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).

  • Patent number: 9846199
    Abstract: 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: Grant
    Filed: October 20, 2014
    Date of Patent: December 19, 2017
    Assignee: THE BOEING COMPANY
    Inventors: John L. Vian, Ali R. Mansouri, Rangasamy Elangovan, Mori M. Borumand, Khaled Abdel-Motagaly
  • Publication number: 20150100198
    Abstract: 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: Application
    Filed: October 20, 2014
    Publication date: April 9, 2015
    Applicant: The Boeing Company
    Inventors: John L. Vian, Ali R. Mansouri, Rangasamy Elangovan, Mori M. Borumand, Khaled Abdel-Motagaly
  • Patent number: 8890480
    Abstract: 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: Grant
    Filed: November 30, 2006
    Date of Patent: November 18, 2014
    Assignee: The Boeing Company
    Inventors: John L. Vian, Ali R. Mansouri, Rangasamy Elangovan, Mori M. Borumand, Khaled Abdel-Motagaly
  • Patent number: 8849603
    Abstract: 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: Grant
    Filed: November 21, 2008
    Date of Patent: September 30, 2014
    Assignee: The Boeing Company
    Inventors: Clete M. Boldrin, Ali R. Mansouri, John L. Vian
  • Patent number: 8437904
    Abstract: 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: Grant
    Filed: September 28, 2007
    Date of Patent: May 7, 2013
    Assignee: The Boeing Company
    Inventors: Ali R. Mansouri, John L. Vian, Krzysztof Wojtek Przytula, David Allen
  • Patent number: 8406936
    Abstract: 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: Grant
    Filed: August 1, 2011
    Date of Patent: March 26, 2013
    Assignee: The Boeing Company
    Inventors: Mori M. Borumand, Ali R. Mansouri, John L. Vian
  • Patent number: 8010250
    Abstract: 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: Grant
    Filed: June 5, 2007
    Date of Patent: August 30, 2011
    Assignee: The Boeing Company
    Inventors: Mori M. Borumand, Ali R. Mansouri, John L. Vian
  • Patent number: 7813888
    Abstract: 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: Grant
    Filed: July 24, 2006
    Date of Patent: October 12, 2010
    Assignee: The Boeing Company
    Inventors: 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
  • Publication number: 20100131238
    Abstract: 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: Application
    Filed: November 21, 2008
    Publication date: May 27, 2010
    Applicant: The Boeing Company
    Inventors: Clete M. Boldrin, Ali R. Mansouri, John L Vian
  • Publication number: 20100121587
    Abstract: 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: Application
    Filed: November 30, 2006
    Publication date: May 13, 2010
    Applicant: The Boeing Company
    Inventors: John L. Vian, Ali R. Mansouri, Rangasamy Elangovan, Mori M. Borumand, Khaled Abdel-Motagaly
  • Publication number: 20100057511
    Abstract: 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: Application
    Filed: March 2, 2009
    Publication date: March 4, 2010
    Inventors: Ali R. Mansouri, John L. Vian, John T. Peters
  • Publication number: 20080312783
    Abstract: 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: Application
    Filed: September 28, 2007
    Publication date: December 18, 2008
    Applicant: THE BOEING COMPANY
    Inventors: Ali R. Mansouri, John L. Vian, Krzysztof Wojtek Przytula, David Allen
  • Publication number: 20080306637
    Abstract: 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: Application
    Filed: June 5, 2007
    Publication date: December 11, 2008
    Inventors: Mori M. Borumand, Ali R. Mansouri, John L. Vian
  • Publication number: 20080033684
    Abstract: 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: Application
    Filed: July 24, 2006
    Publication date: February 7, 2008
    Applicant: THE BOEING COMPANY
    Inventors: 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