|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||322/23 ; 322/28 ; 322/29 ; 361/20|
|발명자 / 주소|
|출원인 / 주소|
|인용정보||피인용 횟수 : 36 인용 특허 : 0|
The problems of minimizing size and weight in an aircraft and avoiding requirements for custom design are minimized in a generator control unit (22) provided with separate digital control circuits (74 and 76) for implementing voltage regulation and speed control. These circuits (74 and 76) are manufactured using custom very large scale integration (VLSI) technology to reduce size, weight, life cycle costs and improve reliability.
A generator control unit for an electrical power generating system (EPGS) having a generator, a drive for the generator, and fault control means connecting said generator in the EPGS for protecting the EPGS under fault conditions, the generator control unit comprising: a control circuit including means responsive to system condition inputs for controlling generator operation to maintain generator output power at a desired voltage level and frequency, wherein said control circuit includes first and second digital control circuits for developing respective...