Invention Grant
- Patent Title: Acoustic liner for gas turbine engine components
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Application No.: US14984767Application Date: 2015-12-30
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Publication No.: US10174675B2Publication Date: 2019-01-08
- Inventor: Michael Moses Martinez , Rudramuni Kariveerappa Majjigi , Steven Thomas Davies , Egbert Geertsema
- Applicant: General Electric Company , MRA SYSTEMS, INC.
- Applicant Address: US NY Schenectady US MD Baltimore
- Assignee: General Electric Company,MRA Systems, Inc.
- Current Assignee: General Electric Company,MRA Systems, Inc.
- Current Assignee Address: US NY Schenectady US MD Baltimore
- Agency: General Electric Company
- Agent Pamela Kachur
- Main IPC: F02C7/045
- IPC: F02C7/045 ; B64D33/02 ; F04D29/66 ; G10K11/168 ; G10K11/172

Abstract:
A single degree of freedom (SDOF) acoustic liner includes a porous face sheet, a substantially imperforate back sheet generally parallel to and opposing said porous face sheet and defining a thickness therebetween, and an acoustic core layer of contiguous adjacent resonant cavities disposed between the porous face sheet and the imperforate back sheet. The acoustic core layer includes a first resonant cell having a first internal volume therein and a second resonant cell having a second internal volume therein different than the first internal volume. A cell partition wall extends between the porous face sheet and the imperforate back sheet, and separates and seals the first resonant cell from the second resonant cell. In a thickness direction, and perpendicular to a plane generally parallel with the porous face sheet and the substantially imperforate back sheet, the first internal volume overlaps the second internal volume over the cell partition wall.
Public/Granted literature
- US20170191414A1 ACOUSTIC LINER FOR GAS TURBINE ENGINE COMPONENTS Public/Granted day:2017-07-06
Information query
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