUs, the SIU is wired upstream from a rotary switch, between the switch and an existing portable data loader connector or an installed airborne data loader. However, one problem with designs of this type is that only raw parametric data out of the DFDAU is available. Processed reports, based on re-configurable capture criteria in ACMS, e.g., operator selectable channels of smart access recorder (SAR) data, re-programmable ACMS triggered reports, in addition to raw data intended for quick access recorders (QAR), are only available via an ARINC 615-3 data loader interface to the ACMS, and can be retrieved on-ground via disk download, or via ACARS as a defined trigger-event occurs.
  • [0011]
    A primary goal of aircraft manufacturers is to minimize changes to aircraft production processes while at the same time offering increased functional capability and ease of use in new product offerings. When numerous new wiring, LRUs and supporting components are added to production aircraft, aircraft manufacturers incur large, non-recurring costs. To avoid drastic changes that would incur these large costs, ARINC 763 NSSs are being designed with a limited subset of traditional aircraft interfaces. For example, one known ARINC 763 NSS is being designed to tie into two primary interfaces. The first of these two interfaces is an ARINC 573/717 DFDAU serial output bus to an existing QAR interface or parallel ARINC 573/717 path. The second is an existing data loader interface. NSS designers thus minimize usage of aircraft information from different aircraft sources and add a new communication medium to the aircraft information routing scheme, namely, wireless IEEE 802.11. Thus, some data movement issues on the aircraft side remain and some existing features, available in other known avionics LRUs, are not fully utilized.
  • [0012]
    Also, ARINC 758 and ARINC 763 systems have different philosophies regarding routing of aircraft information. ARINC 753 systems are connected to many existing aircraft interfaces with air/ground and limited ground/ground communication via existing radio and satellite technology. On the other hand, ARINC 763 systems are being designed for connection to a very small number of aircraft interfaces with ground to ground and limited air to ground communication (depending upon the distance to an access point) using wireless spread spectrum IEEE 802.11 communication technology. Known systems do not provide integration of these routing functions.
  • [0013]
    Present maintenance practices for downloading aircraft data into Avionics line replaceable units (LRUs) include using a portable or PC-based ARINC 615-3 data loader to download part number controlled databases, operational program configuration (OPC) files, and operational program software (OPS) that is ordinarily transferred using 3 ¼″ floppy disks. A permanently mounted airborne data loader (or a bulk loader in a shop environment) can also be used to load aircraft LRUs.
  • [0014]
    Software loadable LRUs in at least one aircraft line can be downloaded with controlled information stored on floppy disks. The loadable data conforms to ARINC 615 data formatting standards by including a CONFIG.LDR header file, embedded load cyclic redundancy checks (CRCs), system address labels (SALs), and a data bus sequence, and conforms to other file structure requirements. Avionics systems currently installed in this aircraft line provide two-way communication using standard ARINC 615-3 protocol, and this protocol is used on all LRUs that require periodic software upgrades. Wiring to accommodate LRUs that use the ARINC 615-3 protocol are routed to an existing multi-deck rotary switch. In a typical Boeing 747-400, for example, up to 23 LRUs utilize this upload function. A human operator uses the rotary switch to provide connectivity between avionics units to an airborne data loader or to a connector of a portable data loader. The wiring to the switch passes from an electronics equipment (EE) bay to a centralized flight deck location.
  • [0015]
    Because of the need for manual intervention to operate switches to provide connectivity between avionics units, providing automatic uploads of avionics data from aircraft to ground stations via wireless communication links would require extensive rewiring of existing aircraft. Remotely-initiated download of data from ground stations to aircraft would also require extensive rewiring.
  • SUMMARY OF THE INVENTION
  • [0016]
    One configuration of the present invention therefore provides a method for wirelessly communicating data between a plurality of avionics units on an aircraft and a data communication apparatus. The method includes wirelessly communicating download data for one avionics unit from the data communication apparatus from an aircraft data services link in the aircraft; electronically switching a communication path from the aircraft data services link to the avionics unit responsive to the download data; and electronically communicating the download data from the data communication apparatus to the avionics unit via the electronically switched communication path.
  • [0017]
    In another configuration, the present invention provides a method for wirelessly communicating data between a plurality of avionics units on an aircraft and a data communication apparatus. The method includes electronically switching a communication path from one the avionics unit to an aircraft data services link in the aircraft; electronically communicating data from the avionics unit to the aircraft data services link via the electronically switched communication path; and wirelessly communicating the data from the aircraft data services link to the data communication apparatus.
  • [0018]
    Yet another configuration of the present invention provides a method for wirelessly communicating data between a plurality of avionics units on an aircraft and a data communication apparatus. The method includes electronically switching a communication path from one the avionics unit to an aircraft data services link in the aircraft; electronically communicating data from the avionics unit to the aircraft data services link via the electronically switched communication path; and wirelessly communicating the data from the aircraft data services link to the data communication apparatus.
  • [0019]
    In still another configuration, the present invention provides an apparatus for wirelessly communicating data between a plurality of avionics units on an aircraft and a data communication apparatus external to the aircraft. The apparatus includes, onboard an aircraft: an aircraft data services link having a processor, means for wirelessly transmitting and receiving data to and from a data communication apparatus external to the aircraft, and an electronic switch; and a plurality of avionics units coupled to the remotely controllable switch; wherein the processor is responsive to data received from the data communication apparatus via the means for wireless transmitting and receiving to control the electronic switch to selectively couple the avionics units to the aircraft data services link to provide data communication between a selectively coupled avionics unit and the data communication apparatus via the aircraft data services link.
  • [0020]
    In yet another configuration, the present invention provides an apparatus for wirelessly communicating data between a plurality of avionics units on an aircraft and a data communication apparatus external to the aircraft. The apparatus includes, onboard an aircraft: an aircraft data services link having a processor and means for wirelessly transmitting to a data communication apparatus external to the aircraft and a plurality of avionics units coupled to the remotely controllable switch, wherein the processor is responsive to data received from the data communication apparatus via the means for wireless transmitting and receiving to control the electronic switch to selectively couple the avionics units to the aircraft data services link to provide data communication between a selectively coupled avionics unit and the data communication apparatus via the aircraft data services link.
  • [0021]
    Configurations of the present invention provide automatic uploading and/or downloading of data from and/or to ground stations using a wireless communication link, without requiring extensive rewiring or redesign of existing aircraft.
  • [0022]
    Further areas of applicability of the present invention will become apparent from the detailed description provided hereinafter. It should be understood that the detailed description and specific examples, while indicating the preferred embodiment of the invention, are intended for purposes of illustration only and are not intended to limit the scope of the invention.
  • BRIEF DESCRIPTION OF THE DRAWINGS
  • [0023]
    The present invention will become more fully understood from the detailed description and the accompanying drawings, wherein:
  • [0024]
    [0024]FIG. 1 is a block diagram of one configuration of an aircraft avionics system of the present invention.
  • [0025]
    [0025]FIG. 2 is block diagram of a configuration of the aircraft data services link (ADSL) shown FIG. 1.
  • [0026]
    [0026]FIG. 3 is a block diagram of one configuration of a hub or switch suitable for use in the aircraft data services link (ADSL) shown in FIG. 2.
  • DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS
  • [0027]
    The following description of the preferred embodiment(s) is merely exemplary in nature and is in no way intended to limit the invention, its application, or uses.
  • [0028]
    In one configuration of the present invention and referring to FIG. 1, an aircraft avionics system 10 on an aircraft supports communications between the aircraft and a data communication apparatus 12. This communication is provided via a wireless data link 14. A non-exhaustive list of suitable wireless data links include VHF radio links, HF radio links, satellite communication links (SATCOM), and wireless spread spectrum links such as IEEE 802.11. Suitable devices for data communication apparatus 12 include, but are not limited to, airport ground service terminals, wireless hand-held devices such as intranet-enabled cell-phones, pilot access terminals, electronic flight bags (EFBs), and so forth. Depending upon the range of wireless data link 14, data communication apparatus 12 can be external to and a significant distance from the aircraft on which avionics system 10 is installed. In at least one embodiment of the present invention, avionics system 10 is configured to communicate with more than one data communication apparatus 12, although not necessarily with more than one such apparatus 12 at one time. For example, communication with airport ground service terminals can be provided as well as communication with hand-held devices for maintenance.
  • [0029]
    Aircraft avionics system 10 further comprises a plurality of avionics units. In one configuration, these avionics units include an aircraft communication and reporting system (ACARS) 16, a multifunction control display unit (MCDU) 18, an aircraft condition monitoring system (ACMS) 20, and a digital flight data acquisition unit (DFDAU) 22. In one configuration, ACMS 20 and DFDAU 22 comprise a single unit that provides both ACMS and DFDAU functions. In addition, a plurality of additional avionics LRUs (hereinafter avionics units) 24 are provided. These units 24 are collectively represented in FIG. 1 as aircraft systems, communications management units (CMUs), discretes, ARINC 429 systems, and ARINC 573/717 systems. Routing of data to and from a ground-based data communication apparatus 12 to and from avionics units such as 16, 18, 20, 22, and 24 is provided by an aircraft data services link (ADSL) 26 in the aircraft. For example, data transferred by ADSL 26 to and/or from data communication apparatus 12 includes, in one embodiment, software uploads and downloads, flight performance data, and applications for use by flight crew, cabin crew, maintenance crew, airport ground services and airline operations.
  • [0030]
    In one configuration and referring to FIG. 2, ADSL 26 comprises one or more means 32, 36 for wirelessly transmitting and receiving data to and from one or more data communication apparatus 12 (not shown in FIG. 2). For example, an IEEE 802.11 transceiver 32 is coupled to an antenna 34 on the outside of the aircraft to provide communication between the aircraft and a data communication apparatus 12 on the ground. An additional IEEE 802.11 transceiver 36 is provided in one configuration with an antenna 38 inside the aircraft to provide access for portable data communication apparatus onboard the aircraft, such as those used by maintenance personnel. In one configuration not shown in FIG. 2, the spread spectrum transmitter and receiver are separate components. In another configuration, transceiver 32 is any variety of IEEE 802.11 transceiver or separate transmitter and receiver, such as a separate IEEE 802.11a transmitter and receiver. In yet another configuration, transmitting and receiving means 32 is an amplitude modulation receiver and transmitter, or an amplitude modulation transceiver. (As used herein, IEEE 802.11 includes variations thereof, such as IEEE 802.11b).
  • [0031]
    Wireless transmitting and receiving means 32 is communicatively coupled to a network server unit (NSU) 41 that comprises at least one CPU or processor 40 and a memory 42. Additional wireless transmitting and receiving means 36, if present, are also coupled to NSU 41. In one configuration, memory 42 includes instructions to operate CPU 40. Include in these instructions in one configuration are instructions to maintain a database containing version identifiers of software stored in software-loadable avionics units (not shown in FIG. 2). In one configuration, the operative coupling of NSU 41 to avionics units comprises “direct coupling” to one or more externally accessible busses 44, or indirect coupling 54 via a system interface unit/firewall (hereinafter, SIU) 46. SIU 46 sends and receives data to and from NSU 41 in one configuration via an Ethernet connection 56. It will be understood that the “direct coupling” to busses 44 may include timing and level interface circuitry, as required. This circuitry is not shown in FIG. 2. However, the design of such circuitry is considered to be within the capability of one of ordinary skill in the art.
  • [0032]
    ADSL 26 further comprises a remotely controllable switch 52, sometimes also referred to as a “hub.” Switch 52 sends and receives data to and from NSU 41 either directly 50, or in another configuration, via a bus or other data connection 48 to SIU 46. Switch 52 is coupled to a plurality of avionics units, represented collectively in FIG. 1 as 24. For example, switch 52 is coupled to a plurality of software-loadable ARINC 615 or 615A units. Such units have, in the past, been loaded utilizing a manually-switched connector in an avionics bay of an aircraft, because the ARINC 429 (or A429) standard does not allow more than one such unit to share a single bus. The use of a remotely controllable switch 52 permits communication between a data communication apparatus 12 and a selectively coupled avionics unit out of a plurality of such units using A429 busses (via antenna 34 or 38, and NSU 41) without shorting of A429 busses from different avionics units.
  • [0033]
    In one configuration, switch 52 is remotely controlled by NSU 41 either directly 50 or via bus or data connection 48. When data is downloaded for a selected avionics unit from a ground-based data communication apparatus 12, NSU 41 identifies the intended destination avionics unit. For example, instructions stored in memory 42 instruct NSU 41 processor 40 to buffer downloaded ARINC 615 or 615A compliant data in memory 42 and to identify the intended destination avionics source unit from information contained in the standard format of the data. Processor 40 then electronically switches hub or switch 52 (for example, by a signal sent via data connection 48 or 50 and recognized by hub or switch 52) to provide a communication path from ADSL 26 to the proper avionics unit for downloading the buffered data via the communication path to the proper avionics unit. Thus, processor 40 is responsive to data received from data communications apparatus 12 via wireless transmitting and receiving means 32 to selectively couple avionics units to ADSL 26 to provide communication between a selectively coupled avionics unit and data communication apparatus 12 via ADSL 26.
  • [0034]
    In addition, processor 40 updates its database to reflect the updated software version in that avionics unit. In configurations in which the selected avionics unit is able to report fault information pertaining to the uploaded data, this fault data is communicated back to ADSL 26 over the electronically switched communication path and wirelessly communicated via ADSL 26 back to the data communication apparatus 12 that transmitted the update. Also in one configuration, fault information is incorporated into the database stored in memory 42.
  • [0035]
    Thus, in one configuration of the present invention, a communication path such as an ARINC 429 bus is switched to provide communication continuity between an avionics unit (such as one of the units indicated collectively at 24) and ADSL 26. Data is communicated electronically from the avionics unit to ADSL 26 via this electronically switched communication path, and then this data is wirelessly communicated 14 from ADSL 26 to data communication apparatus 12. Remotely controllable switch 52 in one configuration is coupled to at least two avionics units via ARINC 429 (A429) busses, and selects one of the avionics units at a time for coupling to processor 40.
