Systems and methods for controlling aircraft electrical power

Systems and methods for controlling aircraft electrical power

Systems and methods for controlling aircraft electrical power are disclosed. A system in accordance with one embodiment includes an electric motor, an aircraft load coupled to the electric motor and powered by the electric motor, and a motor controller coupled to the electric motor to vary an output...

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Hauptverfasser: White, Jeffrey J, Toy, David K, Groat, J. Everett
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Sprache:eng
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creator White, Jeffrey J
Toy, David K
Groat, J. Everett
description Systems and methods for controlling aircraft electrical power are disclosed. A system in accordance with one embodiment includes an electric motor, an aircraft load coupled to the electric motor and powered by the electric motor, and a motor controller coupled to the electric motor to vary an output of the electric motor. The motor controller is changeable among a fixed number of preset controller modes, with individual controller modes corresponding to an operation mode of the aircraft and a non-zero output level of the electric motor. In further embodiments, motor controllers can be substituted for each other, e.g., in the event one motor controller becomes unoperational.
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A system in accordance with one embodiment includes an electric motor, an aircraft load coupled to the electric motor and powered by the electric motor, and a motor controller coupled to the electric motor to vary an output of the electric motor. The motor controller is changeable among a fixed number of preset controller modes, with individual controller modes corresponding to an operation mode of the aircraft and a non-zero output level of the electric motor. 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Everett</creatorcontrib><creatorcontrib>The Boeing Company</creatorcontrib><title>Systems and methods for controlling aircraft electrical power</title><description>Systems and methods for controlling aircraft electrical power are disclosed. A system in accordance with one embodiment includes an electric motor, an aircraft load coupled to the electric motor and powered by the electric motor, and a motor controller coupled to the electric motor to vary an output of the electric motor. The motor controller is changeable among a fixed number of preset controller modes, with individual controller modes corresponding to an operation mode of the aircraft and a non-zero output level of the electric motor. 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Everett</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-uspatents_grants_081558763</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng</language><creationdate>2012</creationdate><toplevel>online_resources</toplevel><creatorcontrib>White, Jeffrey J</creatorcontrib><creatorcontrib>Toy, David K</creatorcontrib><creatorcontrib>Groat, J. Everett</creatorcontrib><creatorcontrib>The Boeing Company</creatorcontrib><collection>USPTO Issued Patents</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>White, Jeffrey J</au><au>Toy, David K</au><au>Groat, J. Everett</au><aucorp>The Boeing Company</aucorp><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>Systems and methods for controlling aircraft electrical power</title><date>2012-04-10</date><risdate>2012</risdate><abstract>Systems and methods for controlling aircraft electrical power are disclosed. A system in accordance with one embodiment includes an electric motor, an aircraft load coupled to the electric motor and powered by the electric motor, and a motor controller coupled to the electric motor to vary an output of the electric motor. The motor controller is changeable among a fixed number of preset controller modes, with individual controller modes corresponding to an operation mode of the aircraft and a non-zero output level of the electric motor. In further embodiments, motor controllers can be substituted for each other, e.g., in the event one motor controller becomes unoperational.</abstract><oa>free_for_read</oa></addata></record>
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title Systems and methods for controlling aircraft electrical power
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