|국가/구분||United States(US) Patent 등록|
|국제특허분류(IPC7판)||B64D-029/06 F01D-025/28 F01D-025/24|
|발명자 / 주소|
|출원인 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 0 인용 특허 : 25|
A core cowl for use with an engine core of a gas turbine engine includes a first cowl section for covering a first side of an engine core and a second cowl section for covering a second side of the engine core. A locking retractor connects the first cowl section to a support structure.
1. A gas turbine engine comprising: an engine core;a core cowl extending circumferentially around the engine core, the core cowl comprising: a first cowl section on a first side of the engine core; anda second cowl section on a second side of the engine core; anda locking retractor connecting the first cowl section to a support structure, the locking retractor comprising: a spool;a flexible coupler attached to and wrapped at least partially around the spool; andan inertial locking mechanism connected to the spool for locking rotation of the spool in resp...