  • [0036]
    Also in one configuration of the present invention, aircraft performance data is transmitted to a ground-based data communication apparatus 12 by aircraft avionics system 10. Referring again to FIGS. 1 and 2, aircraft performance data is gathered by ACMS 20 from avionics unit sources. In one configuration, the avionics unit sources include at least one of an ACARS 16, an MCDU 18 or an DFDAU 22, or combinations thereof. This performance data is communicated from ACMS 20 to ADSL 26 electronically via communication link 64, and wirelessly 14 from ADSL 26 to data communication apparatus 12. NSU 41 processor 40 of ADSL 26 is responsive to data transferred to it by ACMS 20 and, in one configuration, is configured to schedule wireless transmission 14 of the transferred data from ACMS 20 to data communication apparatus 12. For example, a program in memory 42 executed by NSU 41 processor 40 wirelessly transmits 14 this data at scheduled times during a flight, or upon landing.
  • [0037]
    In one configuration, data carried over wireless link 14 includes configuration updates to communication management units (CMUS) 24 downloaded from a ground station to memory 42 in ADSL 26. For example, one type of update is provided as an operational control configuration (OPC) software loadable ‘controlled’ part. Configuration management is provided by a database in the memory of ADSL 26 and at an originating ground network node (i.e., data communications apparatus 12) and are synchronized, coordinated and tracked on both the aircraft and at the ground. Real-time NSU 41 processor 40 handles data acquisition and communication between aircraft interfaces and server/router.
  • [0038]
    Databases and datasets for ADSL 26 functionality are treated as configuration updates in similar form and part number control as CMU OPC updates. Examples of such databases and datasets include navigation databases, weather maps, synthetic vision profile maps and runway maps to assist in surface awareness and/or guidance.
  • [0039]
    Operational program software (OPS) updates by ADSL 26 are handled under strict configuration control guidelines in one configuration of the present invention. Acceptance by ADSL 26 of ground station data OPS downloads via data communication apparatus 12 and storage in NSU 41 memory 42 are conditioned upon passing a number of predetermined tests, such as compatibility checks, revision history checks, and/or synchronization with a version control system at an authenticated source on the ground. In one configuration, an aircraft configuration management application in ADSL 26 is configured to perform automatic OPS downloads when required by hardware replacement, and to flag any unresolved aircraft/software compatibility issues.
  • [0040]
    In one configuration, some types of information from the avionics units are stored and time-tagged for later retrieval and transfer to a network client such as a pilot access terminal, an electronic flight bag (EFB), or ground network system (not shown in the figures). Real-time parametric data is collected from the avionics systems, including (but not limited solely to) data collected from an ARINC 573/717 output of DFDAU 22. This data is stored in a variable recording buffer (shown as digital storage 60 in FIG. 1) to attach trigger events to the function of ACARS 16. In one configuration, the window size of buffer 60 is reprogrammable via an OPC update.
  • [0041]
    In one configuration, ADSL 26 includes an avionics data acquisition function using existing ARINC 615-3 handshaking protocols. Although these protocols are used today to upload software to LRUs, physical connections and software in avionics LRUs that support an upload of fault data already exist. ADSL 26 is also used, in one configuration, to collect avionics LRU configuration information through an avionics gateway and to identify and store in memory the current software part numbers installed on an aircraft. A predefined format is used for each LRU to transmit its software part number to the ADSL 26.
  • [0042]
    In one configuration, there are six major communication paths for transfer of data.
  • [0043]
    1. Aircraft to ADSL.
  • [0044]
    Aircraft to ADSL 26 interfaces 62, 64 communicate upload fault information and configuration information for all connected ARINC 615-3 loadable systems. In one configuration, this information is also provided from ARINC 615A (Ethernet) loadable systems. (Hereinafter, both in the description and in the claims, reference to an ARINC 615 system is intended to encompass all ARINC 615 systems, irrespective of suffix, unless otherwise noted.) Examples of such systems are MCDUs and cabin terminal interfaces. This data is provided, in one configuration, via ARINC 429. In addition, data is provided from CMU interfaces via ARINC 429, discretes, and ARINC 573/717 serial outputs.
  • [0045]
    2. ADSL to aircraft.
  • [0046]
    Bidirectional interface 62, 64 provides a dataload interface for all ARINC 615 upload software to all connected systems via ARINC 429, including, in one configuration, ARINC 615A (Ethernet). Examples of such systems are MCDU 18 and cabin terminal interfaces. This data is provided, in one configuration, via ARINC 429. In addition, data is provided from CMU interfaces via ARINC 429, discretes.
  • [0047]
    3. ADSL to clients.
  • [0048]
    Interface 62. 64 provides fault information and software configuration information from an ARINC 615 download application for use by client-resident applications using IEEE 802.11 protocol. Examples of such systems are enhanced MCDU 18, cabin terminal functionality, software updates to be used by clients, i.e., flight crew, cabin crew, maintenance, airport ground services and airline operations. Real time data captured by ADSL 26 and outputs of “auto-report generation” applications on ADSL 26 are available for display using client resident applications.
  • [0049]
    4. Client to ADSL.
  • [0050]
    Outputs of reports generated by resident applications on client devices, such as pilot access terminals (PATs), electronic flight bag (EFB), etc. (not shown in the figures) are communicated via IEEE 802.11. Clients can emulate MCDU 18, cabin terminal interface for communications. Outputs of applications in client devices, such as pilot access terminals (PATs), electronic flight bag (EFB), etc., via IEEE 802.11.
  • [0051]
    5. ADSL to ground
  • [0052]
    Stored data, reports transmitted automatically to or requested from a ground station via a communication link 14 (for example, HF, VHF, SATCOM, broadband, or IEEE 802.11).
  • [0053]
    6. Ground to ADSL
  • [0054]
    This data comprises software updates for avionics, configuration management synchronization information, selective fault report and configuration data requests. (Databases and configuration updates are considered as software updates for purposes of this description.)
  • [0055]
    ADSL 26 interfaces with the aircraft via the SIU 46 and via a communications router/server 44, 54, 70. SIU 46 provides an upload path for software and updates and a download path for avionics LRU stored information. The avionics LRU stored information can include, but is not limited to, avionics LRU fault information and recorded parametric data and triggered reports.
  • [0056]
    The communications router/server provides end-to-end connection from the aircraft/ground network client to any other aircraft/ground network client in a user-defined infrastructure. For example connection is provided to the flight crew using pilot access terminals or EFBs, to the cabin crew using cabin terminals or EFBs, to the maintenance crew using EFBs, PATs or any of a variety of wireless hand-held devices such as intranet web-connected cell phones, etc., to airport ground services via ground-based terminals and wireless hand-held devices, and to airline operations via ground-based terminals. Connectivity media include ARINC 429, Ethernet, HF radio, VHF radio, SATCOM narrowband, digital broadband, and IEEE 802.11 wireless protocol, as well as combinations thereof.
  • [0057]
    SIU 46 in one configuration is coupled 48 to a remotely controllable electronic switch 50 that is controlled via an Ethernet connection 56 or ARINC 429 interface, depending upon the location of a data load application. The switch is controlled in one configuration using directed commands from an “authenticated” ground station (i.e., a trusted ground-based data communication apparatus 12) or another valid network client via a terminal area wireless local area network (LAN) operating according to a compatible standard. In one configuration, IEEE 802.11 is utilized for the compatible standard. In another configuration in which an Ethernet link is used, a protocol is used between SIU 46 and NSU 41 that permits a remote station 12 of a network client to establish a direct connection to an avionics LRU such as one of avionics units 24 for uploading or downloading an ARINC 615 data. The request for this upload may be initiated using a data communication apparatus 12 such as a pilot access terminal (PAT), electronic flight bag (EFB), or a ground network client. Safety checks, such as those used for data loading by traditional 2-way ARINC communication, are used by avionics LRUs 24. These checks include embedded (or load) cyclic redundancy checks (CRCs) that are independently recalculated by a target avionics LRU 24 upon receipt, use of ARINC assigned system address labels (SAL), hardware/software compatibility checks in the LRUs, and other checks.
  • [0058]
    Some existing aircraft, such as the Boeing 747-400, have a permanently installed airborne data loader that is always powered up. In existing aircraft, relays and switches have been installed to isolate multiple transmitters to avoid connecting two transmitters to a single receiver at the same time. Therefore, in one configuration, a switch such as that described in U.S. Provisional Application No. 60/268,085, filed Feb. 13, 2001 (which is hereby incorporated by reference in its entirety) is used as switch 52. Referring to FIGS. 2 and 3, two or more ARINC 429 inputs 70 are directly connected to a single receiver or transceiver 72 at one time by implementing a software-controlled switch 74 at remotely controlled hub or switch 52. This implementation eliminates the need for external relays, procedural workarounds and major aircraft production revisions. ARINC 429 transceiver 72 in the embodiment of switch 52 represented in FIG. 3 actually includes two receivers as well as a transmitter, with one of the two receivers hard-wired to a single, unswitched ARINC 429 input.
  • [0059]
    In one configuration of the present invention, aircraft data services link (ADSL) 26 performs a remotely controllable data download function utilizing the data loading capabilities of existing aircraft avionics LRUs, 24 including on-board servers. The download of data conforming to the ARINC 615 standard is remotely and/or automatically initiated. The transfer of download data from a network operations center (NOC) via a data communications apparatus 12 or aircraft server to an aircraft avionics unit 24 is similar to downloading of operational software using an ARINC 615 data loader, except that, rather than originating at an ARINC 615 data loader connected by cables to the aircraft, data is downloaded from an on-board server, from one or more network operations centers (NOCs) via a data communications apparatus 12 and/or from a data content service provider. Several different methods are provided in one configuration to initiate uploads. These methods include:
  • [0060]
    (1) Automatic synchronization downloading and associated auto-delete task for aircraft network clients, such as wireless handheld devices, fixed or quick disconnect flight deck mounted displays, WAP or PDA devices on a flightline, the on-board server, and avionics LRUs. When initiated by a NOC, the onboard server synchronizes with the NOC. Aircraft network clients synchronize with the on-board server.
  • [0061]
    (2) Automatic configuration management uploads, i.e., aircraft version change management, for loadable entities on the aircraft that are connected to the aircraft network. When software updates are complete, the revised software configuration information is transmitted back automatically to the enabling NOC to alert a quality assurance representative that the download has successfully completed.
  • [0062]
    (3) Responses to operator-initiated requests from authenticated clients via any of the communication paths connected to ADSL 12. Examples of such requests include access to the data from avionics LRUs without manual operator intervention on the aircraft, synchronization tasks with associated ground network systems, backup and recovery initiation, and other network requests. Network clients include, for example, one or more authorized users communicating using any of ADSL 12 communication links, cabin or flight deck mounted terminals, portable digital assistants (PDAs), wireless electronic flight bags (EFB), or one or more ground terminals.
  • [0063]
    A spread spectrum link 14 is used in one configuration of the present invention to manually initiate an ARINC 615 download. An ARINC 615 CONFIG.LDR file intended for a target LRU is configured for a download. This header file includes an appropriate system address label (SAL) for the target LRU, in addition to load CRCs, etc. A connection to a specific computer occurs prior to activating a data download when multiple computers having the same SAL are installed. A download task/configuration manager informs the operator that a connection to the target LRU has been established. In one configuration, this notification is performed in conjunction with a data loader application resident on a ground-based system, an authorized network client, or the avionics gateway. A communications protocol is utilized between the avionics gateway and an on-board server to tag the most recent configuration changes for transmission back to the NOC.
  • [0064]
    ARINC 615-3 and ARINC 615A data loader data for software, configuration, or database updates are transferred, in one configuration of the present invention, by initiating software downloads from the ground to any software loadable aircraft avionics unit (i.e., LRU) 24, for example, operational program software (OPS), operational program configuration (OPC), and databases for ARINC 615 LRUs. Systems such as flight management computers (FMCs), flight control computers (FCCs), digital flight data acquisition units (DFDAUs) 22, aircraft conditioning monitor systems (ACMSs) 22, SATCOMs, onboard servers and all other ARINC 615-3 or ARINC 615A Ethernet loadable systems can be loaded from the ground using appropriate ARINC 615-3 or ARINC 615A download commands. An aircraft data services link ADSL 26 system is resident on the aircraft to direct software download requests to any loadable system and to transmit data via existing ARINC 429 and Ethernet interfaces to software loadable systems. The ADSL includes one or more processors 40, a memory 42, a remotely controllable SIU 46, and a hub or switch 52 coupled to a transceiver 32 (such as an IEEE 802.11 transceiver) for transmission of data to an aircraft. An existing ARINC 429 data loader interface, centralized and accessible in the aircraft's flight deck compartment, in conjunction with the ADSL 26, allows direct control and transfer of software updates to aircraft subsystems within range of a ground station access point having a wireless data communication apparatus 12.
  • [0065]
    Configurations of the present invention are thus capable of providing routing and configuration management for each loadable system and terminal device connected to an aircraft local area network (LAN), both on and off an aircraft.
  • [0066]
    One suitable SIU 46 and switch 52, in one configuration, provides automated electronic switching and control for data downloading of software in the form of operational programs, operational configuration of databases, collection of software configuration information from systems such as avionics subsystems and uploading data between those subsystems and ARINC 615-3 or 615A data load applications. The data load applications may be resident in existing ARINC 615 airborne, portable, or PC-based data loaders or an optional ARINC 763 type on-aircraft network server system. In one configuration, SIU 46 and switch 52 use a real-time LINUX® based platform that is also capable of hosting any data load application. The switch interface unit can be manually controlled and used as a stand-alone replacement for existing rotary switches, or remotely controlled and integrated into an ARINC 763 type network server system.
  • [0067]
    In one configuration, SIU 46 and switch 52 are configured as a single physical unit as a stand alone, data loader rotary switch replacement. Combination SIU 46 and switch 52 in this configuration comprise a programmable electronic switch that displays and allows selection of loadable systems on an aircraft for the purpose of initiating a software data load. The input and output of the combination unit is programmable, primarily to activate interfaces with loadable LRUs connected to the combination unit, which may vary between different airplane models and airlines. In addition, in one configuration, the combination unit provides the functions of a configuration data tool and repository, by containing a collection of loadable LRUs software part numbers and by providing a data display device. The combination unit also functions as a monitor of incoming and outgoing ARINC 429 traffic, with appropriate connections initiated between communicating end-user systems and a data loader application. The data loader application may, for example, be resident in an existing ARINC 615-3 airborne loader, an ARINC 615A Ethernet loader, a portable data loader (when such is connected to a flight deck connector) or the switch interface unit itself, which is capable of hosting the data loader application in its real-time LINUX® operating system. (LINUX is a registered trademark of Linus Torvalds.) In one configuration, ARINC 615-3 data load applications are in the combination unit, because the connection with the airborne server is Ethernet only, while current airplane communication interfaces to the invention are ARINC 429. A protocol packing and unpacking scheme is not required if ARINC 615-3 is resident in one configuration of the combination unit.
