Acoustic Barrier Caps in Acoustic Honeycomb

Abstract

An acoustic honeycomb structure having cells in which a friction-lock insertion process is used to position an acoustic barrier within the honeycomb cells to provide a multi-degree-of-freedom MDOF acoustic liner with various acoustic resonator depths. A solid polymer film is formed to form an acoustic barrier cap. The acoustic barrier cap is friction-locked and bonded to the cell wall at one or more cell depths to form an acoustically reflective rigid wall that forms an effective bottom edge for the acoustic resonator.

Description

[Technical field]

[0001] The present invention relates generally to acoustic systems used to attenuate noise. The invention involves the use of honeycombs to create nacelles and other structures that are useful for reducing noise generated by aircraft engines or other noise sources. More particularly, the invention is directed to acoustic structures in which an acoustically reflective solid barrier is inserted into one or more of the honeycomb cells to provide an internal termination of the acoustic cell that determines the acoustic depth of the acoustic cell. [Background technology]

[0002] It is widely recognized that the best approach to addressing excess noise generated by a particular source is to treat the noise at the source. This is typically accomplished by adding acoustic damping structures (acoustic treatment devices) to the structure of the noise source. One particular problematic noise source is the jet engine used in many passenger aircraft. Acoustic treatment devices are typically incorporated into the engine nacelles, including the inlet ducts, bypass ducts, and exhaust structures. These acoustic treatment devices have an acoustic liner that includes a relatively thin acoustic material or grid with millions of holes that create an acoustic impedance to the sound energy generated by the engine.

[0003] Honeycomb is a common material for use within aircraft and aerospace vehicles because it is relatively strong and lightweight. For acoustic applications such as engine nacelles, acoustic materials are added to the honeycomb structure so that the honeycomb cells are acoustically closed at the ends located away from the engine and covered with an acoustically transparent cover at the ends located closest to the engine. The closed honeycomb cells create an acoustic resonator that provides noise attenuation, damping, and / or suppression. The particular frequency of noise that is attenuated by a given honeycomb cell or resonator is directly related to the cell depth. In general, as the frequency of the noise decreases, the cell depth must be increased to provide sufficient damping or suppression.

[0004] A typical acoustic liner has a honeycomb core sandwiched between a solid face sheet or skin and a porous or other sound-transmitting face sheet or skin. The porous face sheet is located closest to the noise source, and the solid face sheet forms the bottom of the acoustic resonators. In this type of acoustic liner, all the honeycomb cells have equal depth. Such acoustic liners, where all the acoustic resonators have equal depth, are called single degree of freedom (SDOF) acoustic liners. SDOF liners provide sound damping only near certain sound frequencies.

[0005] The fundamental problem facing acoustic engineers designing acoustic liners for jet engines is to create an acoustic structure that provides sufficient suppression or damping of sound frequencies over the entire range of noise generated by the jet engine. Multiple SDOF acoustic liners with various resonator depths can be combined to attenuate noise over a wide range of frequencies. However, acoustic liners have also been developed that vary the effective resonator depth within a single liner. Such multiple resonator depth acoustic liners are called multiple degree of freedom (MDOF) acoustic liners. MDOF acoustic liners have been found to be effective at damping jet engine noise over a much wider frequency range than is possible when using SDOF acoustic liners.

[0006] One approach to creating an MDOF acoustic liner is to place individual solid inserts within the honeycomb cells. The solid inserts are located at various distances between the honeycomb edges to provide an acoustic barrier that forms the base of the acoustic resonator. See, for example, U.S. Patent No. 8,651,233, in which solid inserts are placed at various locations within the honeycomb cells to provide an MDOF acoustic liner with multiple resonator cavity depths that are well suited to damping a relatively wide range of sound frequencies.

[0007] The solid insert used to form the bottom of the acoustic resonator must be strong enough to act as an acoustic barrier or rigid wall that reflects substantially all sound waves over the frequency range being attenuated or damped. The solid insert must also be able to withstand the high temperatures to which jet engine acoustic liners will be exposed. The solid insert must be as lightweight as possible while still achieving the desired sound reflection.

[0008] Acoustic septa are positioned within the honeycomb cells to provide additional noise attenuation properties to the resonators. Each acoustic septum is typically constructed of a thin polymeric fabric or a perforated polymeric film. Acoustic septa do not function as acoustic barriers or rigid walls. Instead, they provide attenuation or damping of sound waves passing through them. One approach to positioning acoustic septa within honeycomb cells involves inserting separate pieces of light-weight septum fabric into the honeycomb cells to form septum caps with anchor flanges glued to the honeycomb walls. The use of septum caps is described in U.S. Patent No. 7,434,659, U.S. Patent No. 7,510,052, U.S. Patent No. 7,854,298, U.S. Patent No. 8,066,098, U.S. Patent No. 8,607,924, U.S. Patent No. 8,651,233, U.S. Patent No. 8,857,566, U.S. Patent No. 9,016,430, and U.S. Patent No. 9,469,985.

[0009] Another approach for placing acoustic septa within honeycomb cells involves inserting separate pieces of solid polymeric film into the honeycomb cells to form septum caps that also have anchor flanges glued to the honeycomb walls. The solid polymeric film is perforated to form the acoustic septa prior to or after inserting the polymeric film into the honeycomb cells. See, for example, U.S. Patent No. 8,413,761.

