The Boeing Company

Ali Reza Mansouri

John Lyle Vian

Mori M Borumand

Emad William Saad

Khaled Abdel-Motagaly

Rangasamy Elangovan

James J Troy

Trevor Milton Laib

David L Allen

Charles A Erignac

John Anthony Trela

Joseph S Breit

Stefan Richard Bieniawski

Krzysztof Wojtek Przytula

Gregory John Clark

Paul Murray

Richard Leroy Rankin

Clete Mark Boldrin

Jonathan Patrick How

Ronald Carl Provine

Paul E R Pigg

Brett M Bethke

Michael Neil Witting

Markland T Gates

Mario J Valenti

Joseph Sherman Breit

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.

Health management of rechargeable batteries

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.

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.

Systems and methods for control system verification and health assessment

A method for monitoring a geographic area that using a plurality of unmanned mobile vehicles. Each unmanned mobile vehicle may be programmed with an operational plan to cover a specific subregion of said geographic area. Each unmanned mobile vehicle may be used to obtain visual images of its associated said subregion during operation. A surveillance system is also disclosed for monitoring a geographic area. The system includes a plurality of autonomously operated unmanned mobile vehicles. Each vehicle includes an onboard system that executes an operational plan to enable the vehicle to traverse a specific subregion of the geographic area. Each onboard system further includes a monitoring system to obtain visual images of its associated subregion.

Traffic and security monitoring system and method

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.

Systems and methods for health monitoring of complex systems

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.

Modular battery network system with life-optimal power management

A system for automatically detecting corona effects in operating dynamic electromechanical equipment may include: at least one sensor connected to operating dynamic electromechanical equipment, a controller connected to the at least one sensor and to the operating dynamic electromechanical equipment; and a corona phenomena detection device. The at least one sensor may be adapted to measure behavior of emitted signals of the operating dynamic electromechanical equipment. The controller may be adapted to adjust emitted signals of the operating dynamic electromechanical equipment to correct for errors detected by the sensor in the emitted signals The corona phenomena detection device may be adapted to automatically detect corona effects of the dynamic electromechanical equipment. The corona phenomena detection device may be connected to, or embedded in, the dynamic electromechanical equipment during manufacture of the dynamic electromechanical equipment, or retro-fitted to the dynamic electromechanical equipment.

Corona phenomena detection

The disclosure provides for an aircraft galley and lavatory energy system capable of independent operation from a separate aircraft energy generating system. The galley and lavatory energy system comprises an energy source providing electrical energy, heat energy, and at least one by-product; a plurality of galley and lavatory devices for receiving the electrical energy, the heat energy, and the at least one by-product; and, a plurality of connectors for connecting the electrical energy, the heat energy, and the at least one by-product to the galley and lavatory devices. The energy source comprises a fuel cell, a fuel module, and optionally, a supplemental fuel source.

Localized utility power system for aircraft

A method for inspecting structures that includes using a plurality of independent unmanned mobile vehicles. The unmanned mobile vehicles are equipped with a control and guidance system for enabling each unmanned mobile vehicle to operate autonomously. Each unmanned mobile vehicle may be programmed with an operating program that defines a path of travel for it, relative to a structure to be inspected. The unmanned mobile vehicles are deployed so that they cooperatively form a swarm that travels about the structure. At least one of said unmanned mobile vehicles is used to obtain inspection data of a portion of the structure as it executes its respective operating program.

System and method for inspection of structures and objects by swarm of remote unmanned vehicles

Life-optimal power management methods for battery networks system

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.

Growing community of inventors

Bothell, WA, United States of America

Ali Reza Mansouri