  • [0068]
    In a second configuration, the combination unit is utilized in a Network Server System (NSS) that includes an airborne server. In this configuration, the combination unit can be remotely controlled through a provisional Ethernet connection that is activated only by directed commands from the airborne server and/or by directed commands from a ground station via IEEE 802.11 spread spectrum wireless connection. The combination unit may be queried for stored LRU configuration information, for example, software (S/W) part numbers from any or all of the avionics system connected to the combination unit. The combination unit may also, automatically or on request, perform compatibility checks between expected SNV part numbers stored in a resident database or external server connected to the combination unit, and actual part numbers collected by the combination unit.
  • [0069]
    The combination unit bridges a gap between interfacing with existing avionics systems for data uploading and data acquisition without drastically modifying the manner in which airplanes are currently built. The functionality of the combination unit is easily adaptable so that it can become an integral component on future on-board network systems. Embodiments of the combination unit provide can be used efficiently as a directed data query and download engine to an ARINC 763-type network server system. At least one embodiment allows communication with a plurality of computers, which may include a Digital Flight Data Acquisition Unit (DFDAU) and a Flight Management Computer (FMC), without manual intervention via a selection of a rotary switch.
  • [0070]
    In one configuration of the present invention, upon touchdown of an aircraft, an active query of pre-processed Aircraft Conditioning Monitoring System (ACMS), Smart Access Recorder (SAR), Quick Access Recorder (QAR), and Data Acquisition Recorder (DAR) historical data from a concluded flight obtained from avionics units 24 can be initiated using remotely selectable ARINC 429 data loader interfaces connected to a remotely controlled switch 52. No accumulated data is lost. Active queries are prevented in this configuration due to avionics systems interlocks in the air
  • [0071]
    The combination unit functions as the aircraft system selector in a data load/configuration system. The combination unit is line replaceable, and has many advantages over existing rotary switches. The design of the combination unit meets and exceeds current data load interfacing requirements for avionics equipment.
  • [0072]
    Existing functionality includes acquisition of ARINC 615 data of flight operations quality assurance (FOQA) smart access recorder (SAR), quality assurance report (QAR) data and reports for aircraft communications and reporting system (ACARS) stored in ACMS 20. Functionality added in one configuration of the present invention includes uploading of stored fault information from any aircraft LRU 24 connected to ADSL 26. Common system requirements are imposed to achieve this added functionality. For example, fault message formats are specified for data upload of all connected systems for which ARINC 615 upload capability is added or newly utilized. The additional data acquisition feature, combined with storage and transmission of ARINC 615 data and the use of minor software updates to aircraft systems, allows a complete central maintenance function on non CMC-equipped airplanes such as Boeing 737s, 757s, and 767s, without associated production wiring changes.
  • [0073]
    In one configuration, ADSL 26 retrieves a smart access recorder (SAR) data stream of up to eight channels and triggered ACMS 20 reports in adition to a QAR data stream in ARINC 615 data format. Upload retrieval time is about 164 seconds for a 2 MB file acquired from digital flight data acquisition unit DFDAU 22 ARINC 573/717 serial bus output. A 2 MB file represents one flight's worth of flight operations quality assurance (FOQA) data, nominally defined as 2 hours for a flight. The uplink retrieval time is 164 seconds as a result of the data retrieval method used prior to 802.11b transfer. More specifically, the downlink retrieval time includes 160 seconds on ground plus 4 seconds for aircraft ground data transfer. A 40 MB file represents a transfer at the end of a day's worth of flights. The uplink retrieval time for this 40 MB file is 160 seconds, because 18 MB has already been acquired by the server application for previous flight legs. A 200 MB file represents a transfer at the end of two weeks of flights. (200 MB represents a capacity of PCMCIA cards used for FOQA storage devices such as QARs and ACMS.) The uplink retrieval time for this 200 MB file is 400 seconds, because 198 MB is acquired by the server application for previous flight legs.
  • [0074]
    It will thus be seen that configurations of the present invention reduce or eliminate the need for manual intervention to operate switches to provide connectivity between avionics units, and thus provide the capability to automatically upload avionics data from aircraft to ground stations via wireless communication links without requiring extensive rewiring and/or redesign of existing aircraft. The capability for remotely-initiated download of data from ground stations to aircraft is also provided without extensive rewiring and/or design.
  • [0075]
    The description of the invention is merely exemplary in nature and, thus, variations that do not depart from the gist of the invention are intended to be within the scope of the invention. Such variations are not to be regarded as a departure from the spirit and scope of the invention.

Claims (24)

    What is claimed is:
  1. 1. A method for wirelessly communicating data between a plurality of avionics units on an aircraft and a data communication apparatus, said method comprising:
    wirelessly communicating download data for one said avionics unit from the data communication apparatus from an aircraft data services link in the aircraft;
    electronically switching a communication path from said aircraft data services link to said avionics unit responsive to said download data; and
    electronically communicating said download data from said data communication apparatus to said avionics unit via said electronically switched communication path.
  2. 2. A method in accordance with claim 1 wherein said wirelessly communicating download data comprises wirelessly communicating said download data via a wireless spread spectrum link.
  3. 3. A method in accordance with claim 1 further comprising electronically communicating fault information pertaining to said download data from said avionics unit to said aircraft data services link via an electronically switched communication path, and wirelessly communicating said fault information from said aircraft data services link to said data communication apparatus.
  4. 4. A method in accordance with claim 1 further comprising electronically communicating aircraft performance data from an aircraft condition monitoring system on said aircraft to said aircraft data services link, and wirelessly transmitting said aircraft performance data from said aircraft data services link to said data communication apparatus.
  5. 5. A method in accordance with claim 4 further comprising said aircraft condition monitoring system obtaining said aircraft performance data via an electronic communication from at least one member of the group consisting of an aircraft communication and reporting system on said aircraft, a maintenance control display unit on said aircraft, and a digital flight data acquisition unit on the aircraft
  6. 6. A method in accordance with claim 1 wherein said electronically switched communication path comprises an ARINC 429 bus.
  7. 7. A method in accordance with claim 1 wherein said download data comprises an ARINC 615 or ARINC 615A compliant data.
  8. 8. A method in accordance with claim 1 wherein said download data comprises flight operations quality assurance data.
  9. 9. A method for wirelessly communicating data between a plurality of avionics units on an aircraft and a data communication apparatus, said method comprising:
    electronically switching a communication path from one said avionics unit to an aircraft data services link in the aircraft;
    electronically communicating data from said avionics unit to said aircraft data services link via said electronically switched communication path; and
    wirelessly communicating said data from said aircraft data services link to said data communication apparatus.
  10. 10. A method in accordance with claim 9 wherein said electronically switched communication path comprises an ARINC 429 bus.
  11. 11. A method in accordance with claim 9 further comprising electronically communicating aircraft performance data from at least one member of a group consisting of
    an aircraft condition monitoring system on said aircraft,
    a maintenance control display unit on said aircraft, and
    a digital flight data acquisition unit to said aircraft data services link, and wirelessly transmitting said aircraft performance data from said aircraft data services link to said data communication apparatus.
  12. 12. A method for wirelessly communicating data between a plurality of avionics units on an aircraft and a data communication apparatus, said method comprising:
    electronically switching a communication path from one said avionics unit to an aircraft data services link in the aircraft;
    electronically communicating data from said avionics unit to said aircraft data services link via said electronically switched communication path; and
    wirelessly communicating said data from said aircraft data services link to said data communication apparatus.
  13. 13. An apparatus for wirelessly communicating data between a plurality of avionics units on an aircraft and a data communication apparatus external to the aircraft, said apparatus comprising, onboard an aircraft:
    an aircraft data services link having a processor, means for wirelessly transmitting and receiving data to and from a data communication apparatus external to the aircraft, and an electronic switch;
    a plurality of avionics units coupled to said remotely controllable switch;
    wherein said processor is responsive to data received from the data communication apparatus via said means for wireless transmitting and receiving to control said electronic switch to selectively couple said avionics units to said aircraft data services link to provide data communication between a selectively coupled avionics unit and the data communication apparatus via said aircraft data services link.
  14. 14. An apparatus in accordance with claim 13 wherein said means for wireless transmitting and receiving comprises an IEEE 802.11 transceiver.
  15. 15. An apparatus in accordance with claim 13 wherein said means for wireless transmitting and receiving comprises a spread spectrum receiver and transmitter.
  16. 16. An apparatus in accordance with claim 13 wherein said means for wireless transmitting and receiving comprises an IEEE 802.11a receiver and transmitter.
  17. 17. An apparatus in accordance with claim 13 wherein said means for wireless transmitting and receiving comprises an amplitude modulation receiver and transmitter.
  18. 18. An apparatus in accordance with claim 13 further comprising an aircraft condition monitoring system on the aircraft, said aircraft condition monitoring system electronically coupled to said aircraft data services link, wherein said processor is responsive to data transferred from said aircraft condition monitoring system to said aircraft data services link and configured to schedule wireless transmission of said data transferred from said aircraft condition monitoring system to the data communication apparatus.
  19. 19. An apparatus in accordance with claim 18 further comprising at least one member of the group consisting of an aircraft communication and reporting system on the aircraft, a maintenance control display unit on said aircraft, and a digital flight data acquisition unit on the aircraft, and wherein said at least one member is operatively coupled to said aircraft condition monitoring system to communicate information to data communication apparatus wirelessly via said aircraft data services link.
  20. 20. An apparatus in accordance with claim 13 wherein at least two of said plurality of avionics units coupled to said remotely controllable switch are coupled to said remotely controllable switch via A429 busses.
  21. 21. An apparatus in accordance with claim 13 wherein said aircraft data services link is configured to communicate ARINC 615 compliant data to at least some of said avionics units.
  22. 22. An apparatus in accordance with claim 21 wherein said aircraft data services link includes a memory coupled to said processor, and said processor is configured to maintain a database in said memory containing version identifiers of software in said avionics units, and to update said database when data transmitted from said data communication apparatus is communicated to an avionics unit via said aircraft data services link.
  23. 23. An apparatus in accordance with claim 13 configured to wirelessly download flight quality assurance data.
  24. 24. An apparatus for wirelessly communicating data between a plurality of avionics units on an aircraft and a data communication apparatus external to the aircraft, said apparatus comprising, onboard an aircraft:
    an aircraft data services link having a processor and means for wirelessly transmitting to a data communication apparatus external to the aircraft;
    a plurality of avionics units coupled to said remotely controllable switch;
    wherein said processor is responsive to data received from the data communication apparatus via said means for wireless transmitting and receiving to control said electronic switch to selectively couple said avionics units to said aircraft data services link to provide data communication between a selectively coupled avionics unit and the data communication apparatus via said aircraft data services link.