[0010] The process of placing septum caps into honeycomb cells requires friction locking of the septum caps within the cells to hold them in place prior to permanent bonding to the honeycomb walls. Friction locking of the septum caps is a critical aspect of this type of septum insertion procedure. If the friction locking is not sufficient, the septum caps may shift or otherwise move during handling. Even slight shifting of the septum caps can make it difficult to apply adhesive uniformly to the septum caps during bonding. Additionally, shifting of the septum caps can result in uncontrolled changes in acoustic properties. In a worst case scenario, if the friction locking is not sufficient, the septum caps may fall out of the honeycomb cell entirely. [Prior art documents] [Patent documents]

[0011] [Patent Document 1] U.S. Patent No. 8,651,233 [Patent Document 2] U.S. Patent No. 7,434,659 [Patent Document 3] U.S. Patent No. 7,510,052 [Patent Document 4] U.S. Patent No. 7,854,298 [Patent Document 5] U.S. Patent No. 8,066,098 [Patent Document 6] U.S. Patent No. 8,607,924 [Patent Document 7] U.S. Patent No. 8,857,566 [Patent Document 8] U.S. Patent No. 9,016,430 [Patent Document 9] U.S. Patent No. 9,469,985 [Patent Document 10] U.S. Patent No. 8,413,761 Summary of the Invention [Means for solving the problem]

[0012] In accordance with the present invention, it has been discovered that the friction lock insertion process utilized to place acoustic septa within honeycomb cells can also be used to place acoustic barriers within honeycomb cells to provide MDOF acoustic liners with a variety of acoustic resonator depths. The invention is based on the discovery that certain solid polymeric films having specific thicknesses and shapes can be formed to be acoustic barrier caps. The acoustic barrier caps can be friction locked and bonded to the cell walls to form an acoustically reflective rigid wall that forms an effective bottom end for the acoustic resonator.

[0013] The present invention is directed to an acoustic structure designed to be located near a source of noise, such as a jet engine or other power plant. The structure includes a honeycomb having a first edge for location proximate to the noise source, and a second edge. The honeycomb includes a plurality of cells, each having a left side and a right side. Each cell is formed by a lower wall extending between the first and second edges of the honeycomb, and an upper wall also extending between the first and second edges of the honeycomb. The lower wall has a lower left end portion, a lower right end portion, and a central lower portion. The upper wall has an upper left end portion, an upper right end portion, and a central upper portion. A left junction portion is formed along the left side of the cell where the lower and upper walls are joined. A right junction portion is formed along the right side of the cell where the lower and upper walls are joined. The depth of the cell is equal to the distance between the first and second edges of the honeycomb.

[0014] In accordance with a feature of the invention, an acoustic barrier cap is inserted into at least one of the cells to provide an acoustically reflective rigid wall that forms an acoustic bottom of the cell. The acoustic barrier cap is a solid polymeric film that is folded to form a flat acoustic barrier portion and a tab portion that surrounds the acoustic barrier portion. The flat acoustic barrier portion extends transversely to the upper and lower walls of the honeycomb. The flat acoustic barrier portion has a top side located nearest a first edge of the honeycomb and a bottom side located nearest a second edge of the honeycomb. The flat acoustic barrier portion is bounded by a boundary consisting of an upper right boundary portion, a central upper boundary portion, an upper left boundary portion, a lower right boundary portion, a central lower boundary portion, and a lower left boundary portion.

[0015] As another feature or invention, the tab portion of the acoustic barrier cap has an upper right tab, a central upper tab, and an upper left tab, all protruding from an upper boundary of the flat acoustic barrier portion, and the tab portion further has a lower right tab, a lower central tab, and a lower left tab, all protruding from a lower boundary of the flat acoustic barrier portion.

[0016] The acoustic barrier cap is inserted into the cell so that the top right tab friction locks against the top wall at the top right end, the center upper tab friction locks against the top wall at the center upper end, the top left tab friction locks against the top wall at the top left end, the bottom right tab friction locks against the bottom wall at the bottom right end, the center lower tab friction locks against the bottom wall at the center lower end, and the bottom left tab friction locks against the bottom wall at the bottom left end.

[0017] The present invention is directed to a precursor structure formed when an acoustic barrier cap is frictionally locked into a honeycomb cell. The present invention is further directed to an acoustic structure formed when an acoustic barrier cap is permanently bonded into a honeycomb, as well as methods for making the precursor and final acoustic structures.

[0018] The above discussed and many other features and attendant advantages of the present invention will become better understood by reference to the following detailed description when taken in conjunction with the accompanying drawings. [Brief description of the drawings]

[0019] [Figure 1] 1 is a perspective view of an exemplary acoustic structure according to the present invention; [Diagram 2] 2 is an enlarged view of a portion of the example acoustic structure shown in FIG. 1. [Diagram 3] FIG. 1 is a simplified diagram showing the insertion of an acoustic barrier cap into a cell of a honeycomb to form the preceding structure, with the septum frictionally locked within the cell. [Figure 4] FIG. 11 is a simplified diagram illustrating an example method for applying adhesive to a tab portion of an acoustic barrier cap. [Diagram 5] FIG. 1 illustrates a first exemplary acoustic barrier cap for insertion into a hexagonal honeycomb cell. [Figure 6] FIG. 13 illustrates a second exemplary acoustic barrier cap for insertion into a hexagonal honeycomb cell. [Figure 7] FIG. 2 is an exploded view of an exemplary acoustic liner. [Figure 8] FIG. 2 illustrates an example acoustic liner located near a noise source. [Figure 9] FIG. 2 is a simplified diagram showing the intra-honeycomb geometry of an embodiment of the present invention with acoustic barrier caps located at various heights within the same honeycomb. [Figure 10] FIG. 1 is a simplified cross-sectional view of a turbofan jet engine showing an example location where an acoustic liner is located. DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS

[0020] An exemplary acoustic structure according to the present invention is generally shown at 10 in Figures 1, 2 and 7. The acoustic structure 10 has a honeycomb 12 having a first edge 14, which will be located nearest a noise source, and a second edge 16. The honeycomb 10 has cells 18. Each cell 18 has a left side 20 and a right side 22. A lower wall 24 and an upper wall 26 each extend between the first edge 14 and the second edge 16 to define each cell 18. The lower wall 24 and the upper wall 26 preferably extend parallel to one another between the first edge 14 and the second edge 16. The lower wall 24 has a lower left end portion 28, a lower right end portion 30, and a central lower portion 32. The upper wall 26 has an upper left end portion 34, an upper right end portion 36, and a central upper portion 38. A left interface 40 is formed at the left side of each cell where the lower left end portion 28 and the upper left end portion 34 are joined. A right interface 40 is formed at the right side of each cell where the lower right end portion 30 and the upper right end portion 36 are joined.

