Invention Grant
- Patent Title: Acoustic structure for a gas turbine engine
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Application No.: US14228375Application Date: 2014-03-28
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Publication No.: US09909501B2Publication Date: 2018-03-06
- Inventor: Stephen Caulfeild , Bryan Olver , Kin-Leung Cheung
- Applicant: Pratt & Whitney Canada Corp.
- Applicant Address: CA Longueuil, QC
- Assignee: PRATT & WHITNEY CANADA CORP.
- Current Assignee: PRATT & WHITNEY CANADA CORP.
- Current Assignee Address: CA Longueuil, QC
- Agency: Norton Rose Fulbright Canada LLP
- Main IPC: F02C7/25
- IPC: F02C7/25 ; F02C7/24 ; F02K1/82 ; F23M20/00

Abstract:
An acoustic structure for a gas turbine engine comprising a noise reduction layer and a fire protector layer connected to the noise reduction layer. The noise reduction includes a perforated inner wall adapted to be in contact with a first fluidic environment, and a noise reduction adjacent to the inner wall. The fire protector layer includes a non-perforated outer wall adapted to be in contact with a second fluidic environment having potentially a fire, a fire protector adjacent to the outer wall, and a pressure resisting wall disposed between the fire protector and the noise reduction. The second fluidic environment is under a pressure lower than a pressure of the first fluidic environment. The inner and outer walls are load-bearing walls of the acoustic structure.
Public/Granted literature
- US20150118023A1 ACOUSTIC STRUCTURE FOR A GAS TURBINE ENGINE Public/Granted day:2015-04-30
Information query
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