# US 12,180,891 B2 · Acoustic panel for a turbine engine > Agents: this data is available as JSON from the patentgrep API and MCP server — see https://patentgrep.com/llms.txt - Number: US 12,180,891 B2 - Document ID: US12180891B2 - Status: Granted - Kind: B2 - Application number: 18/554,958 - Filed: 2022-04-11 - Published: 2024-06-13 - Granted: 2024-12-31 - Earliest claimed: 2021-04-12 - Assignees: Safran Nacelles - Applicants: Safran Nacelles - Inventors: Marc Versaevel; Bertrand Léon Marie Desjoyeaux; Pierre-Yves Gini - Web page: https://patentgrep.com/patent/US12180891B2 ## CPC - F02C 7/045: having provisions for noise suppression - F02C 7/24: Heat or noise insulation (air intakes having provisions for noise suppression F02C7/045; turbine exhaust heads, chambers, or the like F01D25/30; silencing nozzles of jet-propulsion plants F02K1/00) - F02K 1/827: {Sound absorbing structures or liners} - F05D 2250/283: honeycomb - F05D 2260/96: Preventing, counteracting or reducing vibration or noise - F05D 2260/963: by Helmholtz resonators - F02C: GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS (construction of turbines F01D; jet-propulsion plants F02K; construction of compressors or fans F04; generating combustion products of high pressure or high velocity F23R; using gas turbines in compression refrigeration plants F25B11/00) - F02K: JET-PROPULSION PLANTS (features of jet-propulsion plants common to gas-turbine plants, air intakes or fuel supply control of air-breathing jet-propulsion plants F02C7/00, F02C9/00) - F05D: INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS ## Abstract An acoustic panel for a turbine engine includes a first strip and a second strip each comprising an alternation of first ridges and second ridges connected by sidewalls. The first and second strips are joined to each other to form a plurality of cells, each delimited by a first ridge of the first strip and a first ridge of the second strip. A third strip is interposed between the first strip and the second strip and includes a first lateral wall bearing on the first strip The third strip further includes at least one tab that extends inside one of the cells and delimits all or part of a passage inside the associated cell. ## Claims ### Claim 1 An acoustic panel for a turbine engine, the acoustic panel comprising: a first strip and a second strip, corrugated, each comprising an alternation, according to a first direction (A1), first ridges and second ridges connected by sidewalls, said first strip and said second strip being joined to each other according to a second direction (A2) transverse to the first direction (A1), so as to form a plurality of cells each delimited, in the second direction (A2), by a first ridge of the first strip and a first ridge of the second strip, each cell extending according to a third direction (A3) transverse to the first direction (A1) and to the second direction (A2), and a third strip interposed, in the second direction (A2), between the first strip and the second strip, the third strip comprising a first lateral wall bearing, in the second direction (A2), on the first strip, the third strip further comprising at least one tab which extends inside one of the plurality of cells, at least partially transversely to the third direction (A3) of the associated cell, said at least one tab being connected, at a first end edge in the second direction (A2), to the first lateral wall, said at least a tab delimiting all or part of a passage in the third direction (A3) inside the associated cell, wherein the third strip comprises a plurality of tabs offset from each other in the third direction (A3) of the associated cell, and wherein the passages totally or partially delimited by consecutive first tab and second tab in the third direction (A3) are offset from each other in a direction transverse to the third direction (A3) of the associated cell. ### Claim 2 (depends on 1) The acoustic panel according to claim 1, wherein the passage is delimited by a free edge of the tab and one amongst the first ridge of the first strip and the first ridge of the second strip, delimiting the associated cell. ### Claim 3 (depends on 1) The acoustic panel according to claim 1, wherein the passage is an opening with closed contours formed in the tab. ### Claim 4 (depends on 1) The acoustic panel according to claim 1, wherein each cell has a section transverse to the associated third direction (A3) which is hexagonal, and wherein said at least one tab comprises a central portion which extends, in the second direction (A2), between the first ridges of the first strip and of the second strip, which delimit the associated cell, and two lateral portions each extending, in the second direction (A2), between sidewalls of the first strip and of the second strip, opposite one another in the second direction (A2), which delimit the associated cell. ### Claim 5 An acoustic panel for a turbine engine, the acoustic panel comprising: a first strip and a second strip, corrugated, each comprising an alternation, according to a first direction (A1), first ridges and second ridges connected by sidewalls, said first strip and said second strip being joined to each other according to a second direction (A2) transverse to the first direction (A1), so as to form a plurality of cells each delimited, in the second direction (A2), by a first ridge of the first strip and a first ridge of the second strip, each cell extending according to a third direction (A3) transverse to the first direction (A1) and to the second direction (A2), and a third strip interposed, in the second direction (A2), between the first strip and the second strip, the third strip comprising a first lateral wall bearing, in the second direction (A2), on the first strip, the third strip further comprising at least one tab which extends inside one of the plurality of cells, at least partially transversely to the third direction (A3) of the associated cell, said at least one tab being connected, at a first end edge in the second direction (A2), to the first lateral wall, said at least a tab delimiting all or part of a passage in the third direction (A3) inside the associated cell, wherein the first lateral wall of the third strip comprises an alternation, in the first direction (A1), of first ridges and second ridges connected by sidewalls, each first ridge and second ridge of the first lateral wall respectively bearing, in the second direction (A2), on one of the first ridges and one of the second ridges of the first strip. ### Claim 6 (depends on 5) The acoustic panel according to claim 5, wherein the third strip further comprises a second lateral wall bearing, according to the second direction (A2), on the second strip, said at least one tab being connected, at a second end edge in the second direction (A2), to the second lateral wall. ### Claim 7 (depends on 6) The acoustic panel according to claim 6, wherein the second lateral wall of the third strip comprises an alternation, in the first direction (A1), of first ridges and second ridges connected by sidewalls, each first ridge and second ridge of the first lateral wall respectively bearing, in the second direction (A2), on one of the first ridges and one of the second ridges of the second strip, wherein each second ridge of the second lateral wall of the third strip, is clamped in the second direction (A2) between one of the second ridges of the first strip and one of the second ridges of the second strip. ### Claim 8 (depends on 5) The acoustic panel according to claim 5, wherein each second ridge of the first lateral wall of the third strip is clamped in the second direction (A2) between one of the second ridges of the first strip and one of the second ridges of the second strip. ### Claim 9 (depends on 1) A method for manufacturing an acoustic panel according to claim 1, the method comprising the steps of: i) providing the corrugated first strip and second strip each comprising the plurality of first ridges and second ridges connected by sidewalls, ii) providing the third strip comprising said at least one tab, iii) positioning the first lateral wall of the third strip bearing on the first strip according to the second direction (A2), and iv) joining the second strip to the first strip to form the plurality of cells, with the third strip interposed, in the second direction (A2), between the first strip and the second strip, said at least one tab extending inside one of the cells, wherein the first strip, the second strip and the third strip are preformed before steps iii) and iv). ### Claim 10 (depends on 9) The manufacturing method according to claim 9, wherein the first lateral wall of the third strip comprises an alternation, in the first direction (A1), of first ridges and second ridges connected by sidewalls, each first ridge and second ridge of the first lateral wall respectively bearing, in the second direction (A2), on one of the first ridges and one of the second ridges of the first strip, the third strip further comprising a second lateral wall bearing, according to the second direction (A2), on the second strip, said at least one tab being connected, at a second end edge in the second direction (A2), to the second lateral wall, wherein step ii includes the subsidiary steps of: a2) providing a third strip having a planar shape, b2) forming bend lines that delimit each first ridge and second ridge of the first lateral wall and of the second lateral wall of the third strip, c2) forming at least one pair of bend lines on the third strip, each of the at least one pair of bend line delimiting one of the end edges in the second direction (A2) of said at least one tab, the at least one pair of bend lines being joined at each first ridge of the first lateral wall and of the second lateral wall, d2) making a cutout in the third strip configured to form the passage delimited totally or partially by said at least one tab, e2) bending the first lateral wall and the second lateral wall so that each has a corrugated shape with an alternation of first ridges and second ridges connected by sidewalls, f2) bending said at least one tab with respect to the first lateral wall, and g2) bending the second lateral wall with respect to said at least one tab and to the first lateral wall so that each second ridge of the second lateral wall is opposite one of the second ridges of the first lateral wall. ### Claim 11 (depends on 10) The method according to claim 10, wherein steps e2, g2 and f2 are carried out by an automatic press brake.