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公开(公告)号：US20170331895A1
公开(公告)日：2017-11-16
申请号：US15153877
申请日：2016-05-13
Applicant: Honeywell International Inc.
Inventor： Harisha Bangalore Manjunath
CPC classification number: H04L67/12 , H04L12/40 , H04L41/0213 , H04L67/42 , H04L2012/4028
Abstract: An aircraft data interface function (ADIF) server system comprises a processing module that hosts an aircraft condition monitoring function, comprising an airline modifiable information database including a history buffer and one or more logic units; a management information base (MIB) database; a parameter snapshot database; and a simple network management protocol (SNMP) agent in communication with the MIB database and parameter snapshot database. A core network unit communicates with the SNMP agent and an SNMP manager in an ADIF client. The SNMP agent sends messages to and receives messages from the SNMP manager through the core network unit. The ADIF server system interfaces with one or more avionics systems through a common data network to obtain and store aircraft parameter information. The ADIF client is configured via the core network unit to interact with the ADIF server system to request and receive the aircraft parameter information.
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2.发明申请公开(公告)号：US20220392358A1
公开(公告)日：2022-12-08
申请号：US17443288
申请日：2021-07-23
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： Harisha Bangalore Manjunath , Rushoth Kumar M C , Venu Puttam , Murali Kadeppagari , Prashant Hegde , Chandana Venigalla , Supratik Gon , Brad H. Miller , Gary Ostrom , Ricardo Darif Bortolini , Dhivagar Palanisamy , David Kolbet , John Vo
Abstract: A system and method for implementing an autonomous distress tracking (ADT) triggering function is provided. The method comprises receiving a configuration file containing a plurality of user configurable parameters from a ground-based system, configuring an aircraft condition and monitoring function (ACMF) engine to apply trigger logic specified by the plurality of user configurable parameters to aircraft sensor and/or system data and monitoring for a plurality of distress conditions specified by the plurality of user configurable parameters; executing the configured ACMF engine to detect the occurrence of a distress condition; automatically generating a data message when a distress condition occurrence has been detected wherein the data message can include aircraft position data specified in the user configurable parameters, the aircraft sensor and/or system data on which the detection of the one or more trigger conditions was based, and the identity of the detected distress condition; and automatically sending the data message to a transmission system onboard the aircraft that is configured to transmit a search and rescue signal.
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公开(公告)号：US10554755B2
公开(公告)日：2020-02-04
申请号：US15153877
申请日：2016-05-13
Applicant: Honeywell International Inc.
Inventor： Harisha Bangalore Manjunath
IPC: G06F15/173 , H04L29/08 , H04L12/40 , H04L12/24 , H04L29/06
Abstract: An aircraft data interface function (ADIF) server system comprises a processing module that hosts an aircraft condition monitoring function, comprising an airline modifiable information database including a history buffer and one or more logic units; a management information base (MIB) database; a parameter snapshot database; and a simple network management protocol (SNMP) agent in communication with the MIB database and parameter snapshot database. A core network unit communicates with the SNMP agent and an SNMP manager in an ADIF client. The SNMP agent sends messages to and receives messages from the SNMP manager through the core network unit. The ADIF server system interfaces with one or more avionics systems through a common data network to obtain and store aircraft parameter information. The ADIF client is configured via the core network unit to interact with the ADIF server system to request and receive the aircraft parameter information.
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