发明名称 |
Acoustic structure for a gas turbine engine |
摘要 |
An acoustic structure (20) for a gas turbine engine comprises a noise reduction layer (20a) and a fire protector layer (20b) connected to the noise reduction layer (28). The noise reduction (24) includes a perforated inner wall (22) adapted to be in contact with a first fluidic environment (E1), and a noise reduction (24) adjacent to the inner wall (22). The fire protector layer (20b) includes a non-perforated outer wall (26) adapted to be in contact with a second fluidic environment (E1) having potentially a fire, a fire protector (28) adjacent to the outer wall (26), and a pressure resisting wall (30) disposed between the fire protector (28) and the noise reduction (24). The second fluidic environment (E2) is under a pressure lower than a pressure of the first fluidic environment (E1). The inner and outer walls (22, 26) are load-bearing walls of the acoustic structure (20). |
申请公布号 |
EP2821621(A1) |
申请公布日期 |
2015.01.07 |
申请号 |
EP20140173524 |
申请日期 |
2014.06.23 |
申请人 |
PRATT & WHITNEY CANADA CORP. |
发明人 |
CAULFEILD, STEPHEN;OLVER, BRYAN;CHEUNG, KIN-LEUNG |
分类号 |
F02C7/045;B64C1/40;F02C7/24;F02C7/25;F02K1/82;G10K11/168 |
主分类号 |
F02C7/045 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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