Patents by Inventor Ali R. Mansouri
Ali R. Mansouri has filed for patents to protect the following inventions. This listing includes patent applications that are pending as well as patents that have already been granted by the United States Patent and Trademark Office (USPTO).
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Patent number: 9846199Abstract: A vehicle includes a body and at least one propulsion unit operatively coupled to the body. The vehicle also includes an electrical power system at least partially disposed within the body. The electrical power system includes a rechargeable battery and a health management unit operatively coupled to the rechargeable battery. The health management unit includes a state of health module configured to output information corresponding to battery health based on received battery-related data. The battery-related data includes data collected in real time operation of the rechargeable battery and battery relevant fault history of the vehicle.Type: GrantFiled: October 20, 2014Date of Patent: December 19, 2017Assignee: THE BOEING COMPANYInventors: John L. Vian, Ali R. Mansouri, Rangasamy Elangovan, Mori M. Borumand, Khaled Abdel-Motagaly
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Publication number: 20150100198Abstract: A vehicle includes a body and at least one propulsion unit operatively coupled to the body. The vehicle also includes an electrical power system at least partially disposed within the body. The electrical power system includes a rechargeable battery and a health management unit operatively coupled to the rechargeable battery. The health management unit includes a state of health module configured to output information corresponding to battery health based on received battery-related data. The battery-related data includes data collected in real time operation of the rechargeable battery and battery relevant fault history of the vehicle.Type: ApplicationFiled: October 20, 2014Publication date: April 9, 2015Applicant: The Boeing CompanyInventors: John L. Vian, Ali R. Mansouri, Rangasamy Elangovan, Mori M. Borumand, Khaled Abdel-Motagaly
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Patent number: 8890480Abstract: Systems and methods for health management of rechargeable batteries are disclosed. In one embodiment, a rechargeable battery system includes a rechargeable battery, and a battery health management unit operatively coupled to the rechargeable battery and including a state of health module configured to estimate a battery health by receiving battery-related data and predicting one or more failure modes. The state of health module may further include a prognostic failure mode component configured to combine at least one flight data variable with at least one model-based prognostic. In alternate embodiments, the battery health management unit may further include a state of life module and a state of charge module.Type: GrantFiled: November 30, 2006Date of Patent: November 18, 2014Assignee: The Boeing CompanyInventors: John L. Vian, Ali R. Mansouri, Rangasamy Elangovan, Mori M. Borumand, Khaled Abdel-Motagaly
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Patent number: 8849603Abstract: A method of testing a component of a mobile platform without using an aircraft control system of the mobile platform, where the component forms a part of the aircraft control system. The method may involve using a test controller independent of the aircraft control system to initiate a test operation. The test operation is used to generate a test signal. The test signal is applied to a test subsystem carried on the mobile platform but operable independent of the aircraft control system. The test subsystem is used to act on the component of the aircraft control system. A response of the component may then be evaluated.Type: GrantFiled: November 21, 2008Date of Patent: September 30, 2014Assignee: The Boeing CompanyInventors: Clete M. Boldrin, Ali R. Mansouri, John L. Vian
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Patent number: 8437904Abstract: Systems and methods for health monitoring of complex systems are disclosed. In one embodiment, a method includes receiving a plurality of signals indicative of observation states of plurality of operating variables, performing a combined probability analysis of the plurality of signals using a diagnostic model of a monitored system to provide a health prognosis of the monitored system, and providing an indication of the health prognosis of the monitored system. In some embodiments, the monitored system may be an onboard system of an aircraft.Type: GrantFiled: September 28, 2007Date of Patent: May 7, 2013Assignee: The Boeing CompanyInventors: Ali R. Mansouri, John L. Vian, Krzysztof Wojtek Przytula, David Allen
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Patent number: 8406936Abstract: A system and methods for life optimal power management of a distributed or centralized battery network system for use in aircraft functions and subsystems are disclosed. The method determines power priority of the subsystems, and selectively distributes power from the battery network system to the subsystems based on the power priority. Concurrently with distributing power, the method manages the energy in the battery network system. To determine whether the battery power is sufficient for aircraft functions, the method also computes and indicates the actual available energy left in the battery network systems. With this approach, the system and methods can provide a persistent power supply in the event an unexpected battery failure occurs, thereby enabling the aircraft to safely maintain flight operability despite a battery failure.Type: GrantFiled: August 1, 2011Date of Patent: March 26, 2013Assignee: The Boeing CompanyInventors: Mori M. Borumand, Ali R. Mansouri, John L. Vian
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Patent number: 8010250Abstract: A system and methods for life optimal power management of a distributed or centralized battery network system for use in aircraft functions and subsystems are disclosed. The method determines power priority of the subsystems, and selectively distributes power from the battery network system to the subsystems based on the power priority. Concurrently with distributing power, the method manages the energy in the battery network system. To determine whether the battery power is sufficient for aircraft functions, the method also computes and indicates the actual available energy left in the battery network systems. With this approach, the system and methods can provide a persistent power supply in the event an unexpected battery failure occurs, thereby enabling the aircraft to safely maintain flight operability despite a battery failure.Type: GrantFiled: June 5, 2007Date of Patent: August 30, 2011Assignee: The Boeing CompanyInventors: Mori M. Borumand, Ali R. Mansouri, John L. Vian
