|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||060/786; 060/778; 060/788|
|발명자 / 주소|
|출원인 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 30 인용 특허 : 16|
A power take-off system for a gas turbine engine includes a starter coupled to a second spool, and a clutch assembly coupled between the starter and a first spool, the clutch assembly configured to couple the first spool to the starter when starting the gas turbine engine assembly. A method of assembling a gas turbine engine assembly that includes the power take-off system, and a gas turbine engine assembly including the power take-off system are also described.
What is claimed is: 1. A method for assembling a gas turbine engine assembly including a first spool including a high-pressure compressor, a high-pressure turbine, and shaft coupled between the high-pressure compressor and the high-pressure turbine, and a second spool that is disposed coaxially with the first spool, said method comprising:coupling a starter to the second spool using a drive shaft; andcoupling a clutch assembly between the starter and the first spool, wherein the clutch assembly includes a clutch and a clutch actuator configured to axiall...