[0021] Each cell 18 has a depth (also referred to as a core thickness) equal to and defined by the distance between first edge 14 and second edge 16. Each cell 18 has a cell size equal to the area enclosed by lower wall 24 and upper wall 26, measured at the first edge 14 of the cell and measured perpendicular to the cell walls.

[0022] The acoustic structure 10 has acoustic barrier caps 44. Each acoustic barrier cap 44 is a piece of solid polymeric film folded to form a flat acoustic barrier portion 46 and a tab portion 48 surrounding the flat acoustic barrier portion 46. The acoustic barrier caps 44 are positioned within the cells 18 between the first edge 14 and the second edge 16 to provide an acoustic cavity having a depth less than the depth of the cells 18. The acoustic cavity depth is the distance between the flat acoustic barrier portion 46 and the first edge 14. The flat acoustic barrier portion 46 is oriented transverse to the cell walls. It is preferred that the flat acoustic barrier portion 46 is oriented substantially perpendicular to the cell walls. Substantially perpendicular means an angle of 90°±10°.

[0023] An exemplary polymeric film insert is shown at 50 in FIG. 3 before the insert is folded and inserted into cell 18 to form acoustic barrier cap 44. Insert 50 has a flat acoustic barrier portion 52 and a tab portion 53 that surrounds flat acoustic barrier portion 52. Flat acoustic barrier portion has a boundary 54 (shown in phantom). Boundary 54 has an upper right boundary portion 60, a central upper boundary portion 62, an upper left boundary portion 64, a lower right boundary portion 66, a central lower boundary portion 68, and a lower left boundary portion 70. Flat acoustic barrier portion 52 has a top side 56 that is located nearest a first edge of the honeycomb when insert 50 is placed in the honeycomb cell. A bottom side 58 of the insert is located nearest a second edge of the honeycomb when insert 50 is placed in the honeycomb cell (see FIG. 2). During insertion into the honeycomb cell 18 , the tab portion 53 is folded toward the top side 56 of the flat acoustic barrier portion 54 .

[0024] The tab portion 53 of the insert 50 has: an upper right tab 72 protruding from the upper right border 60; a central upper tab 74 protruding from the central upper border 62; an upper left tab 76 protruding from the upper left border 64; a lower right tab 78 protruding from the lower right border 66; a central lower tab 80 protruding from the central lower border 68; and a lower left tab 82 protruding from the lower left border 70.

[0025] When the insert 50 is placed into the honeycomb cell 18 to form the acoustic barrier cap 44, the tabs frictionally lock against the cell walls as follows: the upper right tab 72 frictionally locks against the upper wall 26 at the upper right end portion 36; the central upper tab 74 frictionally locks against the upper wall 26 at the central upper portion 38; the upper left tab 76 frictionally locks against the upper wall 26 at the upper left end portion 34; the lower right tab 78 frictionally locks against the lower wall 24 at the lower right end portion 30; the central lower tab 82 frictionally locks against the lower wall 24 at the central lower portion 32; and the lower left tab 82 frictionally locks against the lower wall 24 at the lower left end portion 28.

[0026] The honeycomb 12 may be made from any of the conventional materials used to make honeycomb panels, including metals, ceramics, and composites. Exemplary composite materials include fiberglass, resin-impregnated aramid paper such as Nomex®, and various combinations of graphite fibers with appropriate matrix resins. Matrix resins that can withstand relatively high temperatures (177°C (350°F) to 260°C (500°F)) are suitable for use in acoustic panels for jet engines. Honeycombs made from metallic or ceramic materials can function at higher temperatures than honeycombs made from composite materials. However, composite honeycombs are suitable for jet engine acoustic panels because of their relatively light weight. Composite honeycombs are commercially available that can operate at temperatures of 177°C (350°F) to 260°C (500°F) for extended periods of time and up to 371°C (700°F) for short periods of time. Such high temperature honeycombs utilize a fiberglass fibrous support in combination with a high temperature resin, such as a polyamideimide resin or polyimide resin, used for the prepreg resin matrix, node adhesive, and coating resin. A suitable exemplary type of fiberglass reinforced hexagonal polyimide honeycomb is available from Hexcel Corporation (Casa Grande, Arizona) under the trade name HexWeb® HRH-327.

[0027] Honeycomb cells 18 have a cell perimeter shown in phantom at 84 in Figure 1. Cell perimeter 84 is defined by upper wall 26 and lower wall 24. Upper right end portion 36 and upper left end portion 34 each form a larger portion of cell perimeter 84 than central upper portion 38. Lower right end portion 30 and lower left end portion 28 form a larger portion of cell perimeter 84 than central lower portion 32. Irregular hexagonal shapes of this type are preferred.

[0028] Insert 50 is specifically designed to be inserted into irregular hexagonal shaped honeycomb cell 18. Top right tab 72 and top left tab 76 are each larger than center upper tab 74. Bottom right tab 78 and bottom left tab 82 are each larger than center lower tab 80. This tab configuration fits into the respective walls where the tabs frictionally lock when insert 50 is inserted into cell 18.

