DETAILED DESIGN OF A 30-KW SWITCHED RELUCTANCE STARTER GENERATOR SYSTEM FOR A GAS-TURBINE ENGINE APPLICATION

被引：136
|
作者：
FERREIRA, CA [1 ]
JONES, SR [1 ]
HEGLUND, WS [1 ]
JONES, WD [1 ]
机构：
[1] GE CO,AIRCRAFT ENGINE CONTROLS,LYNN,MA 01910
来源：
IEEE TRANSACTIONS ON INDUSTRY APPLICATIONS | 1995年 / 31卷 / 03期
关键词：
D O I：
10.1109/28.382116
中图分类号：
T [工业技术];
学科分类号：
08 ;
摘要：
A new switched reluctance starter/generator (SR S/G) system has been developed for an aircraft engine application, The system is rated at 30 kW, 270 Vdc, 52 k r/min maximum operating speed, The system also provides 17 hp to start the 1400-hp engine. The system consists of an SR machine directly coupled to the gas turbine engine, an inverter converter unit (ICU), and an electronic controller, The system is designed to meet requirements such as power quality per MIL-STD-704E, 30% (9 kW) step loads, 75% constant power loads, operation over a wide speed range, and a -51 degrees C to +125 degrees C environment. This paper focuses on the design and implementation of the system, The SR S/G system is currently undergoing design assurance tests, Test results are given to validate the system design and performanee. System efficiency is about 80% when generating 30 kW.
引用
收藏
页码：553 / 561
页数：9
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