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公开(公告)号：US20230222702A1
公开(公告)日：2023-07-13
申请号：US17572982
申请日：2022-01-11
Applicant: Raytheon Technologies Corporation
Inventor： Creig M. Cavanaugh , Paul Raymond Scheid
IPC: G06T11/00 , H04L43/0894
CPC classification number: G06T11/00 , H04L43/0894 , B64F1/36
Abstract: A system includes a memory system configured to store a plurality of instructions to provide aircraft communication visualization and a processing system. The processing system configured to execute the instructions to result in retrieving a plurality of status data associated with aircraft communication at a target location from a database, determining a plurality of geographic location information for a plurality of aircraft parking locations at the target location, accessing a plurality of imagery data associated with a view at the target location, and generating an aircraft communication visualization map for the target location. The aircraft communication visualization map includes aircraft communication information overlaid upon an image based on the imagery data and the aircraft parking locations at the target location.
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公开(公告)号：US11615653B2
公开(公告)日：2023-03-28
申请号：US17208248
申请日：2021-03-22
Applicant: Raytheon Technologies Corporation
Inventor： Paul Raymond Scheid , Jason E. Posniak , William C. Lamberti
IPC: H04L67/125 , H04L67/00 , H04L12/40 , G07C5/00 , H04L12/417 , H04L12/66
Abstract: A system includes an engine control configured to control a gas turbine engine and a means for wirelessly communicating with an offboard system and communicating with the engine control by establishing communication with the engine control on a first communication bus using system credential authentication, establishing communication between the engine control and a data storage system on a second communication bus, establishing wireless communication with the offboard system using system credential authentication, and providing access from the offboard system to the engine control and from the engine control to the data storage system to enable one or more updates of the data storage system by the offboard system based on service credential authentication.
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公开(公告)号：US11743338B2
公开(公告)日：2023-08-29
申请号：US17888976
申请日：2022-08-16
Applicant: Raytheon Technologies Corporation
Inventor： William C. Lamberti , Paul Raymond Scheid , Jason E. Posniak
CPC classification number: H04L67/125 , F01D21/003 , F02C9/00 , G07C5/008 , G07C5/0808 , G07C5/0841 , H04B7/18506 , F05D2220/323 , F05D2260/80 , F05D2270/80 , G07C5/006 , H04L2012/4028
Abstract: A method of operating a communication adapter of a gas turbine engine of an aircraft includes receiving a plurality of time series data at the communication adapter from an engine control of the gas turbine engine. The method also includes recording a plurality of internal sensor data of an internal sensor system of the communication adapter. The method further includes correlating the time series data with the internal sensor data based on an alignment in time to form an enhanced data set and transmitting the enhanced data set from the communication adapter to an offboard system.
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公开(公告)号：US20220349353A1
公开(公告)日：2022-11-03
申请号：US17245452
申请日：2021-04-30
Applicant: Raytheon Technologies Corporation
Inventor： Paul Raymond Scheid , Jason E. Posniak
IPC: F02C9/00
Abstract: Examples described herein provide a method for assigning tasks to processors of a multi-core processor associated with a gas turbine engine. The method includes assigning a first processing core of the multi-core processor to perform a first type of tasks having a first safety level. The method further includes assigning a second processing core of the multi-core processor to perform a second type of tasks having a second safety level, the second safety level being different than the first safety level. The method further includes executing a first core task of the first type of tasks on the first processing core. The method further includes executing a second core task of the second type of tasks on the second processing core.
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公开(公告)号：US20230362255A1
公开(公告)日：2023-11-09
申请号：US18353921
申请日：2023-07-18
Applicant: Raytheon Technologies Corporation
Inventor： William C. Lamberti , Paul Raymond Scheid , Jason E. Posniak
CPC classification number: H04L67/125 , F01D21/003 , F02C9/00 , G07C5/008 , G07C5/0808 , G07C5/0841 , H04B7/18506 , F05D2220/323 , F05D2260/80 , F05D2270/80 , G07C5/006 , H04L2012/4028
Abstract: A communication adapter of a gas turbine engine of an aircraft includes an internal sensor system including a plurality of sensors within the communication adapter, a memory system, and processing circuitry. The processing circuitry is configured to receive a plurality of time series data at the communication adapter from an engine control of the gas turbine engine, record a plurality of internal sensor data of the internal sensor system, correlate the time series data with the internal sensor data based on an alignment in time to form an enhanced data set, and transmit the enhanced data set from the communication adapter to an offboard system.