[0029] Acoustic barrier caps according to the present invention may also be inserted into cells having shapes other than the irregular hexagonal shape formed by cells 18 if the insert shape is modified to accommodate various cell geometries. The cell shape may be a regular hexagon or other cell shape suitable for use in making acoustical panels. For example, the acoustical honeycomb may be a flexible honeycomb where the cell walls form a combination of convex and concave curvatures that allow the honeycomb to be more easily formed into non-planar acoustical panels. A suitable flexible honeycomb is Flex-Core® flexible honeycomb available from Hexcel Corporation (Dublin, Calif.). Flex-Core® flexible honeycomb is made from a variety of suitable materials including 5052 or 5056 aluminum, aramid / phenolic composite, and fiberglass / phenolic composite.

[0030] The present invention is 2 (0.1 square inch) to 6.45 cm 2 (1.0 in2) is applicable to cell sizes ranging from 0.645cm 2 Cell sizes less than 0.1 in2 are too small to allow for the insertion of an acoustic barrier cap. 2 A cell size greater than 1.0 square inch would require a film that is too thick to fold and insert into the cell. The cell size is the area enclosed by the upper wall 26 and the lower wall 24, as measured at the first edge 14. Preferably, the cell size is 1.94 cm 2 (0.3 square inches) to 3.87 cm2 (0.6 in.) square. Particularly preferred are honeycomb cells in which the distance between opposing walls of the hexagonal cells (DC) is 0.965±0.127 cm (0.38±0.05 in.).

[0031] To provide a suitable acoustic barrier cap, the insert 50 must have sufficient size, shape, and flexibility to be folded and inserted into the cell. Additionally, the folded insert must have sufficient resilience to provide sufficient frictional locking of the acoustic barrier cap within the honeycomb cell to allow for subsequent handling, including application of an adhesive to permanently adhere the acoustic barrier cap within the cell. Additionally, the insert 50 must be made from a polymer capable of withstanding the high temperatures to which jet engine acoustic liners are typically exposed.

[0032] The flat acoustic barrier portion 52 of the insert 50 must be strong enough to allow the resulting acoustic barrier cap 44 to act as the bottom of the acoustic cavity and reflect a significant portion of the sound entering the cell 18. The flat acoustic barrier portion 52, when formed into the flat acoustic barrier portion 46 of the acoustic barrier cap, must be strong enough to provide an acoustic reflection coefficient of at least 0.75 for sound frequencies ranging from 500 Hz to 4000 Hz. More preferably, the reflection coefficient of the acoustic barrier cap is at least 0.8 for sound frequencies ranging from 500 Hz to 4000 Hz. The reflection coefficient is determined by the equation R=(Z-1) / (Z+1), where R is the reflection coefficient and Z is the frequency-dependent normalized impedance of the flat acoustic barrier portion A. A reflection coefficient of 1 equals 100% reflection of sound waves at a given frequency.

[0033] It has been discovered that polyetheretherketone (PEEK) films conventionally used to make perforated acoustic septum caps (see U.S. Patent No. 8,413,761) can also be used to make suitable acoustic barrier caps, provided the above criteria of size, shape, rebound (friction lock), insertion flexibility, and acoustic stiffness are met.

[0034] PEEK is a crystalline thermoplastic polymer that can be processed to form films that are either in the amorphous or crystalline phase. Compared to crystalline PEEK films, amorphous PEEK films have higher transparency and are easier to thermoform. Crystalline PEEK films are formed by heating amorphous PEEK films to a temperature above the glass transition temperature (Tg) of amorphous PEEK for a time sufficient to achieve a crystallinity on the order of 30% to 35%. Crystalline PEEK films have better chemical resistance and abrasion properties than amorphous films. In addition, crystalline PEEK films have lower flexibility and higher resilience than amorphous films. Resilience is the force or bias that causes a folded film to return to its original unfolded (flat) shape. Crystalline PEEK films are suitable for use in making acoustic barrier caps. Films of PEEK may be obtained from SEFAR America Inc. (DePew, NY) under the trade names SEFAR PETEX, SEFAR NITEX, and SEFAR PEEKTEX. PEEK sheets or films are also commercially available from Victrex USA (Greenville, SC), which produces films of PEEK under the trade name VICTREX® PEEK™ polymer.

[0035] Polymeric films other than PEEK film may be used if they exhibit comparable properties with respect to resilience (friction locking), insertion flexibility, acoustic strength, and thermal stability. For example, polyimide film is an alternative to PEEK film when used to make acoustic barrier caps. A variety of suitable polyimide films are available from DuPont Chemical Company (Midland, Michigan) under the trade name KAPTON® polyimide films. Films made from polyether ketone or polyphenylene sulfide are also suitable.

[0036] The polymeric film used to make the inserts must be between 0.00762 cm (0.003 in) and 0.0889 cm (0.035 in) thick, with a cell size of 0.645 cm or less. 2 (0.1 square inch) to 6.45 cm 2 (1.0 sq. inch). For cells 18 having a cell size of 0.4 inch to 0.5 inch, a preferred polymeric film thickness is 0.010 inch to 0.025 inch. This preferred film thickness has been found to provide a particularly useful combination of collapsibility, friction locking, and high acoustic reflection coefficient for insertion of the acoustic barrier cap. Inserts 50 preferably have a polymeric film thickness of 0.003 inch to 0.009 inch. Such inserts preferably have a polymeric film thickness of 0.645 cm. 2 (0.1 square inch) to 3.87 cm 2 It is used to make acoustic barrier caps that are inserted into hexagonal honeycombs with cell sizes of 0.6 square inches.

[0037] For hexagonal honeycomb cell sizes of 0.4 inches to 1.0 inches, insert thicknesses of 0.010 inches to 0.035 inches are preferred. Such a thicker insert is shown at 50T in FIG. 4. Insert 50T has the same basic shape as insert 50 (FIG. 3) except that a thin hole is cut in the tab to form a sub-tab that improves the flexibility of the thicker insert. This sub-tab portion ensures that the thicker insert 50T has the flexibility and resilience required to be inserted into the cells and frictionally locked therein.

