Invention Grant
- Patent Title: Thermal stress reduction in aircraft motor controllers
- Patent Title (中): 飞机电机控制器的热应力降低
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Application No.: US14282273Application Date: 2014-05-20
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Publication No.: US09435263B2Publication Date: 2016-09-06
- 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
- Agency: Cantor Colburn LLP
- Main IPC: H02P1/04
- IPC: H02P1/04 ; F02C7/26 ; H02M7/487 ; 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
- US20140250910A1 THERMAL STRESS REDUCTION IN AIRCRAFT MOTOR CONTROLLERS Public/Granted day:2014-09-11
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