Thermal stress reduction in aircraft motor controllers

US9435264B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-9435264-B2
Application numberUS-201414282312-A
CountryUS
Kind codeB2
Filing dateMay 20, 2014
Priority dateApr 20, 2012
Publication dateSep 6, 2016
Grant dateSep 6, 2016

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  2. Abstract

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  5. First independent claim

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Abstract

Official abstract text for this publication.

A thermal stress reduction method includes ramping an electric power generator to start an aircraft engine, for a time period associated with the aircraft engine start sequence toggling a three-level inverter switch array to a three-level pulse width modulation mode, determining if a first time interval in the three-level pulse width modulation mode exceeded a predetermined three-level pulse width modulation mode interval, in response to the first time interval exceeding the three-level pulse width modulation mode interval, toggling the three-level inverter switch array to a two-level pulse width modulation mode, determining if a second time interval in the two-level pulse width modulation mode exceeded a predetermined two-level pulse width modulation mode interval and in response to the second time interval exceeding the two-level pulse width modulation mode interval, toggling the three-level inverter switch array to the three-level pulse width modulation mode.

First claim

Opening claim text (preview).

The invention claimed is: 1. A thermal stress reduction method for an aircraft motor controller having a three-level inverter switch array, and configured to control an electric power generator coupled to an aircraft engine during an aircraft engine start sequence, the method comprising: ramping the electric power generator to start the aircraft engine; and for a time period associated with the aircraft engine start sequence, ramping an output frequency of the motor controller from…

Assignees

Inventors

Classifications

  • H02M7/487Primary

    Electricity · mapped topic

  • Electricity · mapped topic

  • F02C7/26Primary

    Mechanical Engineering · mapped topic

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What does patent US9435264B2 cover?
A thermal stress reduction method includes ramping an electric power generator to start an aircraft engine, for a time period associated with the aircraft engine start sequence toggling a three-level inverter switch array to a three-level pulse width modulation mode, determining if a first time interval in the three-level pulse width modulation mode exceeded a predetermined three-level pulse wi…
Who is the assignee on this patent?
Hamilton Sundstrand Corp
What technology area does this patent fall under?
Primary CPC classification H02M7/487. Mapped technology areas include Electricity.
When was this patent published?
Publication date Tue Sep 06 2016 00:00:00 GMT+0000 (Coordinated Universal Time) (B2). Legal status and post-grant events are not shown on this page.
What related patents are in patentsdb?
We list 8 related publications on this page (citations in our corpus or others sharing the same primary CPC).