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US10075032 Abandoned US20030069015A1 (en) 2001-02-13 2002-02-12 Method and apparatus for remote initiation of ARINC 615 downloads
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Cited By (99)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20030182404A1 (en) * 2002-03-25 2003-09-25 Jean-Francois Saint-Etienne Installation, gateway and process for downloading information between equipment onboard an aircraft and offboard loading means
EP1426870A2 (en) * 2002-12-02 2004-06-09 The Boeing Company Remote aircraft manufacturing, monitoring, maintenance and management system
US20040162067A1 (en) * 2002-08-20 2004-08-19 Arinc Inc. Security messenger system
US6801769B1 (en) 2003-03-12 2004-10-05 The Boeing Company Modular aircraft information network system and an associated method of packaging the same
US20040253945A1 (en) * 1999-03-04 2004-12-16 Janik Craig M. System for providing content, management, and interactivity for thin client devices
US20050026609A1 (en) * 2001-02-13 2005-02-03 Brinkley Roger R. Methods and apparatus for wireless upload and download of aircraft data
US20050039006A1 (en) * 2003-07-25 2005-02-17 Desi Stelling Method for controlling customer-implemented data updates
US20050047065A1 (en) * 2003-08-26 2005-03-03 The Boeing Company Expansion module and network for avionic devices
EP1517236A2 (en) * 2003-08-13 2005-03-23 Airbus Deutschland GmbH System and method for exchanging programs in aircraft computers
US20050086360A1 (en) * 2003-08-27 2005-04-21 Ascential Software Corporation Methods and systems for real time integration services
US6885921B1 (en) * 2002-05-09 2005-04-26 Grace H. Farmer Method and apparatus for managing aircraft maintenance records
US20050129239A1 (en) * 2002-11-21 2005-06-16 Farley Rodney J. Secure terminal data loader apparatus and method for a mobile platform
US20050149238A1 (en) * 2004-01-05 2005-07-07 Arinc Inc. System and method for monitoring and reporting aircraft quick access recorder data
US20050197848A1 (en) * 2004-03-08 2005-09-08 Chou Y. H. Airport customer support dispatch system and method for operation for the same
US20050220055A1 (en) * 1999-05-14 2005-10-06 Nelson Eric A Aircraft data communications services for users
US20050228558A1 (en) * 2004-04-12 2005-10-13 Patrick Valette Method and system for remotely communicating and interfacing with aircraft condition monitoring systems
US20050228559A1 (en) * 2004-04-12 2005-10-13 Laurent Bloch PCMCIA card for remotely communicating and interfacing with aircraft condition monitoring systems
US20050262191A1 (en) * 2003-08-27 2005-11-24 Ascential Software Corporation Service oriented architecture for a loading function in a data integration platform
US20050261820A1 (en) * 2004-05-21 2005-11-24 Feeney Mark E Method of monitoring gas turbine engine operation
US20050262192A1 (en) * 2003-08-27 2005-11-24 Ascential Software Corporation Service oriented architecture for a transformation function in a data integration platform
WO2005121722A1 (en) * 2004-06-04 2005-12-22 Texas Research International, Inc. Distributed mode system for real tme acoustic emission monitoring
US20050288831A1 (en) * 2004-06-23 2005-12-29 Lusardi Robert A User-configurable electronic flight bag
US20060041340A1 (en) * 2004-08-17 2006-02-23 Arinc Inc. Systems and methods for crew interaction and coordination using portable electronic data storage and display devices
US20060229103A1 (en) * 2005-04-08 2006-10-12 The Boeing Company Point-to-multipoint communications system and method
US20060229077A1 (en) * 2005-04-08 2006-10-12 The Boeing Company Soft handoff method and apparatus for mobile vehicles using directional antennas
US20060229772A1 (en) * 2005-04-08 2006-10-12 Honeywell International Inc. Systems and methods for avionics software delivery
US20060229070A1 (en) * 2005-04-08 2006-10-12 The Boeing Company Soft handoff method and apparatus for mobile vehicles using directional antennas
US20060252422A1 (en) * 2003-03-27 2006-11-09 Kauffman Donald C In-flight communications system
US20060262022A1 (en) * 2005-05-17 2006-11-23 Desargant Glen J Compact, mechanically scanned cassegrain antenna system and method
US20070010236A1 (en) * 2005-07-07 2007-01-11 David Allen Mobile platform distributed data load management system
US20070016344A1 (en) * 2005-07-15 2007-01-18 Arinc, Incorporated Systems and methods for voice communications and control using adapted portable data storage and display devices
US20070027589A1 (en) * 2001-02-13 2007-02-01 Brinkley Roger R Methods and apparatus for wirelss upload and download of aircraft data
US20070033277A1 (en) * 2005-08-08 2007-02-08 Yukawa Steven J Fault data management
US20070042727A1 (en) * 2005-08-16 2007-02-22 Arinc Inc. Systems and methods for voice and data communication
US20070042708A1 (en) * 2005-08-16 2007-02-22 Arinc Inc. Systems and methods for voice and data communication
US20070055416A1 (en) * 2005-07-13 2007-03-08 Allen David L Integrating portable electronic devices with electronic flight bag systems installed in aircraft
WO2007050164A1 (en) 2005-10-28 2007-05-03 The Boeing Company Remote aircraft maintenance in a networked environment
WO2007059333A2 (en) 2005-11-16 2007-05-24 The Boeing Company Integrated maintenance and materials service for fleet aircraft and system for determining pricing thereof
US20070124222A1 (en) * 2005-11-16 2007-05-31 Avery Robert L Integrated materials management for commercial aircraft fleets including access to real-time on-board systems information
US20070127460A1 (en) * 2005-12-02 2007-06-07 The Boeing Company Scalable On-Board Open Data Network Architecture
US20070130437A1 (en) * 2005-12-02 2007-06-07 Larson Craig A Methods and systems for managing computer system configuration data
US20070150124A1 (en) * 2005-12-22 2007-06-28 Patrick Wipplinger Methods and systems for displaying enroute moving maps
US20070183435A1 (en) * 2005-12-02 2007-08-09 Kettering Christopher B Methods and apparatus providing an airborne e-enabled architecture as a system of systems
US7257469B1 (en) * 2003-11-25 2007-08-14 Garmin International, Inc. Delivering data updates to an avionics device
US20070220109A1 (en) * 1998-09-09 2007-09-20 Nelson Eric A Method and Apparatus For Data Communication Utilizing The North American Terrestrial System
US20070243867A1 (en) * 2002-08-20 2007-10-18 Arinc Incorporated Acars messages over iridium
WO2006124277A3 (en) * 2005-05-17 2007-11-01 Universal Electronics Inc System and method for providing content, management, and interactivity for client devices
US20070264953A1 (en) * 2006-05-12 2007-11-15 Thiru Srinivasan Automated delivery of flight data to aircraft cockpit devices
US20080039076A1 (en) * 2004-09-16 2008-02-14 Harris Corporation System and method of transmitting data from an aircraft
US20080117858A1 (en) * 2006-11-21 2008-05-22 Honeywell International Inc. System and method for transmitting information using aircraft as transmission relays
US7386374B1 (en) * 2002-10-18 2008-06-10 Garmin International, Inc. Methods, data structures, and systems to configure avionic equipment with profile data
US20080154442A1 (en) * 2006-12-21 2008-06-26 Patrick Ralf Wipplinger Methods and systems for displaying electronic enroute maps
US20080162155A1 (en) * 2006-12-29 2008-07-03 Gregory John Small Methods and apparatus providing an e-enabled ground architecture
US20080235634A1 (en) * 2007-03-22 2008-09-25 Arinc Incorporated Electronic paper device for use by aircraft pilots and crew
US20080235626A1 (en) * 2007-03-22 2008-09-25 Arinc Incorporated Electronic paper device for use by aircraft and railway passengers
FR2914804A1 (en) * 2007-04-06 2008-10-10 Airbus Sas System of communication between a network of computers in an aircraft and a network of computers to the ground
FR2914803A1 (en) * 2007-04-06 2008-10-10 Airbus Sas Method and maintenance device in an aircraft
US20090037034A1 (en) * 2007-07-30 2009-02-05 Patrick Mattingly Vehicle performance monitoring system with multi-level caching
US20090041041A1 (en) * 2007-08-08 2009-02-12 Honeywell International Inc. Aircraft data link network routing
US20090040963A1 (en) * 2007-08-08 2009-02-12 Honeywell International Inc. Gatelink startup controlled by acars cmu
US20090077203A1 (en) * 1999-03-04 2009-03-19 Ez4Media, Inc. Clock with link to the internet
US20090082013A1 (en) * 2007-09-20 2009-03-26 Honeywell International Inc. System and method for wireless routing of data from an aircraft
US20090103473A1 (en) * 2007-10-19 2009-04-23 Honeywell International Inc. Method to establish and maintain an aircraft ad-hoc communication network
US20090103452A1 (en) * 2007-10-19 2009-04-23 Honeywell International Inc. Ad-hoc secure communication networking based on formation flight technology
US20090138518A1 (en) * 2007-11-27 2009-05-28 The Boeing Company Proxy Server for Distributing Aircraft Software Parts
US20090138873A1 (en) * 2007-11-27 2009-05-28 The Boeing Company Method and Apparatus for Loadable Aircraft Software Parts Distribution
US20090138872A1 (en) * 2007-11-27 2009-05-28 The Boeing Company Method and Apparatus for Processing Commands in an Aircraft Network
US20090138871A1 (en) * 2007-11-27 2009-05-28 The Boeing Company Onboard Electronic Distribution System
US20090138517A1 (en) * 2007-11-27 2009-05-28 The Boeing Company Alternate Parts Signature List File
US20090138874A1 (en) * 2007-11-27 2009-05-28 The Boeing Company Software Maintenance Tool
US20090138385A1 (en) * 2007-11-27 2009-05-28 The Boeing Company Crate Tool
US20090138516A1 (en) * 2007-11-27 2009-05-28 The Boeing Company Aircraft software part library
US20090141669A1 (en) * 2007-12-04 2009-06-04 Honeywell International Inc. Travel characteristics-based ad-hoc communication network algorithm selection
US20090192659A1 (en) * 2008-01-30 2009-07-30 Beebe Clifford A Aircraft maintenance laptop
US20090197595A1 (en) * 2008-02-04 2009-08-06 Honeywell International Inc. Use of alternate communication networks to complement an ad-hoc mobile node to mobile node communication network
US20090196201A1 (en) * 2008-02-01 2009-08-06 Airbus France Switching device adapted to switch an aircraft wireless network from a maintenance configuration to a commercial configuration and vice-versa
US20090318138A1 (en) * 2008-06-20 2009-12-24 Honeywell International Inc. System and method for in-flight wireless communication
US20090318137A1 (en) * 2008-06-20 2009-12-24 Honeywell International Inc. Internetworking air-to-air network and wireless network
US20100036547A1 (en) * 2005-02-25 2010-02-11 The Boeing Company System and methods for on-board pre-flight aircraft dispatching
US20100075614A1 (en) * 2008-09-23 2010-03-25 Honeywell International Inc. Communication management unit server capability
US7827400B2 (en) 2005-07-28 2010-11-02 The Boeing Company Security certificate management
US20110040595A1 (en) * 2009-08-12 2011-02-17 Chou Y Hong Real-time service management and dispatch system
US7921442B2 (en) 2000-08-16 2011-04-05 The Boeing Company Method and apparatus for simultaneous live television and data services using single beam antennas
US20110185207A1 (en) * 2010-01-25 2011-07-28 Honeywell International Inc. Pcmcia memory card with ethernet/wireless connectivity and battery backup for avionics applications
US20110252295A1 (en) * 2010-04-09 2011-10-13 Beacham William H Avionic data validation system
US8160757B1 (en) * 2007-05-18 2012-04-17 Rockwell Collins, Inc. System and method for providing optimum multi-map overlay in a flight deck navigation display
US8228911B2 (en) 2008-09-19 2012-07-24 Honeywell International Inc. Enhanced data link communication over iridium
US8515658B1 (en) * 2009-07-06 2013-08-20 The Boeing Company Managing navigational chart presentation
US20130232237A1 (en) * 2012-03-01 2013-09-05 Honeywell International Inc. Programmable portable electronic device for airborne operational communications
US20140316613A1 (en) * 2013-04-23 2014-10-23 The Boeing Company Aircraft Performance Monitoring System
US9160543B2 (en) 2013-05-07 2015-10-13 The Boeing Company Verification of aircraft information in response to compromised digital certificate
US9237022B2 (en) 2013-05-07 2016-01-12 The Boeing Company Use of multiple digital signatures and quorum rules to verify aircraft information
US20160016671A1 (en) * 2014-07-18 2016-01-21 Thales Processing of aircraft alarm and maintenance messages
US20160036513A1 (en) * 2013-04-22 2016-02-04 Chad Klippert Aircraft flight data monitoring and reporting system and use thereof
US9306657B2 (en) 2005-04-08 2016-04-05 The Boeing Company Soft handoff method and apparatus for mobile vehicles using directional antennas
US20160197857A1 (en) * 2015-01-06 2016-07-07 The Boeing Company Aircraft control domain communication framework
US9563580B2 (en) 2013-07-25 2017-02-07 North Flight Data Systems, LLC System, methodology, and process for wireless transmission of sensor data onboard an aircraft to a portable electronic device
US9576404B2 (en) 2004-09-16 2017-02-21 Harris Corporation System and method of transmitting data from an aircraft
US9826039B2 (en) 2014-02-04 2017-11-21 Honeywell International Inc. Configurable communication systems and methods for communication

Families Citing this family (202)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8363744B2 (en) * 2001-06-10 2013-01-29 Aloft Media, Llc Method and system for robust, secure, and high-efficiency voice and packet transmission over ad-hoc, mesh, and MIMO communication networks
USRE45775E1 (en) 2000-06-13 2015-10-20 Comcast Cable Communications, Llc Method and system for robust, secure, and high-efficiency voice and packet transmission over ad-hoc, mesh, and MIMO communication networks
US20020160773A1 (en) * 2001-03-29 2002-10-31 Tenzing Communications, Inc. Communications systems for aircraft including wireless systems
US20040206818A1 (en) * 2001-12-03 2004-10-21 Loda David C. Engine-mounted microserver
US8082317B2 (en) * 2002-02-26 2011-12-20 United Technologies Corporation Remote tablet-based internet inspection system
US7069261B2 (en) * 2002-04-02 2006-06-27 The Boeing Company System, method and computer program product for accessing electronic information
US7689752B1 (en) * 2002-09-11 2010-03-30 Gte Wireless Incorporated Cabin telecommunication unit
US6894611B2 (en) * 2002-09-23 2005-05-17 General Electric Company Method and system for uploading and downloading engine control data
US20080039997A1 (en) * 2003-11-10 2008-02-14 Aeromechanical Services Ltd. Aircraft flight data management system
US9374828B2 (en) * 2003-01-13 2016-06-21 Hamilton Sundstrand Corporation Channel allocation for a multi-device communication system
US20070176840A1 (en) * 2003-02-06 2007-08-02 James Pristas Multi-receiver communication system with distributed aperture antenna
US7356336B2 (en) * 2004-01-06 2008-04-08 The Boeing Company Systems and methods of recording events onboard a vehicle
US7844385B2 (en) * 2004-01-28 2010-11-30 United Technologies Corporation Microserver engine control card
US7167788B2 (en) * 2004-01-30 2007-01-23 United Technologies Corporation Dual-architecture microserver card
DE102004005680A1 (en) * 2004-02-05 2005-08-25 Bayerische Motoren Werke Ag Apparatus and method for controlling control devices in an electrical system of a motor vehicle
WO2005111871A1 (en) 2004-05-07 2005-11-24 Panasonic Avionics Corporation System and method for managing content on mobile platforms
FR2871012B1 (en) * 2004-05-28 2006-08-11 Sagem Method file upload from a client to a target server and device for implementing PROCESS
US7584032B2 (en) * 2004-06-17 2009-09-01 Honeywell International Inc. Method and system for dynamic collection of flight test data
US20060018479A1 (en) * 2004-06-29 2006-01-26 Ying-Nan Chen Update method for wireless system of vehicle security system
DE102004049895A1 (en) * 2004-10-13 2006-04-20 Airbus Deutschland Gmbh Interface device for a communications network for multiple electronic units in an aircraft has a switching unit and send and receive antennae for unique connection of any of a 1st node group to any of a wireless 2nd node group
EP1813035B1 (en) * 2004-11-05 2014-03-05 Panasonic Avionics Corporation System and method for receiving broadcast content on a mobile platform during international travel
JP4742138B2 (en) * 2005-03-29 2011-08-10 パナソニック・アビオニクス・コーポレイションPanasonic Avionics Corporation System and method for routing communication signals over a data distribution network
WO2006113858A3 (en) * 2005-04-19 2007-03-29 Long Bui System and method for presenting high-quality video
US8854980B2 (en) 2005-05-06 2014-10-07 Lockheed Martin Corporation Switching module
CN101253768B (en) * 2005-06-23 2012-07-04 松下航空电子公司 System and method for providing searchable data transport stream encryption
US8944822B2 (en) * 2005-07-22 2015-02-03 Appareo Systems, Llc Synchronized video and synthetic visualization system and method
US7848698B2 (en) 2005-07-22 2010-12-07 Appareo Systems Llc Flight training and synthetic flight simulation system and method
US7724848B2 (en) * 2005-07-26 2010-05-25 Data Device Corporation Predictive signal cancellation for extracting 1 Mb/s MIL-STD-1553 component from composite high performance 1553 signal
DE102005043335A1 (en) * 2005-09-12 2007-05-16 Siemens Ag Arrangement with a tachograph
US20070121641A1 (en) * 2005-10-21 2007-05-31 Hovey Matthew N Method and system for network services with a mobile vehicle
FI20051216A0 (en) * 2005-11-29 2005-11-29 Nokia Corp Method, system and arrangements for establishing and maintaining a WLAN connection predictably moving vehicle
US20070136078A1 (en) 2005-12-08 2007-06-14 Smartdrive Systems Inc. Vehicle event recorder systems
US20070150138A1 (en) 2005-12-08 2007-06-28 James Plante Memory management in event recording systems
US20070132773A1 (en) * 2005-12-08 2007-06-14 Smartdrive Systems Inc Multi-stage memory buffer and automatic transfers in vehicle event recording systems
US7898383B2 (en) * 2006-03-13 2011-03-01 The Boeing Company System and method for detecting security violation
US9201842B2 (en) 2006-03-16 2015-12-01 Smartdrive Systems, Inc. Vehicle event recorder systems and networks having integrated cellular wireless communications systems
US8996240B2 (en) 2006-03-16 2015-03-31 Smartdrive Systems, Inc. Vehicle event recorders with integrated web server
US7987027B2 (en) * 2006-04-27 2011-07-26 Caterpillar Inc. Systems for processing machine health information
US20100005194A1 (en) * 2006-04-28 2010-01-07 Avfinity, Inc Method, system, apparatus, and storage device to facilitate communication between systems
US8239575B2 (en) * 2006-04-28 2012-08-07 Avfinity, Llc Method, system, apparatus, and program to facilitate communication between systems
US7756134B2 (en) 2006-05-02 2010-07-13 Harris Corporation Systems and methods for close queuing to support quality of service
FR2901442B1 (en) * 2006-05-17 2008-08-22 Airbus France Sas Method Secure file transfer
US7894509B2 (en) * 2006-05-18 2011-02-22 Harris Corporation Method and system for functional redundancy based quality of service
US7920588B2 (en) * 2006-05-22 2011-04-05 Edgewater Computer Systems, Inc. Data communications system and method of data transmission
US7990860B2 (en) 2006-06-16 2011-08-02 Harris Corporation Method and system for rule-based sequencing for QoS
US8064464B2 (en) 2006-06-16 2011-11-22 Harris Corporation Method and system for inbound content-based QoS
US8516153B2 (en) 2006-06-16 2013-08-20 Harris Corporation Method and system for network-independent QoS
US7856012B2 (en) 2006-06-16 2010-12-21 Harris Corporation System and methods for generic data transparent rules to support quality of service
US7916626B2 (en) 2006-06-19 2011-03-29 Harris Corporation Method and system for fault-tolerant quality of service
US8730981B2 (en) 2006-06-20 2014-05-20 Harris Corporation Method and system for compression based quality of service
US7769028B2 (en) 2006-06-21 2010-08-03 Harris Corporation Systems and methods for adaptive throughput management for event-driven message-based data
US20070298741A1 (en) * 2006-06-22 2007-12-27 Harnist Kevin A Multi radio/multi channel base station for wireless networks
US8903789B2 (en) * 2006-07-12 2014-12-02 Verizon Patent And Licensing Inc. Derived presence-aware service from associated entities
US7881276B2 (en) * 2006-07-31 2011-02-01 Industrial Technology Research Institute System and method for relaying data
FR2904448B1 (en) * 2006-07-31 2008-09-26 Airbus France Sas Method and device support in the management of successive flights of an aircraft.
