US3819007A - Controllable laminar sound absorptive structure - Google Patents
Controllable laminar sound absorptive structure Download PDFInfo
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- US3819007A US3819007A US00355161A US35516173A US3819007A US 3819007 A US3819007 A US 3819007A US 00355161 A US00355161 A US 00355161A US 35516173 A US35516173 A US 35516173A US 3819007 A US3819007 A US 3819007A
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Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B3/00—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form
- B32B3/26—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form characterised by a particular shape of the outline of the cross-section of a continuous layer; characterised by a layer with cavities or internal voids ; characterised by an apertured layer
- B32B3/266—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form characterised by a particular shape of the outline of the cross-section of a continuous layer; characterised by a layer with cavities or internal voids ; characterised by an apertured layer characterised by an apertured layer, the apertures going through the whole thickness of the layer, e.g. expanded metal, perforated layer, slit layer regular cells B32B3/12
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- E—FIXED CONSTRUCTIONS
- E04—BUILDING
- E04B—GENERAL BUILDING CONSTRUCTIONS; WALLS, e.g. PARTITIONS; ROOFS; FLOORS; CEILINGS; INSULATION OR OTHER PROTECTION OF BUILDINGS
- E04B1/00—Constructions in general; Structures which are not restricted either to walls, e.g. partitions, or floors or ceilings or roofs
- E04B1/62—Insulation or other protection; Elements or use of specified material therefor
- E04B1/74—Heat, sound or noise insulation, absorption, or reflection; Other building methods affording favourable thermal or acoustical conditions, e.g. accumulating of heat within walls
- E04B1/82—Heat, sound or noise insulation, absorption, or reflection; Other building methods affording favourable thermal or acoustical conditions, e.g. accumulating of heat within walls specifically with respect to sound only
- E04B1/84—Sound-absorbing elements
- E04B1/86—Sound-absorbing elements slab-shaped
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B3/00—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form
- B32B3/10—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form characterised by a discontinuous layer, i.e. formed of separate pieces of material
- B32B3/12—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form characterised by a discontinuous layer, i.e. formed of separate pieces of material characterised by a layer of regularly- arranged cells, e.g. a honeycomb structure
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- G—PHYSICS
- G10—MUSICAL INSTRUMENTS; ACOUSTICS
- G10K—SOUND-PRODUCING DEVICES; METHODS OR DEVICES FOR PROTECTING AGAINST, OR FOR DAMPING, NOISE OR OTHER ACOUSTIC WAVES IN GENERAL; ACOUSTICS NOT OTHERWISE PROVIDED FOR
- G10K11/00—Methods or devices for transmitting, conducting or directing sound in general; Methods or devices for protecting against, or for damping, noise or other acoustic waves in general
- G10K11/16—Methods or devices for protecting against, or for damping, noise or other acoustic waves in general
- G10K11/172—Methods or devices for protecting against, or for damping, noise or other acoustic waves in general using resonance effects
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2307/00—Properties of the layers or laminate
- B32B2307/10—Properties of the layers or laminate having particular acoustical properties
- B32B2307/102—Insulating
-
- E—FIXED CONSTRUCTIONS
- E04—BUILDING
- E04B—GENERAL BUILDING CONSTRUCTIONS; WALLS, e.g. PARTITIONS; ROOFS; FLOORS; CEILINGS; INSULATION OR OTHER PROTECTION OF BUILDINGS
- E04B1/00—Constructions in general; Structures which are not restricted either to walls, e.g. partitions, or floors or ceilings or roofs
- E04B1/62—Insulation or other protection; Elements or use of specified material therefor
- E04B1/74—Heat, sound or noise insulation, absorption, or reflection; Other building methods affording favourable thermal or acoustical conditions, e.g. accumulating of heat within walls
- E04B2001/742—Use of special materials; Materials having special structures or shape
- E04B2001/748—Honeycomb materials
-
- E—FIXED CONSTRUCTIONS
- E04—BUILDING
- E04B—GENERAL BUILDING CONSTRUCTIONS; WALLS, e.g. PARTITIONS; ROOFS; FLOORS; CEILINGS; INSULATION OR OTHER PROTECTION OF BUILDINGS
- E04B1/00—Constructions in general; Structures which are not restricted either to walls, e.g. partitions, or floors or ceilings or roofs
- E04B1/62—Insulation or other protection; Elements or use of specified material therefor
- E04B1/74—Heat, sound or noise insulation, absorption, or reflection; Other building methods affording favourable thermal or acoustical conditions, e.g. accumulating of heat within walls
- E04B1/82—Heat, sound or noise insulation, absorption, or reflection; Other building methods affording favourable thermal or acoustical conditions, e.g. accumulating of heat within walls specifically with respect to sound only
- E04B1/84—Sound-absorbing elements
- E04B2001/8423—Tray or frame type panels or blocks, with or without acoustical filling
- E04B2001/8428—Tray or frame type panels or blocks, with or without acoustical filling containing specially shaped acoustical bodies, e.g. funnels, egg-crates, fanfolds
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- E—FIXED CONSTRUCTIONS
- E04—BUILDING
- E04B—GENERAL BUILDING CONSTRUCTIONS; WALLS, e.g. PARTITIONS; ROOFS; FLOORS; CEILINGS; INSULATION OR OTHER PROTECTION OF BUILDINGS
- E04B1/00—Constructions in general; Structures which are not restricted either to walls, e.g. partitions, or floors or ceilings or roofs
- E04B1/62—Insulation or other protection; Elements or use of specified material therefor
- E04B1/74—Heat, sound or noise insulation, absorption, or reflection; Other building methods affording favourable thermal or acoustical conditions, e.g. accumulating of heat within walls
- E04B1/82—Heat, sound or noise insulation, absorption, or reflection; Other building methods affording favourable thermal or acoustical conditions, e.g. accumulating of heat within walls specifically with respect to sound only
- E04B1/84—Sound-absorbing elements
- E04B2001/8423—Tray or frame type panels or blocks, with or without acoustical filling
- E04B2001/8433—Tray or frame type panels or blocks, with or without acoustical filling with holes in their face
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/24—Structurally defined web or sheet [e.g., overall dimension, etc.]