[0038] The reference numbers used to indicate the various elements of insert 50T correspond to the reference numbers used to indicate the elements of insert 50. The corresponding reference numbers in FIG. 4 are appended with a "T" to reflect that the insert 50T is the same elements as those described for insert 50, except that it is thicker. Thus, the above description of the various reference numbers associated with insert 50 also applies to the corresponding reference numbers (T) described in FIG. 4. Tab portion 53T of insert 50T has an additional slot that divides each of tabs 72T, 74T, 76T, 78T, 80T, and 82T into a first sub-tab portion and a second sub-tab portion. The sub-tab portions are indicated in FIG. 4 using tab numbers suffixed with an "a" or "b" to indicate the individual sub-tab portions.

[0039] The size and shape of the flat acoustic barrier portion 52 (52T) will be the same as or slightly smaller than the size and shape of the cells. Preferably, the distance D (DT) between the opposing upper boundary portion 62 (62T) and the central lower boundary portion 68 (68T) is 85% to 95% of the corresponding distance between the opposing central upper wall portion 38 and the central lower wall portion 32. The slots in the insert S (ST) that separate the tabs from one another should terminate at or near the boundary of the flat acoustic portion 54 (54T). The slots should terminate at a distance from the boundary 54 (54T) equal to 0% to 50% of the tab width W (WT). Preferably, the slots should terminate at a distance from the boundary 54 (54T) equal to 2% to 20% of the tab width.

[0040] The width W(WT) of the tab portion 53 (53T) may vary depending on a number of factors, including cell size, flexibility (thickness) of the polymeric film, the number of tabs in the tab portion, and the adhesive used to permanently adhere the acoustic barrier cap to the cell wall. Tab portion widths on the order of 0.1 inch to 0.5 inch are suitable. Preferably, the tab portion width W(WT) is 5% to 35% of the distance D(DT) between the opposing central upper and lower borders.

[0041] The slots S (ST) separating the tabs from one another may be U-shaped, as shown at 90 and 90T, or V-shaped, as shown at 92 and 92T. It is preferred that the upper left tab 76 (76T) and the lower left tab 82 (82T) are separated from one another by V-shaped slots, and that the upper right tab 72 (72T) and the lower right tab 78 (78T) are also separated from one another by V-shaped slots. It has been found that V-shaped slots in these locations are effective in promoting proper folding and friction locking of the film insert within the honeycomb cells.

[0042] The insert with the combination of U-shaped and V-shaped slots shown in FIG. 3 was made from a crystalline PEEK film having a thickness of 0.006 inches. This insert was used to form an acoustic barrier cap in a HexWeb® HRH-327 honeycomb using cells with a DC of 0.38 inches. This acoustic barrier cap exhibited a reflection coefficient of about 0.8 for sound frequencies ranging from 500 Hz to 2000 Hz and 3500 Hz to 4000 Hz. The insert with the combination of U-shaped and V-shaped slots shown in FIG. 4 was made from a crystalline PEEK film having a thickness of 0.010 inches. This insert was used to form an acoustic barrier cap in a HexWeb® HRH-327 honeycomb using cells with a DC of 0.38 inches. The acoustic barrier cap exhibited a reflection coefficient that increased from 0.8 at 500 Hz to 0.9 over the entire range of 500 Hz to 4000 Hz. The thicker insert (0.010 inches) is particularly preferred because it provides a relatively high reflection coefficient over a wider frequency range compared to the thinner insert (0.006 inches). A relatively small increase in thickness of the PEEK film (0.004 inches) would not result in such an increase in reflection coefficient characteristics.

[0043] The tab portion of the insert may be perforated to increase the surface area of ​​the tab portion to enhance adhesive adhesion to the cell wall. These perforations increase the surface area and thus the openings through which the adhesive can enter, thereby improving adhesion of the tab portion to the cell wall. These perforations or holes may be drilled mechanically or using chemicals. Preferably, the perforations are made by laser drilling holes through a relatively thin polymeric film. Preferably, the polymeric film is laser drilled to provide the desired number of perforations before forming the insert into an acoustic barrier cap. The advantage of this procedure is that the flat insert surface makes it easier to focus the laser beam on the polymeric film during the drilling operation.

[0044] An exemplary method for inserting acoustic barrier caps into honeycomb cells to form a precursor structure in which the acoustic barrier caps are frictionally locked within the honeycomb cells is shown in Figure 5. The reference numbers used to indicate the honeycomb structure in Figure 5 are the same as those in Figure 1, except that the reference numbers have a "P" to indicate that the structure is a precursor structure in which the acoustic barrier caps have not yet been permanently bonded to the cell walls.

[0045] As shown in FIG. 5, a polymeric film 81 is cut to form an appropriately sized insert, such as insert 50 shown in FIG. 3. An appropriately sized plunger 83 is used to force insert 50 into the honeycomb cells using plunger 83. A cap folding die (not shown) may be used to assist the insertion process. The cap folding die has a die opening that is sized and shaped to pre-fold and form the acoustic barrier cap prior to being placed into the honeycomb cells. While the use of a cap folding die is preferred, this is not necessary. It is also possible to use the honeycomb as a die to form the acoustic barrier cap by simply forcing insert 50 into the cells using plunger 83. Many honeycomb panels tend to have relatively rough edges because the panels are cut from a typically larger honeycomb block during the manufacturing process. Such rough honeycomb edges tend to catch, tear, and smear the acoustic barrier cap when a flat insert film is forced directly into the cell, therefore, if the honeycomb is used as a die to fold and form the acoustic barrier cap, the honeycomb edges should be as smooth as possible.