US7926758B2 (en) * 2006-07-31 2011-04-19 Industrial Technology Research Institute Apparatus and system for roll-to-roll processing
US8300653B2 (en) 2006-07-31 2012-10-30 Harris Corporation Systems and methods for assured communications with quality of service
US7822126B2 (en) * 2006-08-10 2010-10-26 Edgewater Computer Systems, Inc. Interference cancellation system and method
CA2661897A1 (en) 2006-09-15 2008-03-20 Thales Avionics, Inc. System and method for wirelessly transferring content to and from an aircraft
FR2906048B1 (en) * 2006-09-19 2008-12-19 Thales Sa Method and device for modifying a flight plan including a procedure for an aircraft takeoff
US8116922B2 (en) * 2006-09-25 2012-02-14 Appareo Systems, Llc Method for resolving ground level errors in simulations
US7616449B2 (en) * 2006-09-25 2009-11-10 Appareo Systems, Llc Crash-hardened memory device and method of creating the same
US8565943B2 (en) * 2006-09-25 2013-10-22 Appereo Systems, LLC Fleet operations quality management system
US9202318B2 (en) 2006-09-25 2015-12-01 Appareo Systems, Llc Ground fleet operations quality management system
US9047717B2 (en) 2006-09-25 2015-06-02 Appareo Systems, Llc Fleet operations quality management system and automatic multi-generational data caching and recovery
US8280366B2 (en) * 2006-10-10 2012-10-02 Broadcom Corporation Sensing RF environment to detect change in geographic location of cellular base station
US8744466B2 (en) * 2006-10-10 2014-06-03 Broadcom Corporation Sensing RF environment to manage mobile network resources
US8620342B2 (en) 2006-10-10 2013-12-31 Broadcom Corporation Sensing RF environment to determine geographic location of cellular base station
US7907690B2 (en) * 2006-10-17 2011-03-15 Edgewater Computer Systems, Inc. Interference cancellation system and method using impulse response
US8285694B1 (en) 2006-10-17 2012-10-09 At&T Mobility Ii Llc Distribution of enterprise related alerts via the emergency alert system
EP1916781B1 (en) * 2006-10-24 2012-04-18 Rockwell-Collins France Radio communication system for ACARS messages exchange
US8989959B2 (en) 2006-11-07 2015-03-24 Smartdrive Systems, Inc. Vehicle operator performance history recording, scoring and reporting systems
US8649933B2 (en) 2006-11-07 2014-02-11 Smartdrive Systems Inc. Power management systems for automotive video event recorders
US20080114856A1 (en) * 2006-11-09 2008-05-15 Gary Kendall System and method for autonomously delivering information on demand
US8868288B2 (en) 2006-11-09 2014-10-21 Smartdrive Systems, Inc. Vehicle exception event management systems
US20080143497A1 (en) * 2006-12-15 2008-06-19 General Motors Corporation Vehicle Emergency Communication Mode Method and Apparatus
EP2118873A2 (en) 2006-12-19 2009-11-18 Engineered Arresting Systems Corporation System and method for providing runway conditions to landing aircraft
US20080167820A1 (en) * 2007-01-04 2008-07-10 Kentaro Oguchi System for predicting driver behavior
JP2008269395A (en) * 2007-04-23 2008-11-06 Fujitsu Ten Ltd Multimedia system and navigation unit terminal
US8239092B2 (en) 2007-05-08 2012-08-07 Smartdrive Systems Inc. Distributed vehicle event recorder systems having a portable memory data transfer system
US20080295090A1 (en) * 2007-05-24 2008-11-27 Lockheed Martin Corporation Software configuration manager
US8289201B2 (en) 2007-06-06 2012-10-16 The Boeing Company Method and apparatus for using non-linear ground penetrating radar to detect objects located in the ground
US8299924B2 (en) 2007-06-06 2012-10-30 The Boeing Company Method and apparatus for locating objects using radio frequency identification
US7893862B2 (en) * 2007-06-06 2011-02-22 The Boeing Company Method and apparatus for using collimated and linearly polarized millimeter wave beams at Brewster's angle of incidence in ground penetrating radar to detect objects located in the ground
US20090030563A1 (en) * 2007-07-26 2009-01-29 United Technologies Corp. Systems And Methods For Providing Localized Heat Treatment Of Metal Components
US20090070841A1 (en) * 2007-09-12 2009-03-12 Proximetry, Inc. Systems and methods for delivery of wireless data and multimedia content to aircraft
US8326282B2 (en) * 2007-09-24 2012-12-04 Panasonic Avionics Corporation System and method for receiving broadcast content on a mobile platform during travel
CN101822047A (en) * 2007-10-05 2010-09-01 松下航空电子公司 System and method for presenting advertisement content on a mobile platform during travel
US20090106749A1 (en) * 2007-10-23 2009-04-23 Wolfgang Daum System, method, and computer software code for determining whether a change in a subsystem is compatible with a system
US8644225B2 (en) * 2007-11-19 2014-02-04 Telcordia Technologies, Inc. Method for determining transmission channels for a LPG based vehicle communication network
US8055393B2 (en) * 2008-02-06 2011-11-08 The Boeing Company Method and apparatus for loading software aircraft parts
US8051031B2 (en) * 2008-02-06 2011-11-01 The Boeing Company Metadata for software aircraft parts
CN101939932A (en) * 2008-02-08 2011-01-05 松下航空电子公司 Optical communication system and method for distributing content aboard a mobile platform during travel
US8516096B2 (en) * 2008-07-09 2013-08-20 In Motion Technology Inc. Cognitive wireless system
US8352577B2 (en) * 2008-07-22 2013-01-08 Lockheed Martin Corporation Method and apparatus for updating information on an embedded system
FR2935079B1 (en) * 2008-08-13 2013-02-08 Airbus France hybrid communication system ACARS
US8121593B2 (en) * 2008-10-07 2012-02-21 Honeywell International Inc. System and method for air-to-air communications using network formed between aircraft
EP2345022A1 (en) * 2008-10-10 2011-07-20 Raytheon Company Tracking air and ground vehicles
US9398096B2 (en) * 2008-11-10 2016-07-19 Volkswagen Ag System and method for accessing an in-vehicle communication network via a media interface
US8447977B2 (en) * 2008-12-09 2013-05-21 Canon Kabushiki Kaisha Authenticating a device with a server over a network
US8509990B2 (en) 2008-12-15 2013-08-13 Panasonic Avionics Corporation System and method for performing real-time data analysis
JP4748332B2 (en) * 2008-12-15 2011-08-17 信越化学工業株式会社 Fiber treatment agent composition, detergents and fabric softeners, as well as the treated textile by these
US8169999B2 (en) 2009-01-16 2012-05-01 Broadcom Corporation Method and system for preserving content timing across femtocell interfaces via timestamp insertion
US9003500B2 (en) * 2009-03-13 2015-04-07 Hti Ip, Llc Method and system for facilitating synchronizing media content between a vehicle device and a user device
FR2943152A1 (en) * 2009-03-13 2010-09-17 Airbus France Processes and devices automates download software, in an apparatus such as aircraft, comprising the updating of the associated documentation
US9379775B2 (en) 2009-03-17 2016-06-28 General Electric Company Data communication system and method
US8532850B2 (en) 2009-03-17 2013-09-10 General Electric Company System and method for communicating data in locomotive consist or other vehicle consist
US8935022B2 (en) 2009-03-17 2015-01-13 General Electric Company Data communication system and method
US8798821B2 (en) 2009-03-17 2014-08-05 General Electric Company System and method for communicating data in a locomotive consist or other vehicle consist
US9637147B2 (en) 2009-03-17 2017-05-02 General Electronic Company Data communication system and method
US8583299B2 (en) 2009-03-17 2013-11-12 General Electric Company System and method for communicating data in a train having one or more locomotive consists
US8259617B2 (en) 2009-03-18 2012-09-04 Broadcom Corporation Method and system for timely delivery of multimedia content via a femtocell
US8903669B1 (en) 2009-03-27 2014-12-02 The Boeing Company Multi-band receiver using harmonic synchronous detection
US8054212B1 (en) 2009-03-27 2011-11-08 The Boeing Company Multi-band receiver using harmonic synchronous detection
US8271709B2 (en) * 2009-05-11 2012-09-18 Honeywell International Inc. Bus protocol for control of communications between two computers
US8054204B2 (en) * 2009-05-29 2011-11-08 United Technologies Corporation Method for remotely updating wireless sensors
US8275572B2 (en) * 2009-06-10 2012-09-25 The Boeing Company Difference frequency detection with range measurement
WO2010144815A9 (en) 2009-06-11 2011-06-30 Panasonic Avionics Corporation System and method for providing security aboard a moving platform
FR2946769B1 (en) * 2009-06-16 2011-07-01 Airbus France Method and avionics reconfiguration device.
