다음과 같은 기능을 한번의 로그인으로 사용 할 수 있습니다.NTIS 바로가기
다음과 같은 기능을 한번의 로그인으로 사용 할 수 있습니다.DataON 바로가기
다음과 같은 기능을 한번의 로그인으로 사용 할 수 있습니다.Edison 바로가기
다음과 같은 기능을 한번의 로그인으로 사용 할 수 있습니다.Kafe 바로가기
|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||60/3916 ; R ; 60/3951 ; R|
|발명자 / 주소|
|출원인 / 주소|
|인용정보||피인용 횟수 : 11 인용 특허 : 1|
A gas turbine engine is constructed having a forward differentially geared power output with an adjacent inlet for the introduction of airflow to the engine. After the airflow is compressed, it is discharged into an annular regenerator which is heated by exhaust gases. A reverse flow can-type combustor is located within the annular regenerator and receives the preheated air therefrom. The exhaust gas from the combustor is directed forward, first, to the power turbine and then to the gasifier turbine, after which it is exhausted through the regenerator.
A gas turbine engine having forward and rear portions comprising: a housing having an interior duct through which air may pass, said duct having upstream and downstream portions relative to the direction of airflow through the duct; a compressor shaft rotably mounted within the housing, said compressor shaft being constructed with a coaxial interior passage; a compressor impeller mounted on the compressor shaft for rotation therewith, said impeller extending into the interior duct to increase the velocity of the air flowing in the duct upon rotation of t...