[0046] Importantly, the size, shape, and flexibility of the polymeric film, and the size / shape of the plunger and die (or just the plunger if no die is used) may be selected to allow the acoustic barrier cap to be inserted into the cell without damaging the polymeric film while providing sufficient frictional contact between the tab portion and the cell wall to hold the acoustic barrier cap in place during subsequent handling of the preceding structure. The strength of the frictional lock or retention should be sufficient to keep the acoustic barrier cap from falling out of the honeycomb even if the preceding structure is accidentally dropped during handling.

[0047] Frictional locking of the acoustic barrier cap against the cell walls is achieved by varying the tab portion size, number of tabs, polymer film thickness, polymer film strength / resilience, slot size, and slot shape until a sufficient level of frictional locking is achieved. For example, frictional locking tends to decrease as the number of tabs and / or slot size increase. Frictional locking tends to increase as the polymer film thickness, polymer film strength / resilience, and tab size increase. It has been found that certain combinations of these parameters, such as those described above for inserts 50 and 50T, provide sufficient frictional locking of the acoustic barrier cap in the prior honeycomb structure.

[0048] The degree of friction locking of the acoustic barrier cap against the honeycomb cell walls is measured by placing a test weight on top of the acoustic barrier cap and determining whether any movement of the cap occurs as a result. For example, an acoustic barrier cap is considered to be frictionally locked against the honeycomb cell walls with sufficient friction locking force if it passes the following test: A test weight (27 grams) is placed on top of the dry acoustic barrier cap, insertion side up. Friction locking is sufficient if the dry cap supports the 27 grams without sliding downward along the honeycomb cell. In the exemplary test, the 27 gram test weight is a steel rod having a diameter of 0.935 cm (0.368 in) and a length of 5.08 cm (2.00 in).

[0049] The friction lock only holds the acoustic barrier cap 44p in place in the prior structure 10P of FIG. 5. As mentioned above, the friction lock must be great enough to hold the bulkhead cap securely in place until it can be permanently bonded using a suitable adhesive. The adhesive used may be any of the conventional adhesives used in the manufacture of honeycomb panels. Suitable adhesives include those that are stable at high temperatures (177°C (350°F) to 260°C (500°F)). Exemplary adhesives include epoxies, acrylics, phenolics, cyanoacrylates, bismaleimides, polyamideimides, and polyimides.

[0050] A variety of known adhesive application procedures may be used to apply the adhesive to the tab portion / cell wall interface. An important consideration is that the adhesive should be applied in a controlled manner. The adhesive should be applied to the tab portion at the cell wall interface as a minimum. An exemplary adhesive application procedure is shown in FIG. 6. In this exemplary procedure, the honeycomb 12P is simply dipped into a pool 91 of liquid adhesive so that only the tab portion 48P is immersed in the adhesive. This dipping procedure may be used to precisely apply the adhesive to the tab portion / cell wall interface if the acoustic barrier cap is frictionally locked at exactly the same level as it was prior to dipping. For acoustic barrier caps located at various heights, multiple dipping steps may be required. Alternatively, the adhesive may be applied using a brush or other site-specific application technique. Some of these techniques may be used to apply the adhesive to the core wall prior to inserting the acoustic barrier cap. Alternatively, the adhesive may be screen printed onto the tab portion prior to insertion into the core.

[0051] Such a dipping procedure for applying the adhesive depicted in FIG. 6 is preferred because the adhesive will tend to move upwards due to capillary action into the interface between the tab portion and the cell wall. This upward movement of the adhesive will fill any air gap between the tab portion and the cell wall, thereby ensuring that the acoustic barrier cap provides maximum sound reflection. Once in place, the adhesive is allowed to set or otherwise cure in accordance with known procedures, thereby permanently bonding the acoustic barrier cap to the honeycomb cell wall.

[0052] The acoustic structure according to the invention may be used in a wide variety of situations requiring noise attenuation. The acoustic structure is well suited for use in connection with power plant systems where noise attenuation is typically an issue. Because honeycomb is a relatively lightweight material, the acoustic structure according to the invention is particularly well suited for use in aircraft systems. Exemplary uses include nacelles for jet engines, cowlings for large turbine or reciprocating engines, or related acoustic structures. An exemplary turbofan jet engine is shown at 100 in FIG. 10. Jet engine 100 has a nacelle 102. Acoustic panels or liners according to the invention may be positioned, for example, at locations 104, 106, and 108 to provide damping or attenuation of noise generated by the jet engine.

[0053] The basic acoustic structure of the present invention is typically thermally formed to the final shape of the engine nacelle, and then a skin or sheet of outer material is bonded to the outer edges of the formed acoustic structure using an adhesive layer. This completed sandwich panel is set in a holding tool that maintains the complex shape of the nacelle during bonding. For example, as shown in FIG. 7, the acoustic structure 10 is bonded to a solid, sound-impermeable sheet or skin 80 on the second edge 16, and a sound-transmitting, porous skin or sheet 82 is bonded on the first edge 14, thereby forming an acoustic panel or liner. Bonding of the solid skin 80 and the porous skin 82 is typically accomplished on a bonding tool at high temperatures and pressures. The bonding tool is typically required to maintain the desired shape of the acoustic structure during the panel forming process.

[0054] In FIG. 8, a portion of an example acoustic panel 112 is shown in place as part of a nacelle surrounding a jet engine or other noise source. The jet engine or other noise source is shown generally at 110. The acoustic panel 112 has an acoustic structure 114, a sound-transmissive skin 116, and a solid sound-impermeable skin 118. Acoustic barrier caps 120 are present in some of the honeycomb cells 122 to form acoustic resonators having a depth equal to the distance from the sound-transmissive skin 116 to the flat acoustic portion of the acoustic barrier cap 120. Other honeycomb cells 124 do not have acoustic barrier caps, so that the effective resonator depth is equal to the distance from the sound-transmissive skin 116 to the solid skin 118. The acoustic panel 112 is illustrative of a type of MDOF acoustic liner that may be made in accordance with the present invention by using acoustic barrier caps to reduce the depth of some of the honeycomb cells.

