Invention Application
- Patent Title: THERMAL STRESS REDUCTION IN AIRCRAFT MOTOR CONTROLLERS
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Application No.: US14282312Application Date: 2014-05-20
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Publication No.: US20140253005A1Publication Date: 2014-09-11
- Inventor: Huazhen Chai , Adam M. White , Mustansir Kheraluwala
- Applicant: Hamilton Sundstrand Corporation
- Applicant Address: US NC Charlotte
- Assignee: Hamilton Sundstrand Corporation
- Current Assignee: Hamilton Sundstrand Corporation
- Current Assignee Address: US NC Charlotte
- Main IPC: H02P9/08
- IPC: H02P9/08

Abstract:
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.
Public/Granted literature
- US09435264B2 Thermal stress reduction in aircraft motor controllers Public/Granted day:2016-09-06
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