US8509963B1 (en) * 2009-07-23 2013-08-13 Rockwell Collins, Inc. Remote management of aircraft computer systems
JP4883149B2 (en) * 2009-07-28 2012-02-22 富士通株式会社 Mobile communication device, a communication method and a communication system
WO2011018656A3 (en) 2009-08-12 2011-12-15 Bae Systems Plc System integration
US8326959B2 (en) * 2009-09-04 2012-12-04 Spirit Aerosystems, Inc. Virtual production testing of large integrated products
DE102009041599A1 (en) * 2009-09-15 2011-04-14 Airbus Operations Gmbh Control means, input / output device connection switching apparatus and method for an aircraft control system
US9016627B2 (en) 2009-10-02 2015-04-28 Panasonic Avionics Corporation System and method for providing an integrated user interface system at a seat
US8452475B1 (en) * 2009-10-02 2013-05-28 Rockwell Collins, Inc. Systems and methods for dynamic aircraft maintenance scheduling
US20110205364A1 (en) * 2009-11-09 2011-08-25 Charles Lampe Method and apparatus to transmit video data
EP2378468A1 (en) * 2009-11-10 2011-10-19 Airbus Operations GmbH Platform for aircraft maintenance services and asset management
CN102870306B (en) 2009-12-14 2015-09-09 松下航空电子公司 Systems and methods for providing dynamic power management
EP2526506A1 (en) * 2010-01-21 2012-11-28 Telcordia Technologies, Inc. System and method for load balancing and handoff management based on flight plan and channel occupancy
GB201002889D0 (en) * 2010-02-19 2010-04-07 Thales Holdings Uk Plc Aircraft radio system
US8340839B2 (en) * 2010-03-22 2012-12-25 Honeywell International Inc. Aircraft communications radio tuning aid system and method
WO2011137101A1 (en) 2010-04-27 2011-11-03 Panasonic Avionics Corporation Deployment system and method for user interface devices
FR2959633B1 (en) * 2010-04-29 2012-08-31 Airbus Operations Sas Method for setting a level of an aircraft
DE102010019394A1 (en) * 2010-05-04 2011-11-10 Becker Flugfunkwerk Gmbh Communication system for an aircraft
US8655517B2 (en) 2010-05-19 2014-02-18 General Electric Company Communication system and method for a rail vehicle consist
US8825239B2 (en) 2010-05-19 2014-09-02 General Electric Company Communication system and method for a rail vehicle consist
FR2962619B1 (en) * 2010-07-09 2013-01-18 Thales Sa Device access to data aboard an aircraft
US8301196B2 (en) * 2010-08-03 2012-10-30 Honeywell International Inc. Reconfigurable wireless modem adapter including diversity/MIMO modems
US8326359B2 (en) * 2010-08-03 2012-12-04 Honeywell International Inc. Reconfigurable wireless modem adapter
US8417860B2 (en) 2010-08-05 2013-04-09 Honda Motor Co., Ltd. Hybrid in-vehicle infotainment network
EP2614003B1 (en) 2010-09-10 2016-04-20 Panasonic Avionics Corporation Chair with an integrated user interface system and method
US9349295B2 (en) * 2010-09-27 2016-05-24 Honeywell International Inc. Mixed-intiative transfer of datalink-based information
US8702043B2 (en) 2010-09-28 2014-04-22 General Electric Company Rail vehicle control communication system and method for communicating with a rail vehicle
US9412273B2 (en) 2012-03-14 2016-08-09 Autoconnect Holdings Llc Radar sensing and emergency response vehicle detection
US9384609B2 (en) 2012-03-14 2016-07-05 Autoconnect Holdings Llc Vehicle to vehicle safety and traffic communications
US9082238B2 (en) 2012-03-14 2015-07-14 Flextronics Ap, Llc Synchronization between vehicle and user device calendar
US9082239B2 (en) 2012-03-14 2015-07-14 Flextronics Ap, Llc Intelligent vehicle for assisting vehicle occupants
US9378601B2 (en) 2012-03-14 2016-06-28 Autoconnect Holdings Llc Providing home automation information via communication with a vehicle
US20120106653A1 (en) * 2010-11-03 2012-05-03 Broadcom Corporation Multimedia processing within a vehicular communication network
US9513630B2 (en) 2010-11-17 2016-12-06 General Electric Company Methods and systems for data communications
US8929830B2 (en) * 2011-01-24 2015-01-06 Honeywell International Inc. Systems and methods for detecting a loss of communication using statistical analysis
FR2973131B1 (en) 2011-03-22 2013-04-19 Airbus Operations Sas Method and device incompatibilities of detection of logical interfaces for embedded systems equipment
JP2012222403A (en) * 2011-04-04 2012-11-12 Denso Corp Information display system, and in-vehicle device and portable device constituting the system
US8516150B2 (en) 2011-04-11 2013-08-20 Honeywell International Inc. Systems and methods for multiple computer dataloading using a standard dataloader
US20120290529A1 (en) * 2011-05-09 2012-11-15 Honeywell International Inc. Systems and methods for updating a database and handling interruptions
WO2012172319A1 (en) * 2011-06-15 2012-12-20 Bae Systems Plc Data transfer
US9350423B2 (en) 2011-06-30 2016-05-24 The Boeing Company Methods and system for increasing data transmission rates across a three-phase power system
EP2734905A4 (en) 2011-07-22 2015-04-08 Aspen Avionics Inc Avionics gateway interface, systems and methods
US8762990B2 (en) 2011-07-25 2014-06-24 The Boeing Company Virtual machines for aircraft network data processing systems
US9239247B1 (en) * 2011-09-27 2016-01-19 The Boeing Company Verification of devices connected to aircraft data processing systems
US8806579B1 (en) 2011-10-12 2014-08-12 The Boeing Company Secure partitioning of devices connected to aircraft network data processing systems
US8589020B1 (en) 2011-11-29 2013-11-19 The Boeing Company Updating identity information in aircraft network data processing systems
US8914170B2 (en) 2011-12-07 2014-12-16 General Electric Company System and method for communicating data in a vehicle system
FR2990547B1 (en) * 2012-05-11 2014-06-20 Thales Sa Maintenance System centralized parameterizable indicated to an aircraft
US9336187B2 (en) * 2012-05-14 2016-05-10 The Boeing Company Mediation computing device and associated method for generating semantic tags
US9092611B1 (en) * 2012-06-11 2015-07-28 Rockwell Collins, Inc. Adaptive, multi-level security for flight deck applications hosted on mobile platforms
US9172481B2 (en) 2012-07-20 2015-10-27 Appareo Systems, Llc Automatic multi-generational data caching and recovery
US9728228B2 (en) 2012-08-10 2017-08-08 Smartdrive Systems, Inc. Vehicle event playback apparatus and methods
GB201214921D0 (en) * 2012-08-22 2012-10-03 Ge Aviat Systems Ltd Method and system of implementing data load protocols
US9334063B2 (en) * 2012-09-10 2016-05-10 Rosemount Aerospace, Inc. Aircraft avionics tablet interface module
FR2997259B1 (en) * 2012-10-23 2015-11-20 Sagem Defense Securite PCMCIA card to transfer flight data
US9818151B2 (en) * 2012-12-04 2017-11-14 I.D. Systems, Inc. Remote vehicle rental systems and methods
US9277352B1 (en) * 2013-01-14 2016-03-01 Amazon Technologies, Inc. Mobile distributed memory systems
FR3001061B1 (en) * 2013-01-15 2015-02-27 Airbus Operations Sas Steering system for aircraft provided with a performance feature server.
US9264905B2 (en) 2013-02-21 2016-02-16 Digi International Inc. Establishing secure connection between mobile computing device and wireless hub using security credentials obtained from remote security credential server
CA2841685A1 (en) 2013-03-15 2014-09-15 Panasonic Avionics Corporation System and method for providing multi-mode wireless data distribution
CN104321620A (en) 2013-04-15 2015-01-28 弗莱克斯电子有限责任公司 Altered map routes based on user profile information
US20140309872A1 (en) 2013-04-15 2014-10-16 Flextronics Ap, Llc Customization of vehicle user interfaces based on user intelligence
US20150032296A1 (en) * 2013-07-26 2015-01-29 Bell Helicopter Textron Inc. Avionics system adapted for employing smartphone to input-output flight data
US9501878B2 (en) 2013-10-16 2016-11-22 Smartdrive Systems, Inc. Vehicle event playback apparatus and methods
US9610955B2 (en) 2013-11-11 2017-04-04 Smartdrive Systems, Inc. Vehicle fuel consumption monitor and feedback systems
US9419846B2 (en) 2014-01-03 2016-08-16 Honeywell International Inc. Integrated wireless module
US8892310B1 (en) 2014-02-21 2014-11-18 Smartdrive Systems, Inc. System and method to detect execution of driving maneuvers
US9607445B2 (en) * 2014-02-27 2017-03-28 Satcom Direct, Inc. System for automated recording of aircraft flight and maintenance information and associated methods
US9482552B2 (en) * 2014-06-23 2016-11-01 Ge Aviation Systems Llc Method of simulating a real-time aircraft system input to an avionics component
US9756485B2 (en) * 2014-10-02 2017-09-05 Deborah Lynn Pinard Methods and systems for walkie-talkie communications
US9663127B2 (en) 2014-10-28 2017-05-30 Smartdrive Systems, Inc. Rail vehicle event detection and recording system
CN104580459A (en) * 2015-01-06 2015-04-29 中电科航空电子有限公司 Avionics target hardware equipment Ethernet data loading method
KR101621878B1 (en) * 2015-01-21 2016-05-17 현대자동차주식회사 A communication system of avn for vehicle, and a method of wireless communication for the same
US9699200B2 (en) 2015-05-07 2017-07-04 The Boeing Company Inline arinc data authenticity inspection module, method and computer program product
US9965262B2 (en) * 2015-05-21 2018-05-08 International Business Machines Corporation Application bundle pulling
US20170013086A1 (en) * 2015-07-06 2017-01-12 The Boeing Company Wireless Software Loader
DE102015224950A1 (en) * 2015-12-11 2017-06-14 Airbus Operations Gmbh Technique for updating software on board an aircraft
US9817654B2 (en) * 2016-02-23 2017-11-14 The Boeing Company System and method for communication of software
US9824513B2 (en) 2016-04-14 2017-11-21 United Airlines, Inc. Method of detecting elevator tab failure
US20180004691A1 (en) * 2016-06-30 2018-01-04 Ge Aviation Systems Llc Management of data transfers
US20180012197A1 (en) 2016-07-07 2018-01-11 NextEv USA, Inc. Battery exchange licensing program based on state of charge of battery pack
US9928734B2 (en) 2016-08-02 2018-03-27 Nio Usa, Inc. Vehicle-to-pedestrian communication systems
US9967172B2 (en) 2016-10-11 2018-05-08 Panasonic Avionics Corporation Methods and systems for content loading and offloading to and from a transportation vehicle
US20180121188A1 (en) * 2016-10-27 2018-05-03 Honeywell International Inc. Tracking aircraft with older version of software/database and initiating autoload of latest version of software/database when aircraft is in safe state for dataload
US20180127001A1 (en) 2016-11-07 2018-05-10 NextEv USA, Inc. Feedback Performance Control and Tracking

Family Cites Families (51)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3573740A (en) * 1968-07-03 1971-04-06 Ncr Co Communication multiplexer for online data transmission
US5077671A (en) * 1989-07-05 1991-12-31 The Boeing Company Test cart for aircraft control surface measurements
US5079707A (en) * 1990-01-19 1992-01-07 The Boeing Company Integrated certification-calibration system for a testing system having multiple test instruments
FR2676319B1 (en) * 1991-05-07 1993-12-10 Sextant Avionique Method and device selection information used by a local unit reliee a digital transmission system.
US5307505A (en) * 1992-05-05 1994-04-26 The United States Of America As Represented By The Secretary Of The Navy Rapid reprogramming terminal
FR2692667B1 (en) * 1992-06-18 1994-08-19 Alsthom Cge Alcatel A device for measuring displacement for vehicle, particularly for all-terrain robot, and vehicle fitted with such a device.
US5959596A (en) * 1993-06-24 1999-09-28 Nintendo Co., Ltd. Airline-based video game and communications system
US5424949A (en) * 1993-07-30 1995-06-13 Honeywell Inc. Multi-channel data receiver system
US5761625A (en) * 1995-06-07 1998-06-02 Alliedsignal Inc. Reconfigurable algorithmic networks for aircraft data management
US6047165A (en) * 1995-11-14 2000-04-04 Harris Corporation Wireless, frequency-agile spread spectrum ground link-based aircraft data communication system
US6275172B1 (en) * 1996-02-29 2001-08-14 L-3 Communications Corporation Method and apparatus for improving performance of aircraft display utilizing TCAS computer and mode S transponder
US5805828A (en) * 1996-05-14 1998-09-08 The Boeing Company Method and apparatus for an avionics system utilizing both ARINC 429 and ARINC 629 compliant systems
DE19628918C1 (en) * 1996-07-18 1997-07-31 Daimler Benz Aerospace Airbus Arrangement for detecting HF noise signal on board aircraft esp. passenger aircraft
US5841969A (en) * 1996-08-13 1998-11-24 Honeywell Inc. Single bus architecture supporting subsystems of various criticality levels
US6236365B1 (en) * 1996-09-09 2001-05-22 Tracbeam, Llc Location of a mobile station using a plurality of commercial wireless infrastructures
US7764231B1 (en) * 1996-09-09 2010-07-27 Tracbeam Llc Wireless location using multiple mobile station location techniques
US7714778B2 (en) * 1997-08-20 2010-05-11 Tracbeam Llc Wireless location gateway and applications therefor
US6201797B1 (en) * 1997-12-12 2001-03-13 At&T Wireless Services Inc. High bandwidth delivery and internet access for airborne passengers
US6181990B1 (en) * 1998-07-30 2001-01-30 Teledyne Technologies, Inc. Aircraft flight data acquisition and transmission system
GB9909825D0 (en) * 1998-09-08 1999-06-23 Airnet Global Holdings Limited Communications system for aircraft
US6760778B1 (en) * 1998-09-09 2004-07-06 At&T Wireless Services, Inc. System and method for communication between airborne and ground-based entities
US6546425B1 (en) * 1998-10-09 2003-04-08 Netmotion Wireless, Inc. Method and apparatus for providing mobile and other intermittent connectivity in a computing environment
US20030146871A1 (en) * 1998-11-24 2003-08-07 Tracbeam Llc Wireless location using signal direction and time difference of arrival
US6385513B1 (en) * 1998-12-08 2002-05-07 Honeywell International, Inc. Satellite emergency voice/data downlink
US6459411B2 (en) * 1998-12-30 2002-10-01 L-3 Communications Corporation Close/intra-formation positioning collision avoidance system and method
US6477152B1 (en) * 1998-12-30 2002-11-05 Honeywell Inc. Apparatus and method for data communications
US6545601B1 (en) * 1999-02-25 2003-04-08 David A. Monroe Ground based security surveillance system for aircraft and other commercial vehicles
US6262679B1 (en) * 1999-04-08 2001-07-17 Honeywell International Inc. Midair collision avoidance system
US6154636A (en) * 1999-05-14 2000-11-28 Harris Corporation System and method of providing OOOI times of an aircraft
US6148179A (en) * 1999-06-25 2000-11-14 Harris Corporation Wireless spread spectrum ground link-based aircraft data communication system for engine event reporting
US6163681A (en) * 1999-06-25 2000-12-19 Harris Corporation Wireless spread spectrum ground link-based aircraft data communication system with variable data rate
US6160998A (en) * 1999-06-25 2000-12-12 Harris Corporation Wireless spread spectrum ground link-based aircraft data communication system with approach data messaging download