[0055] Another exemplary acoustic panel is shown at 130 in FIG. 9. Acoustic panel 130 has an acoustic structure 132, a sound-transmissive skin 134, and a solid sound-impermeable skin 136. Acoustic barrier caps 138 and 140 are located within cells 142 and 146, respectively, to provide resonator cavities with different depths. Cell 148 has no acoustic barrier cap. Designing this type of MDOF such that multiple resonator depths are realized allows for fine tuning of the noise attenuation characteristics of the acoustic structure. The multiple resonator depth configuration shown in FIG. 9 is intended to be merely one example of the wide variety of possible multi-level acoustic barrier cap arrangements possible in accordance with the present invention. As will be recognized by those skilled in the art, the number and variations of the various acoustic barrier cap arrangement levels possible are vast and can be tailored to suit specific noise attenuation requirements.

[0056] Although exemplary embodiments of the present invention have been described, those skilled in the art should note that the present disclosure includes only examples, and that various other alternatives, adaptations, and modifications can be made within the scope of the present invention. Therefore, the present invention is not limited to only the preferred embodiments and examples described above, but is limited only by the following claims.

Claims

1. 1. A precursor to an acoustic structure in which an acoustic barrier cap is frictionally locked within a honeycomb cell to form an acoustic cavity for attenuating noise emanating from a source when the acoustic barrier cap is adhesively adhered within the honeycomb cell to form an acoustically rigid wall, A) a honeycomb having a first edge that will be located nearest the source, and a second edge, the honeycomb having cells having a left side and a right side, the cells being defined by a lower sidewall extending between the first edge and the second edge, and an upper sidewall also extending between the first edge and the second edge, the lower sidewall having a lower left end portion, a lower right end portion, and a central lower portion located between the lower left end portion and the lower right end portion, the upper sidewall having an upper left end portion, an upper right end portion, and a central lower portion located between the upper left end portion and the upper right end portion. a left junction along the left side of the cell at which the lower left end portion and the upper left end portion are joined, and a right junction along the right side of the cell at which the lower right end portion and the upper right end portion are joined, the cell having a depth defined by the distance between the first edge and the second edge, the cell having a cell area defined by the area enclosed by the upper and lower walls measured at the first edge, the cell area being 0.645 cm ２ (0.1 square inch) to 6.45 cm ２ (1.0 in 2 ) honeycomb; B) an acoustic barrier cap having a solid polymeric film folded to form a planar acoustic barrier portion and a tab portion surrounding the planar acoustic barrier portion, the solid film having a thickness of 0.00762 cm (0.003 inches) to 0.0889 cm (0.035 inches), the acoustic barrier cap positioned within the cell between the first edge and the second edge to provide an acoustic cavity having a depth less than a depth of the cell: a) the flat acoustic barrier portion extends transversely to the upper and lower walls, the flat acoustic barrier portion having a top side located closest to the first edge and a bottom side located closest to the second edge, the flat acoustic barrier portion having a boundary having a top right boundary, a central upper boundary, an upper left boundary, a lower right boundary, a central lower boundary, and a lower left boundary; b) the tab portions have a top right tab protruding from the top right boundary, a central upper tab protruding from the central upper boundary, an upper left tab protruding from the top left boundary, a lower right tab protruding from the bottom right boundary, a central lower tab protruding from the central lower boundary, and a lower left tab protruding from the bottom left boundary, the tab portions provide friction locking of the acoustic barrier cap within the cell, the top right tab frictionally locks against the top wall at the top right end portion, the central upper tab frictionally locks against the top wall at the top center portion, the top left tab frictionally locks against the top wall at the top left end portion, the bottom right tab frictionally locks against the bottom wall at the bottom right end portion, the central lower tab frictionally locks against the bottom wall at the bottom center portion, and the bottom left tab frictionally locks against the bottom wall at the bottom left end portion. Acoustic Barrier Cap and A precursor structure to an acoustic structure.

2. The acoustic structure of claim 1 , wherein the upper and lower walls form a hexagonal cell.

3. 3. The acoustic structure of claim 2, wherein the solid film has a thickness of 0.01 inch to 0.035 inch, and each of the upper right tab, the central upper tab, the upper left tab, the lower right tab, the central lower tab, and the lower left tab are divided into a first sub-tab portion and a second sub-tab portion.

4. 3. The acoustic structure of claim 2, wherein the cell has a cell perimeter defined by the upper and lower walls, the upper right and upper left end portions each form a portion of the cell perimeter that is larger than the central upper portion, the lower right and lower left end portions each form a portion of the cell perimeter that is larger than the central lower portion, each of the upper right and upper left tabs is larger than the central upper tab, and each of the lower right and lower left tabs is larger than the central lower tab.

5. 4. The acoustic structure of claim 3, wherein the cell has a cell perimeter defined by the upper and lower walls, the upper right and upper left end portions each form a portion of the cell perimeter that is larger than the central upper portion, the lower right and lower left end portions each form a portion of the cell perimeter that is larger than the central lower portion, each of the upper right and upper left tabs is larger than the central upper tab, and each of the lower right and lower left tabs is larger than the central lower tab.

6. 2. The acoustic structure of claim 1, wherein the upper left tab and the lower left tab are separated from each other by a V-shaped notch, and the upper right tab and the lower right tab are separated from each other by a V-shaped notch.

7. 2. The acoustic structure of claim 1, wherein the polymeric film is selected from the group consisting of polyetheretherketone films, polyimide films, polyetherketone films, and polyphenylene sulfide films.

