|국가/구분||United States(US) Patent 등록|
|국제특허분류(IPC7판)||B64D-027/24 B60L-011/06 H02J-001/10 H02J-004/00 B64D-027/02 H02J-001/00|
|발명자 / 주소|
|출원인 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 0 인용 특허 : 82|
A propulsion system includes an electric propulsor and a gas turbine engine. The propulsion system also includes an electric machine coupled to a rotary component of the gas turbine engine generating a voltage at a baseline voltage magnitude during operation of the gas turbine engine. An electric communication bus is provided electrically connecting the electric machine to the electric propulsor. The propulsion system additionally includes a means for providing a differential voltage to the electric propulsor equal to about twice the baseline voltage mag...
1. A propulsion system for an aeronautical device comprising: an electric propulsor;a gas turbine engine comprising a compressor section, a turbine section, and a rotary component rotatable with at least a portion of the compressor section and with at least a portion of the turbine;a first electric machine coupled to the rotary component of the gas turbine engine, the first electric machine generating a positive voltage at a baseline voltage magnitude during operation of the gas turbine engine;an electric communication bus electrically connecting the fir...