|국가/구분||United States(US) Patent 등록|
|국제특허분류(IPC7판)||F23R-003/60 F23R-003/00 F23M-020/00|
|발명자 / 주소|
|출원인 / 주소|
|인용정보||피인용 횟수 : 0 인용 특허 : 23|
An acoustically dampened gas turbine engine having a gas turbine engine combustor with an acoustic damping resonator system is disclosed. The acoustic damping resonator system may be formed from one or more resonators positioned within the gas turbine engine combustor at an outer housing forming a combustor basket and extending circumferentially within the combustor. The resonator may be positioned in a head region of the combustor basket. In one embodiment, the resonator may be positioned in close proximity to an intersection between the outer housing a...
1. A turbine engine with an acoustic clamping resonator system, comprising: a gas turbine engine combustor positioned downstream from a compressor and formed from at least one outer housing defining a combustor basket and at least one upstream wall that is attached to the at least one outer housing, wherein at least one fuel nozzle of a fuel nozzle assembly extends into the combustor;at least one resonator positioned within the gas turbine engine combustor at the at least one outer housing and extending circumferentially within the combustor;wherein the ...