8. 10. An acoustic structure comprising a precursor structure of claim 1 and an adhesive bonding said tab portions to said upper and lower walls to form said acoustically rigid walls.

9. 10. The acoustic structure of claim 8, further comprising a sound permeable sheet attached to a first edge of a honeycomb and a solid sound impermeable sheet attached to a second edge of said honeycomb.

10. 1. A method of making a precursor to an acoustic structure, comprising the steps of: frictionally locking an acoustic barrier cap into a cell of a honeycomb to form an acoustic cavity for attenuating noise emanating from a source when the acoustic barrier cap is adhesively adhered into the cell of the honeycomb to form an acoustically rigid wall; A) providing a honeycomb having a first edge that will be located nearest the source, and a second edge, the honeycomb having cells having a left side and a right side, the cells being defined by a lower side wall extending between the first edge and the second edge, and an upper side wall also extending between the first edge and the second edge, the lower side wall having a lower left end portion, a lower right end portion, and a central lower portion located between the lower left end portion and the lower right end portion, the upper side wall having an upper left end portion, an upper right end portion, and a central lower portion located between the upper left end portion and the upper right end portion, a left junction along the left side of the cell is formed at the left junction joining the lower left end portion and the upper left end portion, and a right junction along the right side of the cell is formed at the right junction joining the lower right end portion and the upper right end portion, the cell having a depth defined by the distance between the first edge and the second edge, the cell having a cell area defined by the area enclosed by the upper and lower walls measured at the first edge, the cell area being 0.645 cm ２ (0.1 square inch) to 6.45 cm ２ (1 inch square) honeycomb; B) providing a solid film that can be folded to form an acoustic barrier cap having a flat acoustic barrier portion and a tab portion surrounding said flat acoustic barrier portion, said solid film having a thickness of 0.00762 cm (0.003 inches) to 0.0889 cm (0.035 inches); a) the flat acoustic barrier portion has a boundary having a top right boundary portion, a central upper boundary portion, a top left boundary portion, a bottom right boundary portion, a central lower boundary portion, and a bottom left boundary portion; b) the tab portion has a top right tab protruding from the top right border, a central upper tab protruding from the central upper border, a top left tab protruding from the top left border, a bottom right tab protruding from the bottom right border, a central lower tab protruding from the central lower border, and a bottom left tab protruding from the bottom left border. providing a solid film; C) placing the solid film into the cell to form the acoustic barrier cap, the planar acoustic barrier portion extending transversely to the upper and lower walls, the planar acoustic barrier portion having a top side located nearest the first edge and a bottom side located nearest the second edge, the acoustic barrier cap positioned between the first and second edges to provide an acoustic cavity having a depth less than a depth of the cell, and the tab portion providing frictional locking of the acoustic barrier cap within the cell; placing said upper right tab frictionally locks against said upper wall at said upper right end portion, said central upper tab frictionally locks against said upper wall at said central upper portion, said upper left tab frictionally locks against said upper wall at said upper left end portion, said lower right tab frictionally locks against said lower wall at said lower right end portion, said central lower tab frictionally locks against said lower wall at said central lower portion, and said lower left tab frictionally locks against said lower wall at said lower left end portion; A method comprising:

11. 11. The method for making a precursor structure for an acoustic structure according to claim 10, wherein the upper and lower walls form a hexagonal cell.

12. 12. The method for making an acoustic structure of claim 11, wherein the solid film has a thickness of 0.01 inch to 0.035 inch, and each of the upper right tab, the central upper tab, the upper left tab, the lower right tab, the central lower tab, and the lower left tab are divided into a first sub-tab portion and a second sub-tab portion.

13. 12. A method for making a precursor structure for an acoustic structure as described in claim 11, wherein the cell has a cell perimeter defined by the upper and lower walls, the upper right and upper left end portions each form a portion of the cell perimeter that is larger than the central upper portion, the lower right and lower left end portions each form a portion of the cell perimeter that is larger than the central lower portion, each of the upper right and upper left tabs is larger than the central upper tab, and each of the lower right and lower left tabs is larger than the central lower tab.

14. 13. A method for making a precursor structure for an acoustic structure as described in claim 12, wherein the cell has a cell perimeter defined by the upper and lower walls, the upper right and upper left end portions each form a portion of the cell perimeter that is larger than the central upper portion, the lower right and lower left end portions each form a portion of the cell perimeter that is larger than the central lower portion, each of the upper right and upper left tabs is larger than the central upper tab, and each of the lower right and lower left tabs is larger than the central lower tab.

15. 11. The method for making a precursor structure of an acoustic structure according to claim 10, wherein the polymeric film is selected from the group consisting of polyetheretherketone films, polyimide films, polyetherketone films, and polyphenylene sulfide films.

16. 11. A method for making an acoustic structure precursor as claimed in claim 10, including the additional step of adhesively adhering said tab portions to said upper and lower walls of said cell.

17. 10. A method for making an acoustic structure comprising the steps of: providing a precursor structure to the acoustic structure of claim 1; and adhesively adhering the tab portions to the upper and lower walls of the cell.

18. 20. The method for making an acoustic structure of claim 17, wherein the upper wall and the lower wall form a hexagonal cell.

19. 20. The method for making an acoustic structure of claim 18, wherein the solid film has a thickness of 0.01 inch to 0.035 inch, and each of the upper right tab, the central upper tab, the upper left tab, the lower right tab, the central lower tab, and the lower left tab are divided into a first sub-tab portion and a second sub-tab portion.

20. 20. The method for making an acoustic structure according to claim 17, wherein the polymeric film is selected from the group consisting of polyetheretherketone films, polyimide films, polyetherketone films, and polyphenylene sulfide films.

Images