|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||060/772; 060/224; 060/226.1|
|발명자 / 주소|
|출원인 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 2 인용 특허 : 8|
A gas turbine engine assembly includes at least one propelling gas turbine engine and an auxiliary engine used for generating power. The propelling gas turbine engine includes a fan assembly and a core engine downstream from said fan assembly. The core engine includes a compressor, a high pressure turbine, a low pressure turbine, and a booster turbine coupled together in serial-flow arrangement such that the booster turbine is rotatably coupled between the high and low pressure turbines. The auxiliary engine includes at least one turbine and an inlet. T...
What is claimed is: 1. A method for assembling a gas turbine engine assembly, said method comprising: providing at least one propelling gas turbine engine that includes a fan assembly and a core engine including a core drive fan, a high pressure compressor, and a high pressure turbine coupled together in serial-flow arrangement; and coupling an auxiliary engine to the propelling gas turbine engine such that during operation of the propelling gas turbine engine, at least a portion of the airflow entering the propelling gas turbine engine is selectively e...