|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||060/039.15; 060/224; 060/785|
|발명자 / 주소|
|출원인 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 15 인용 특허 : 8|
A method facilitates assembling a gas turbine engine assembly. The method comprises providing at least one propelling gas turbine engine that includes a core engine including at least one turbine, coupling an auxiliary engine to the propelling gas turbine engine such that during operation of the propelling gas turbine engine, such that at least a portion of the airflow entering the propelling gas turbine engine is extracted from the propelling gas and channeled to the auxiliary engine for generating power, and coupling a modulating valve in flow communi...
What is claimed is: 1. A gas turbine engine assembly comprising: at least one propelling gas turbine engine comprising a fan, a core engine downstream from the fan, and a plurality of extraction points; a modulating valve coupled in flow communication to said at least one propelling gas turbine engine; and an auxiliary engine used for generating electrical power, said auxiliary engine comprising at least one turbine and an inlet, said inlet coupled in flow communication with said modulating valve, such that a portion of airflow entering said at least on...