US6173159B1 (en) * 1999-06-25 2001-01-09 Harris Corporation Wireless spread spectrum ground link-based aircraft data communication system for updating flight management files
US6167238A (en) * 1999-06-25 2000-12-26 Harris Corporation Wireless-based aircraft data communication system with automatic frequency control
US6167239A (en) * 1999-06-25 2000-12-26 Harris Corporation Wireless spread spectrum ground link-based aircraft data communication system with airborne airline packet communications
US6522888B1 (en) * 1999-08-31 2003-02-18 Lucent Technologies Inc. System for determining wireless coverage using location information for a wireless unit
US6298092B1 (en) * 1999-12-15 2001-10-02 Iospan Wireless, Inc. Methods of controlling communication parameters of wireless systems
JP3414357B2 (en) * 2000-04-25 2003-06-09 日本電気株式会社 Transmission power control scheme in Cdma mobile communication system
US20030093798A1 (en) * 2000-07-10 2003-05-15 Michael Rogerson Modular entertainment system configured for multiple broadband content delivery incorporating a distributed server
US6438468B1 (en) * 2000-11-28 2002-08-20 Honeywell International Inc. Systems and methods for delivering data updates to an aircraft
US6671589B2 (en) * 2001-02-13 2003-12-30 William Holst Method and apparatus to support remote and automatically initiated data loading and data acquisition of airborne computers using a wireless spread spectrum aircraft data services link
US6747577B2 (en) * 2001-11-26 2004-06-08 The Boeing Company Methods and systems for air vehicle telemetry
US20040198386A1 (en) * 2002-01-16 2004-10-07 Dupray Dennis J. Applications for a wireless location gateway
FR2837585B1 (en) * 2002-03-25 2004-06-25 Airbus France Installation, gateway and method to download information between Embedded equipment on an aircraft and means of non-Embedded loading
US6937164B2 (en) * 2003-02-17 2005-08-30 The Boeing Company Methods and apparatus for transportation vehicle security monitoring
US7215969B2 (en) * 2003-07-21 2007-05-08 Lucent Technologies Inc. Method for RF dead zone data collection using mobile station
US7197310B2 (en) * 2003-07-29 2007-03-27 Lucent Technologies Inc. Methods and systems for controlling handoffs in a wireless communication system
US7260408B2 (en) * 2004-02-20 2007-08-21 Airespace, Inc. Wireless node location mechanism using antenna pattern diversity to enhance accuracy of location estimates
US7286833B2 (en) * 2004-02-27 2007-10-23 Airespace, Inc. Selective termination of wireless connections to refresh signal information in wireless node location infrastructure
US7116988B2 (en) * 2004-03-16 2006-10-03 Airespace, Inc. Location of wireless nodes using signal strength weighting metric
US7489992B2 (en) * 2004-04-12 2009-02-10 Sagem Avionics, Inc. Method and system for remotely communicating and interfacing with aircraft condition monitoring systems

Cited By (208)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20070220109A1 (en) * 1998-09-09 2007-09-20 Nelson Eric A Method and Apparatus For Data Communication Utilizing The North American Terrestrial System
US8495240B2 (en) 1998-09-09 2013-07-23 At&T Mobility Ii Llc Method and apparatus for data communication utilizing the North American terrestrial system
US20090077203A1 (en) * 1999-03-04 2009-03-19 Ez4Media, Inc. Clock with link to the internet
US20090298490A9 (en) * 1999-03-04 2009-12-03 Janik Craig M System for providing content, management, and interactivity for thin client devices
US20040253945A1 (en) * 1999-03-04 2004-12-16 Janik Craig M. System for providing content, management, and interactivity for thin client devices
US7937450B2 (en) 1999-03-04 2011-05-03 Viviana Research Llc System for providing content, management, and interactivity for thin client devices
US9042205B2 (en) 1999-03-04 2015-05-26 Viviana Research Llc Clock with link to the internet
US8578037B2 (en) 1999-05-14 2013-11-05 At&T Mobility Ii Llc Aircraft data services
US8250221B2 (en) * 1999-05-14 2012-08-21 At&T Mobility Ii Llc Aircraft data communications services for users
US20050220055A1 (en) * 1999-05-14 2005-10-06 Nelson Eric A Aircraft data communications services for users
US7921442B2 (en) 2000-08-16 2011-04-05 The Boeing Company Method and apparatus for simultaneous live television and data services using single beam antennas
US20070027589A1 (en) * 2001-02-13 2007-02-01 Brinkley Roger R Methods and apparatus for wirelss upload and download of aircraft data
US7970410B2 (en) 2001-02-13 2011-06-28 The Boeing Company Method and apparatus for remote initiation of ARINC 615 downloads
US20050026609A1 (en) * 2001-02-13 2005-02-03 Brinkley Roger R. Methods and apparatus for wireless upload and download of aircraft data
US20050197748A1 (en) * 2001-02-13 2005-09-08 William Holst Vehicle data services
US7908042B2 (en) 2001-02-13 2011-03-15 The Boeing Company Methods and apparatus for wireless upload and download of aircraft data
US7356389B2 (en) 2001-02-13 2008-04-08 William Holst Vehicle data services
US20030182404A1 (en) * 2002-03-25 2003-09-25 Jean-Francois Saint-Etienne Installation, gateway and process for downloading information between equipment onboard an aircraft and offboard loading means
US6885921B1 (en) * 2002-05-09 2005-04-26 Grace H. Farmer Method and apparatus for managing aircraft maintenance records
US20070243867A1 (en) * 2002-08-20 2007-10-18 Arinc Incorporated Acars messages over iridium
US7904082B2 (en) 2002-08-20 2011-03-08 Arinc Incorporated ACARS messages over iridium
US20040162067A1 (en) * 2002-08-20 2004-08-19 Arinc Inc. Security messenger system
US7904081B2 (en) * 2002-08-20 2011-03-08 Arinc Incorporated ACARS messages over iridium
US7398057B2 (en) * 2002-08-20 2008-07-08 Arinc Inc. Security messenger system
US20090009363A1 (en) * 2002-10-18 2009-01-08 Garmin International Inc. Methods, data structures, and systems to configure avionic equipment with profile data
US7386374B1 (en) * 2002-10-18 2008-06-10 Garmin International, Inc. Methods, data structures, and systems to configure avionic equipment with profile data
US8723692B2 (en) 2002-11-21 2014-05-13 Systems And Software Enterprises, Llc Secure terminal data loader apparatus and method for a mobile platform
US20050129239A1 (en) * 2002-11-21 2005-06-16 Farley Rodney J. Secure terminal data loader apparatus and method for a mobile platform
US8126147B2 (en) 2002-11-21 2012-02-28 Systems And Software Enterprises, Inc. Secure terminal data loader system and in-flight entertainment management system
US7580528B2 (en) * 2002-11-21 2009-08-25 Systems And Software Enterprises, Inc. Secure terminal data loader apparatus and method for a mobile platform
US20100008503A1 (en) * 2002-11-21 2010-01-14 Rodney Farley Secure Terminal Data Loader Apparatus and Method for a Mobile Platform
EP1426870A2 (en) * 2002-12-02 2004-06-09 The Boeing Company Remote aircraft manufacturing, monitoring, maintenance and management system
US7636568B2 (en) 2002-12-02 2009-12-22 The Boeing Company Remote aircraft manufacturing, monitoring, maintenance and management system
EP1426870A3 (en) * 2002-12-02 2004-09-29 The Boeing Company Remote aircraft manufacturing, monitoring, maintenance and management system
US6801769B1 (en) 2003-03-12 2004-10-05 The Boeing Company Modular aircraft information network system and an associated method of packaging the same
US7466980B2 (en) * 2003-03-27 2008-12-16 Honeywell International Inc. In-flight communications system
US20060252422A1 (en) * 2003-03-27 2006-11-09 Kauffman Donald C In-flight communications system
US20070111725A1 (en) * 2003-03-27 2007-05-17 Honeywell International Inc. In-flight communications system
US7142854B1 (en) * 2003-03-27 2006-11-28 Honeywell International Inc. In-flight communications system
US20050039006A1 (en) * 2003-07-25 2005-02-17 Desi Stelling Method for controlling customer-implemented data updates
US7213268B2 (en) * 2003-07-25 2007-05-01 Aviation Communication And Surveillance Systems, Llc Method for controlling customer-implemented data updates
US7151985B2 (en) * 2003-08-13 2006-12-19 Airbus Deutschland Gmbh System and method for exchanging programs in aircraft computers
US20050065670A1 (en) * 2003-08-13 2005-03-24 Helmut Tripmaker System and method for exchanging programs in aircraft computers
EP1517236A2 (en) * 2003-08-13 2005-03-23 Airbus Deutschland GmbH System and method for exchanging programs in aircraft computers
EP1517236A3 (en) * 2003-08-13 2005-09-28 Airbus Deutschland GmbH System and method for exchanging programs in aircraft computers
US6967830B2 (en) 2003-08-26 2005-11-22 The Boeing Company Expansion module and network for avionic devices
US20050047065A1 (en) * 2003-08-26 2005-03-03 The Boeing Company Expansion module and network for avionic devices
US20050262192A1 (en) * 2003-08-27 2005-11-24 Ascential Software Corporation Service oriented architecture for a transformation function in a data integration platform
US8307109B2 (en) 2003-08-27 2012-11-06 International Business Machines Corporation Methods and systems for real time integration services
US20050262191A1 (en) * 2003-08-27 2005-11-24 Ascential Software Corporation Service oriented architecture for a loading function in a data integration platform
US20050086360A1 (en) * 2003-08-27 2005-04-21 Ascential Software Corporation Methods and systems for real time integration services
US8060553B2 (en) 2003-08-27 2011-11-15 International Business Machines Corporation Service oriented architecture for a transformation function in a data integration platform
US8041760B2 (en) * 2003-08-27 2011-10-18 International Business Machines Corporation Service oriented architecture for a loading function in a data integration platform
US7257469B1 (en) * 2003-11-25 2007-08-14 Garmin International, Inc. Delivering data updates to an avionics device
US7149612B2 (en) 2004-01-05 2006-12-12 Arinc Incorporated System and method for monitoring and reporting aircraft quick access recorder data
US20050149238A1 (en) * 2004-01-05 2005-07-07 Arinc Inc. System and method for monitoring and reporting aircraft quick access recorder data
US20050197848A1 (en) * 2004-03-08 2005-09-08 Chou Y. H. Airport customer support dispatch system and method for operation for the same
WO2005086905A3 (en) * 2004-03-08 2007-03-01 Y Hong Chou Airport customer support dispatch system and method of operation for the same
US20050228559A1 (en) * 2004-04-12 2005-10-13 Laurent Bloch PCMCIA card for remotely communicating and interfacing with aircraft condition monitoring systems
WO2005101283A3 (en) * 2004-04-12 2007-07-12 Stephane Larose Method and system for remotely communicating and interfacing with aircraft condition monitoring systems
US20050228558A1 (en) * 2004-04-12 2005-10-13 Patrick Valette Method and system for remotely communicating and interfacing with aircraft condition monitoring systems
EP2551641A1 (en) * 2004-04-12 2013-01-30 Sagem Avionics, Inc. Method and system for remotely communicating and interfacing with aircraft condition monitoring systems
US7103456B2 (en) * 2004-04-12 2006-09-05 Sagem Avionics, Inc. PCMCIA card for remotely communicating and interfacing with aircraft condition monitoring systems
US7489992B2 (en) 2004-04-12 2009-02-10 Sagem Avionics, Inc. Method and system for remotely communicating and interfacing with aircraft condition monitoring systems
WO2005101284A3 (en) * 2004-04-12 2006-04-20 Sagem Avionics Inc A pcmcia card for remotely communicating and interfacing with aircraft condition monitoring systems
US7487029B2 (en) 2004-05-21 2009-02-03 Pratt & Whitney Canada Method of monitoring gas turbine engine operation
US20090229272A1 (en) * 2004-05-21 2009-09-17 Mark Edward Feeney Method of monitoring gas turbine engine operation
US8594903B2 (en) 2004-05-21 2013-11-26 Pratt & Whitney Canada Corp. Method of monitoring gas turbine engine operation
US20050261820A1 (en) * 2004-05-21 2005-11-24 Feeney Mark E Method of monitoring gas turbine engine operation
WO2005121722A1 (en) * 2004-06-04 2005-12-22 Texas Research International, Inc. Distributed mode system for real tme acoustic emission monitoring
US7080555B2 (en) * 2004-06-04 2006-07-25 Texas Research International, Inc. Distributed mode system for real time acoustic emission monitoring
US20060032313A1 (en) * 2004-06-04 2006-02-16 Austin Russell K Distributed mode system for real time acoustic emission monitoring
US20050288831A1 (en) * 2004-06-23 2005-12-29 Lusardi Robert A User-configurable electronic flight bag
US7769501B2 (en) * 2004-06-23 2010-08-03 The Boeing Company User-configurable electronic flight bag
US7437220B2 (en) 2004-08-17 2008-10-14 Arinc, Inc. Systems and methods for crew interaction and coordination using portable electronic data storage and display devices
US20060041340A1 (en) * 2004-08-17 2006-02-23 Arinc Inc. Systems and methods for crew interaction and coordination using portable electronic data storage and display devices
US9576404B2 (en) 2004-09-16 2017-02-21 Harris Corporation System and method of transmitting data from an aircraft
US9191053B2 (en) 2004-09-16 2015-11-17 Harris Corporation System and method of transmitting data from an aircraft
US8744372B2 (en) * 2004-09-16 2014-06-03 Harris Corporation System and method of transmitting data from an aircraft
US20080039076A1 (en) * 2004-09-16 2008-02-14 Harris Corporation System and method of transmitting data from an aircraft
US8244412B2 (en) * 2005-02-25 2012-08-14 The Boeing Company System and methods for on-board pre-flight aircraft dispatching
US20100036547A1 (en) * 2005-02-25 2010-02-11 The Boeing Company System and methods for on-board pre-flight aircraft dispatching
US20060229772A1 (en) * 2005-04-08 2006-10-12 Honeywell International Inc. Systems and methods for avionics software delivery
US20060229070A1 (en) * 2005-04-08 2006-10-12 The Boeing Company Soft handoff method and apparatus for mobile vehicles using directional antennas
US8280309B2 (en) 2005-04-08 2012-10-02 The Boeing Company Soft handoff method and apparatus for mobile vehicles using directional antennas
US9306657B2 (en) 2005-04-08 2016-04-05 The Boeing Company Soft handoff method and apparatus for mobile vehicles using directional antennas
US20060229103A1 (en) * 2005-04-08 2006-10-12 The Boeing Company Point-to-multipoint communications system and method
US7636552B2 (en) 2005-04-08 2009-12-22 The Boeing Company Point-to-multipoint communications system and method
US20060229077A1 (en) * 2005-04-08 2006-10-12 The Boeing Company Soft handoff method and apparatus for mobile vehicles using directional antennas
US7256749B2 (en) 2005-05-17 2007-08-14 The Boeing Company Compact, mechanically scanned cassegrain antenna system and method
WO2006124277A3 (en) * 2005-05-17 2007-11-01 Universal Electronics Inc System and method for providing content, management, and interactivity for client devices