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Patent Agency Ranking
公开(公告)号：US11746708B2
公开(公告)日：2023-09-05
申请号：US17940288
申请日：2022-09-08
Applicant: Raytheon Technologies Corporation
Inventor： William C. Lamberti , Paul Raymond Scheid , Jason E. Posniak
CPC classification number: F02C9/00 , G06F8/65 , H04W12/06 , F05D2270/44 , F05D2270/54
Abstract: A communication adapter of a gas turbine engine of an aircraft includes a communication interface configured to wirelessly communicate with an offboard system and to communicate with an engine control of the gas turbine engine. The communication adapter also includes a memory system and processing circuitry configured to receive one or more configuration items from the offboard system, confirm an authentication between the communication adapter and the engine control, apply a cryptographic algorithm using one or more parameters received and cryptographic information to decrypt the one or more configuration items, wherein the cryptographic information includes a combination of received cryptographic information and previously stored cryptographic information, and transfer the one or more configuration items to the engine control based on the authentication.
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公开(公告)号：US20230064394A1
公开(公告)日：2023-03-02
申请号：US17972861
申请日：2022-10-25
Applicant: Raytheon Technologies Corporation
Inventor： Paul Raymond Scheid
IPC: G06F16/2457 , G06F16/9535 , G06Q10/06
Abstract: A data request workflow system comprises vehicle operational data. A file delivery request comprises a data request for a subset of the vehicle operational data. A file processing system receives the vehicle operational data and includes at least one set of predefined file editing rules. The file processing system automatically applies at least one set of predefined file editing rules to filter out a predefined sub-set of the vehicle operational data and to automatically edit data that is part of the data request per predefined criteria for each type of vehicle operational data to provide a converted data file to be transmitted to a user that submitted the file delivery request.
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公开(公告)号：US11975863B2
公开(公告)日：2024-05-07
申请号：US17245425
申请日：2021-04-30
Applicant: Raytheon Technologies Corporation
Inventor： Paul Raymond Scheid , Jason E. Posniak
CPC classification number: B64D45/00 , B64D43/00 , G08G5/0013 , G08G5/003 , B64D2045/0085
Abstract: Examples described herein provide a method that includes receiving engine data from a sensor associated with the engine. The method further includes associating a header with the engine data to generate packaged engine data. The method further includes transmitting the packaged engine data to an aircraft communication unit, wherein the header provides for the aircraft communication unit to transmit the packaged engine data to a ground station communication unit via a communication protocol.
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公开(公告)号：US20230120679A1
公开(公告)日：2023-04-20
申请号：US18081941
申请日：2022-12-15
Applicant: Raytheon Technologies Corporation
Inventor： William C. Lamberti , Paul Raymond Scheid , Jason E. Posniak
Abstract: A gas turbine engine of an aircraft includes an engine control configured to monitor and control operation of the gas turbine engine in real-time and a communication adapter that includes a housing and a plurality of antennas in the housing. The communication adapter is configured to establish communication with the engine control and wireless communication with an offboard system external to the aircraft through at least one of the antennas of the communication adapter. The housing includes a metal chassis with a non-conductive substrate between the metal chassis and the antennas. The antennas are partitioned into two or more portions. A communication interface of the communication adapter is configured to establish wireless communication through the antennas using two or more different wireless communication protocols.
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公开(公告)号：US20230003173A1
公开(公告)日：2023-01-05
申请号：US17940288
申请日：2022-09-08
Applicant: Raytheon Technologies Corporation
Inventor： William C. Lamberti , Paul Raymond Scheid , Jason E. Posniak
Abstract: A communication adapter of a gas turbine engine of an aircraft includes a communication interface configured to wirelessly communicate with an offboard system and to communicate with an engine control of the gas turbine engine. The communication adapter also includes a memory system and processing circuitry configured to receive one or more configuration items from the offboard system, confirm an authentication between the communication adapter and the engine control, apply a cryptographic algorithm using one or more parameters received and cryptographic information to decrypt the one or more configuration items, wherein the cryptographic information includes a combination of received cryptographic information and previously stored cryptographic information, and transfer the one or more configuration items to the engine control based on the authentication.
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