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Patent number: 7813888Abstract: Systems and methods for development testing of vehicles and components are disclosed. In one embodiment, a system includes a position reference system and a command and control architecture. The position reference system is configured to repetitively measure one or more position and motion characteristics of one or more vehicles operating within a control volume. The command and control architecture is configured to receive the repetitively measured characteristics from the position reference system, and to determine corresponding control signals based thereon. The control signals are then transmitted to the one or more vehicles to control at least one of position, movement, and stabilization of the one or more vehicles in a closed-loop feedback manner. The system may further include a health monitoring component configured to monitor health conditions of the one or more vehicles, the control signals being determined at least in part on the health conditions.Type: GrantFiled: July 24, 2006Date of Patent: October 12, 2010Assignee: The Boeing CompanyInventors: John L. Vian, Ronald C. Provine, Stefan R. Bieniawski, Emad W. Saad, Paul E. R. Pigg, Gregory J. Clark, Ali R. Mansouri, Khaled Abdel-Motagaly, Charles A. Erignac, James J. Troy, Paul Murray, Jonathan P. How, Mario J. Valenti, Brett M. Bethke
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Publication number: 20100131238Abstract: A method of testing a component of a mobile platform without using an aircraft control system of the mobile platform, where the component forms a part of the aircraft control system. The method may involve using a test controller independent of the aircraft control system to initiate a test operation. The test operation is used to generate a test signal. The test signal is applied to a test subsystem carried on the mobile platform but operable independent of the aircraft control system. The test subsystem is used to act on the component of the aircraft control system. A response of the component may then be evaluated.Type: ApplicationFiled: November 21, 2008Publication date: May 27, 2010Applicant: The Boeing CompanyInventors: Clete M. Boldrin, Ali R. Mansouri, John L Vian
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Publication number: 20100121587Abstract: Systems and methods for health management of rechargeable batteries are disclosed. In one embodiment, a rechargeable battery system includes a rechargeable battery, and a battery health management unit operatively coupled to the rechargeable battery and including a state of health module configured to estimate a battery health by receiving battery-related data and predicting one or more failure modes. The state of health module may further include a prognostic failure mode component configured to combine at least one flight data variable with at least one model-based prognostic. In alternate embodiments, the battery health management unit may further include a state of life module and a state of charge module.Type: ApplicationFiled: November 30, 2006Publication date: May 13, 2010Applicant: The Boeing CompanyInventors: John L. Vian, Ali R. Mansouri, Rangasamy Elangovan, Mori M. Borumand, Khaled Abdel-Motagaly
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Publication number: 20100057511Abstract: An apparatus for managing a fleet of vehicles. On each of the vehicles are a plurality of vehicle subsystems, each subsystem capable of monitoring conditions and assessing capabilities of the subsystem. For each vehicle, a vehicle management system has one or more processors and memory configured to: monitor conditions and assess capabilities of the vehicle based on subsystem condition and capability information provided by the subsystems, and based on the monitored vehicle conditions and assessed vehicle capabilities, initiate performance of one or more fleet management functions.Type: ApplicationFiled: March 2, 2009Publication date: March 4, 2010Inventors: Ali R. Mansouri, John L. Vian, John T. Peters
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Publication number: 20080312783Abstract: Systems and methods for health monitoring of complex systems are disclosed. In one embodiment, a method includes receiving a plurality of signals indicative of observation states of plurality of operating variables, performing a combined probability analysis of the plurality of signals using a diagnostic model of a monitored system to provide a health prognosis of the monitored system, and providing an indication of the health prognosis of the monitored system. In some embodiments, the monitored system may be an onboard system of an aircraft.Type: ApplicationFiled: September 28, 2007Publication date: December 18, 2008Applicant: THE BOEING COMPANYInventors: Ali R. Mansouri, John L. Vian, Krzysztof Wojtek Przytula, David Allen
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Publication number: 20080306637Abstract: A system and methods for life optimal power management of a distributed or centralized battery network system for use in aircraft functions and subsystems are disclosed. The method determines power priority of the subsystems, and selectively distributes power from the battery network system to the subsystems based on the power priority. Concurrently with distributing power, the method manages the energy in the battery network system. To determine whether the battery power is sufficient for aircraft functions, the method also computes and indicates the actual available energy left in the battery network systems. With this approach, the system and methods can provide a persistent power supply in the event an unexpected battery failure occurs, thereby enabling the aircraft to safely maintain flight operability despite a battery failure.Type: ApplicationFiled: June 5, 2007Publication date: December 11, 2008Inventors: Mori M. Borumand, Ali R. Mansouri, John L. Vian
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Publication number: 20080033684Abstract: Systems and methods for development testing of vehicles and components are disclosed. In one embodiment, a system includes a position reference system and a command and control architecture. The position reference system is configured to repetitively measure one or more position and motion characteristics of one or more vehicles operating within a control volume. The command and control architecture is configured to receive the repetitively measured characteristics from the position reference system, and to determine corresponding control signals based thereon. The control signals are then transmitted to the one or more vehicles to control at least one of position, movement, and stabilization of the one or more vehicles in a closed-loop feedback manner. The system may further include a health monitoring component configured to monitor health conditions of the one or more vehicles, the control signals being determined at least in part on the health conditions.Type: ApplicationFiled: July 24, 2006Publication date: February 7, 2008Applicant: THE BOEING COMPANYInventors: John L. Vian, Ronald C. Provine, Stefan R. Bieniawski, Emad W. Saad, Paul E. R. Pigg, Gregory J. Clark, Ali R. Mansouri, Khaled Abdel-Motagaly, Charles A. Erignac, James J. Troy, Paul Murray, Jonathan P. How, Mario J. Valenti, Brett M. Bethke