Invention Grant
- Patent Title: Dual-structured aircraft engine starter/generator
- Patent Title (中): 双结构飞机发动机起动器/发电机
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Application No.: US11797451Application Date: 2007-05-03
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Publication No.: US07687928B2Publication Date: 2010-03-30
- Inventor: Dinesh N. Taneja , Hao Huang , Gary A. Padgett , Jan Zywot , Paul J. Wirsch, Jr. , Mohamed A. Abbas
- Applicant: Dinesh N. Taneja , Hao Huang , Gary A. Padgett , Jan Zywot , Paul J. Wirsch, Jr. , Mohamed A. Abbas
- Applicant Address: US MI Grand Rapids
- Assignee: Smiths Aerospace, LLC
- Current Assignee: Smiths Aerospace, LLC
- Current Assignee Address: US MI Grand Rapids
- Agency: Armstrong Teasdale LLP
- Agent William Scott Andes, Esq.
- Main IPC: H02P9/00
- IPC: H02P9/00 ; H02P9/02 ; F02N11/04

Abstract:
An aircraft starting and generating system includes a first starter/main machine assembly that includes a first exciter and a first main machine, and second starter/main machine assembly that includes a second exciter and a second main machine. The system also includes a permanent magnet generator (PMG) that is connected to the first and second starter/main machine assemblies. The system further includes a first inverter/converter/controller (ICC) that is connected to the first starter/main machine assembly and to the PMG, and a second ICC that is connected to the second starter/main machine assembly and to the PMG. The first and second ICCs generate AC power to respective drive the first and second starter/main machine assemblies in a start mode of the starting and generating system for starting a prime mover of the aircraft, and the first and second ICCs convert AC power, respectively obtained from the PMG after the prime mover has been started, to DC power in a generate mode of the starting and generating system.
Public/Granted literature
- US20080093850A1 Dual-structured aircraft engine starter/generator Public/Granted day:2008-04-24
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