US20060262022A1 (en) * 2005-05-17 2006-11-23 Desargant Glen J Compact, mechanically scanned cassegrain antenna system and method
US20070010236A1 (en) * 2005-07-07 2007-01-11 David Allen Mobile platform distributed data load management system
US7260389B2 (en) * 2005-07-07 2007-08-21 The Boeing Company Mobile platform distributed data load management system
US20070055416A1 (en) * 2005-07-13 2007-03-08 Allen David L Integrating portable electronic devices with electronic flight bag systems installed in aircraft
US8732233B2 (en) 2005-07-13 2014-05-20 The Boeing Company Integrating portable electronic devices with electronic flight bag systems installed in aircraft
US20070016344A1 (en) * 2005-07-15 2007-01-18 Arinc, Incorporated Systems and methods for voice communications and control using adapted portable data storage and display devices
US7827400B2 (en) 2005-07-28 2010-11-02 The Boeing Company Security certificate management
US7788002B2 (en) 2005-08-08 2010-08-31 The Boeing Company Fault data management
US20070033277A1 (en) * 2005-08-08 2007-02-08 Yukawa Steven J Fault data management
US20070042708A1 (en) * 2005-08-16 2007-02-22 Arinc Inc. Systems and methods for voice and data communication
US20070042727A1 (en) * 2005-08-16 2007-02-22 Arinc Inc. Systems and methods for voice and data communication
US8255112B2 (en) 2005-10-28 2012-08-28 The Boeing Company Remote aircraft maintenance in a networked environment
US20070115938A1 (en) * 2005-10-28 2007-05-24 The Boeing Company Remote aircraft maintenance in a networked environment
WO2007050164A1 (en) 2005-10-28 2007-05-03 The Boeing Company Remote aircraft maintenance in a networked environment
WO2007059333A2 (en) 2005-11-16 2007-05-24 The Boeing Company Integrated maintenance and materials service for fleet aircraft and system for determining pricing thereof
US20070124222A1 (en) * 2005-11-16 2007-05-31 Avery Robert L Integrated materials management for commercial aircraft fleets including access to real-time on-board systems information
US8423430B2 (en) 2005-11-16 2013-04-16 The Boeing Company Integrated materials management for commercial aircraft fleets including access to real-time on-board systems information
US20070127460A1 (en) * 2005-12-02 2007-06-07 The Boeing Company Scalable On-Board Open Data Network Architecture
US7840770B2 (en) 2005-12-02 2010-11-23 The Boeing Company Methods and systems for managing computer system configuration data
US20070130437A1 (en) * 2005-12-02 2007-06-07 Larson Craig A Methods and systems for managing computer system configuration data
WO2007064655A1 (en) * 2005-12-02 2007-06-07 The Boeing Company Scalable on-board open data network architecture
WO2007067279A3 (en) * 2005-12-02 2007-07-26 Boeing Co Methods and systems for staging configuration data for aircraft computers
US20070183435A1 (en) * 2005-12-02 2007-08-09 Kettering Christopher B Methods and apparatus providing an airborne e-enabled architecture as a system of systems
US7756145B2 (en) 2005-12-02 2010-07-13 The Boeing Company Methods and apparatus providing an airborne e-enabled architecture as a system of systems
US8341298B2 (en) 2005-12-02 2012-12-25 The Boeing Company Scalable on-board open data network architecture
US20070150124A1 (en) * 2005-12-22 2007-06-28 Patrick Wipplinger Methods and systems for displaying enroute moving maps
US8271150B2 (en) * 2005-12-22 2012-09-18 The Boeing Company Methods and systems for displaying enroute moving maps
US8423009B2 (en) * 2006-05-12 2013-04-16 The Boeing Company Automated delivery of flight data to aircraft cockpit devices
US20070264953A1 (en) * 2006-05-12 2007-11-15 Thiru Srinivasan Automated delivery of flight data to aircraft cockpit devices
US20080117858A1 (en) * 2006-11-21 2008-05-22 Honeywell International Inc. System and method for transmitting information using aircraft as transmission relays
US8509140B2 (en) 2006-11-21 2013-08-13 Honeywell International Inc. System and method for transmitting information using aircraft as transmission relays
US20080154442A1 (en) * 2006-12-21 2008-06-26 Patrick Ralf Wipplinger Methods and systems for displaying electronic enroute maps
US7756637B2 (en) * 2006-12-21 2010-07-13 The Boeing Company Methods and systems for displaying electronic enroute maps
US8645148B2 (en) 2006-12-29 2014-02-04 The Boeing Company Methods and apparatus providing an E-enabled ground architecture
US20080162155A1 (en) * 2006-12-29 2008-07-03 Gregory John Small Methods and apparatus providing an e-enabled ground architecture
US20080235626A1 (en) * 2007-03-22 2008-09-25 Arinc Incorporated Electronic paper device for use by aircraft and railway passengers
US20080235634A1 (en) * 2007-03-22 2008-09-25 Arinc Incorporated Electronic paper device for use by aircraft pilots and crew
US9367971B2 (en) 2007-04-06 2016-06-14 Airbus Aircraft maintenance method and device
JP2010524750A (en) * 2007-04-06 2010-07-22 エアバス Communication system between a computer network and ground of a computer network in an aircraft
WO2008139060A2 (en) * 2007-04-06 2008-11-20 Airbus System enabling communication between an aircraft-based computer network and a ground-based computer network
FR2914803A1 (en) * 2007-04-06 2008-10-10 Airbus Sas Method and maintenance device in an aircraft
JP2010523387A (en) * 2007-04-06 2010-07-15 エアバス The method and apparatus of the aircraft maintenance
RU2475990C2 (en) * 2007-04-06 2013-02-20 Эрбюс Method and device of service in aircraft
JP2014028614A (en) * 2007-04-06 2014-02-13 Airbus Aircraft maintenance method and device
US20100131149A1 (en) * 2007-04-06 2010-05-27 Airbus Aircraft maintenance method and device
WO2008139060A3 (en) * 2007-04-06 2009-02-05 Airbus System enabling communication between an aircraft-based computer network and a ground-based computer network
US20100121938A1 (en) * 2007-04-06 2010-05-13 Frederic Saugnac System enabling communication between an aircraft-based computer network and a ground-based computer network
WO2008139061A1 (en) 2007-04-06 2008-11-20 Airbus Aircraft maintenance method and device
US8856277B2 (en) 2007-04-06 2014-10-07 Airbus System enabling communication between an aircraft-based computer network and a ground-based computer network
FR2914804A1 (en) * 2007-04-06 2008-10-10 Airbus Sas System of communication between a network of computers in an aircraft and a network of computers to the ground
US8160757B1 (en) * 2007-05-18 2012-04-17 Rockwell Collins, Inc. System and method for providing optimum multi-map overlay in a flight deck navigation display
US8200376B2 (en) * 2007-07-30 2012-06-12 Symvionics, Inc. Vehicle performance monitoring system with multi-level caching
US20090037034A1 (en) * 2007-07-30 2009-02-05 Patrick Mattingly Vehicle performance monitoring system with multi-level caching
US7729263B2 (en) 2007-08-08 2010-06-01 Honeywell International Inc. Aircraft data link network routing
US20100232295A1 (en) * 2007-08-08 2010-09-16 Honeywell International Inc. Aircraft data link network routing
US8107412B2 (en) * 2007-08-08 2012-01-31 Honeywell International Inc. Gatelink startup controlled by ACARS CMU
US20090040963A1 (en) * 2007-08-08 2009-02-12 Honeywell International Inc. Gatelink startup controlled by acars cmu
US20090041041A1 (en) * 2007-08-08 2009-02-12 Honeywell International Inc. Aircraft data link network routing
US8284674B2 (en) 2007-08-08 2012-10-09 Honeywell International Inc. Aircraft data link network routing
US7835734B2 (en) 2007-09-20 2010-11-16 Honeywell International Inc. System and method for wireless routing of data from an aircraft
US20090082013A1 (en) * 2007-09-20 2009-03-26 Honeywell International Inc. System and method for wireless routing of data from an aircraft
US8811265B2 (en) 2007-10-19 2014-08-19 Honeywell International Inc. Ad-hoc secure communication networking based on formation flight technology
US9264126B2 (en) 2007-10-19 2016-02-16 Honeywell International Inc. Method to establish and maintain an aircraft ad-hoc communication network
US20090103452A1 (en) * 2007-10-19 2009-04-23 Honeywell International Inc. Ad-hoc secure communication networking based on formation flight technology
US20090103473A1 (en) * 2007-10-19 2009-04-23 Honeywell International Inc. Method to establish and maintain an aircraft ad-hoc communication network
US9038047B2 (en) 2007-11-27 2015-05-19 The Boeing Company Aircraft software part library
US20090138385A1 (en) * 2007-11-27 2009-05-28 The Boeing Company Crate Tool
US20090138873A1 (en) * 2007-11-27 2009-05-28 The Boeing Company Method and Apparatus for Loadable Aircraft Software Parts Distribution
US8442751B2 (en) 2007-11-27 2013-05-14 The Boeing Company Onboard electronic distribution system
US8185609B2 (en) 2007-11-27 2012-05-22 The Boeing Company Method and apparatus for processing commands in an aircraft network
US20090138516A1 (en) * 2007-11-27 2009-05-28 The Boeing Company Aircraft software part library
US9208308B2 (en) 2007-11-27 2015-12-08 The Boeing Company Alternate parts signature list file
US20090138518A1 (en) * 2007-11-27 2009-05-28 The Boeing Company Proxy Server for Distributing Aircraft Software Parts
US9225765B2 (en) 2007-11-27 2015-12-29 The Boeing Company Onboard electronic distribution system
US8165930B2 (en) 2007-11-27 2012-04-24 The Boeing Company Crate tool
US8490074B2 (en) 2007-11-27 2013-07-16 The Boeing Company Aircraft software part library
US20090138874A1 (en) * 2007-11-27 2009-05-28 The Boeing Company Software Maintenance Tool
US20090138872A1 (en) * 2007-11-27 2009-05-28 The Boeing Company Method and Apparatus for Processing Commands in an Aircraft Network
US9807149B2 (en) 2007-11-27 2017-10-31 The Boeing Company Method and apparatus for loadable aircraft software parts distribution
US20090138871A1 (en) * 2007-11-27 2009-05-28 The Boeing Company Onboard Electronic Distribution System
US20090138517A1 (en) * 2007-11-27 2009-05-28 The Boeing Company Alternate Parts Signature List File
US8930310B2 (en) 2007-11-27 2015-01-06 The Boeing Company Proxy server for distributing aircraft software parts
US20090141669A1 (en) * 2007-12-04 2009-06-04 Honeywell International Inc. Travel characteristics-based ad-hoc communication network algorithm selection
US8570990B2 (en) 2007-12-04 2013-10-29 Honeywell International Inc. Travel characteristics-based ad-hoc communication network algorithm selection
US20090192659A1 (en) * 2008-01-30 2009-07-30 Beebe Clifford A Aircraft maintenance laptop
WO2009097554A1 (en) * 2008-01-30 2009-08-06 The Boeing Company Aircraft maintenance laptop
US8321083B2 (en) 2008-01-30 2012-11-27 The Boeing Company Aircraft maintenance laptop
FR2927210A1 (en) * 2008-02-01 2009-08-07 Airbus France Sas A suitable switching switch has a wireless network to a maintenance configuration has commercial aircraft configuration and vice versa.
US7907545B2 (en) 2008-02-01 2011-03-15 Airbus France Switching device adapted to switch an aircraft wireless network from a maintenance configuration to a commercial configuration and vice-versa
US20090196201A1 (en) * 2008-02-01 2009-08-06 Airbus France Switching device adapted to switch an aircraft wireless network from a maintenance configuration to a commercial configuration and vice-versa
US9467221B2 (en) 2008-02-04 2016-10-11 Honeywell International Inc. Use of alternate communication networks to complement an ad-hoc mobile node to mobile node communication network
US20090197595A1 (en) * 2008-02-04 2009-08-06 Honeywell International Inc. Use of alternate communication networks to complement an ad-hoc mobile node to mobile node communication network
US20090318138A1 (en) * 2008-06-20 2009-12-24 Honeywell International Inc. System and method for in-flight wireless communication
US8190147B2 (en) 2008-06-20 2012-05-29 Honeywell International Inc. Internetworking air-to-air network and wireless network
US20090318137A1 (en) * 2008-06-20 2009-12-24 Honeywell International Inc. Internetworking air-to-air network and wireless network
US8228911B2 (en) 2008-09-19 2012-07-24 Honeywell International Inc. Enhanced data link communication over iridium
US9019960B2 (en) 2008-09-19 2015-04-28 Honeywell International Inc. Enhanced data link communication over iridium
US8554204B2 (en) 2008-09-23 2013-10-08 Honeywell International Inc. Communication management unit server capability
US20100075614A1 (en) * 2008-09-23 2010-03-25 Honeywell International Inc. Communication management unit server capability
US8515658B1 (en) * 2009-07-06 2013-08-20 The Boeing Company Managing navigational chart presentation
US20110040595A1 (en) * 2009-08-12 2011-02-17 Chou Y Hong Real-time service management and dispatch system
US20110185207A1 (en) * 2010-01-25 2011-07-28 Honeywell International Inc. Pcmcia memory card with ethernet/wireless connectivity and battery backup for avionics applications
US8539217B2 (en) * 2010-01-25 2013-09-17 Honeywell International Inc. Method and system to facilitate data transfer to a device
US20110252295A1 (en) * 2010-04-09 2011-10-13 Beacham William H Avionic data validation system
US20130232237A1 (en) * 2012-03-01 2013-09-05 Honeywell International Inc. Programmable portable electronic device for airborne operational communications
US9571181B2 (en) * 2012-03-01 2017-02-14 Honeywell International Inc. Programmable portable electronic device for airborne operational communications
CN103312408A (en) * 2012-03-01 2013-09-18 霍尼韦尔国际公司 Programmable portable electronic device for airborne operational communications
US20160036513A1 (en) * 2013-04-22 2016-02-04 Chad Klippert Aircraft flight data monitoring and reporting system and use thereof
US20140316613A1 (en) * 2013-04-23 2014-10-23 The Boeing Company Aircraft Performance Monitoring System
US9061756B2 (en) * 2013-04-23 2015-06-23 The Boeing Company Aircraft performance monitoring system
US9160543B2 (en) 2013-05-07 2015-10-13 The Boeing Company Verification of aircraft information in response to compromised digital certificate
US9237022B2 (en) 2013-05-07 2016-01-12 The Boeing Company Use of multiple digital signatures and quorum rules to verify aircraft information
US9563580B2 (en) 2013-07-25 2017-02-07 North Flight Data Systems, LLC System, methodology, and process for wireless transmission of sensor data onboard an aircraft to a portable electronic device
US9826039B2 (en) 2014-02-04 2017-11-21 Honeywell International Inc. Configurable communication systems and methods for communication
US20160016671A1 (en) * 2014-07-18 2016-01-21 Thales Processing of aircraft alarm and maintenance messages
US9663242B2 (en) * 2014-07-18 2017-05-30 Thales Processing of aircraft alarm and maintenance messages
US20160197857A1 (en) * 2015-01-06 2016-07-07 The Boeing Company Aircraft control domain communication framework

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