- Y10T428/24149—Honeycomb-like
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/24—Structurally defined web or sheet [e.g., overall dimension, etc.]
- Y10T428/24273—Structurally defined web or sheet [e.g., overall dimension, etc.] including aperture
Definitions
- Permeable sheet materials are widely used in the construction of sound absorptive panels. When used as a facing over a compartmented airspace, such materials are known as laminar absorbers. Such a structure has the property that the resistive component of its acoustic impedance is essentially constant and is not a function of frequency.
- Typical laminar sound absorbers of the prior art are disclosed in U.S. Pat. Nos. 3,502,171 to Cowan and 3,507,355 to Lawson.
- a typical acoustic face sheet is also shown in U.S. Pat. No. 3,700,067 to Dobbs et al.
- These prior art devices do not yield the desired, previously-discussed, property whereby the resistance component of the acoustic impedance is a desired function of frequency.
- an apertured facing sheet in which the resistance component of the acoustic impedance is completely controllable.
- the structure comprises apermeable facing sheet modified by the addition of an array of ducted ports of specified dimensions.
- This facing used over any of several types of air-cavity structures, provides a lower tuning frequency without the usual highfrequency rolloff penalty. It closely follows an ideal facing sheet in that it is characterized by a resistance that increases with frequency and a large initial inertance (inductance) that decreases rapidly toward zero as frequency increases.
- FIG. l is a perspective view of a first embodiment showing the facing Asheet constructed in accordance with the invention together with a back panel and a cavity-type structure interposed therebetween.
- FIG. 2 is a side cross-sectional view of a single collared aperture, constructed in accordance with a second embodiment of the invention.
- FIG. 3 is a side cross-sectional view of a third embodiment of the invention.
- FIG. 4' is a schematic diagram of an equivalent electrical circuit network, useful in the exposition of the invention.
- a typical embodiment comprises a sheet l of permeable material having a relatively large flow resistance.
- the flow resistance is ten times the characteristic impedance of the fluid in which the device is to operate.
- the permeable sheet l may be fabricated from sintered or felted metal, paper, woven or felted fibers, or other similar porous materials.
- the sheet l is provided with regularly-spaced apertures or perforations therethrough, a typical one of which is indicated at 2.
- each perforation (2) is provided with a tubular collar such as shown at 3 which extends from one side of the sheet and in registration with the corresponding perforation.
- each straight-through passage in the sheet l has an effective length 4 which is considerably greater than the thickness 5 of the sheet 1.
- the facing sheet with its integral collared apertures comprises the essence of the invention; however, it should be understood that the invention is especially useful in conjunction with a laminar absorber, or other compartmented airspace type of sound absorber, such as shown in U.S. Pat. No. 3,734,234 entitled Sound Absorption Structure, of common assignee herewith.
- FIG. l shows the present invention as used in conjunction with the aforesaid compartmented sound absorber.
- This assembly comprises impermeable backing sheet 6, impermeable wall members (typically such as those indicated at 7 and 8) which divide the device into a plurality of cellular compartments, and oblique permeable partitions 9 and l0 located within a compartment.
- the structure comprising elements 6-10 has the properties that the resistive component of its acoustic impedance is essentially constant and is not a function of frequency. This is in contradistinction to the property of the present invention wherein the acoustic resistance is proportional to frequency and the acoustic inertance is inversely proportional to frequency.
- the acoustical behavior of the above-described assembly may be best understood in terms of its acoustical elements and their electrical analogs. Circuit elements and their acoustic analogs are listed below:
- FIG. 2 There is shown in FIG. 2 a detailed portion of a second embodiment of the invention comprising a perforated structure having 50 percent open perforations in the planar, or sheet portion 12 of the structure. Typical perforations are indicated at 13 and 14. At spaced intervals, a depending hollow collar portion 15 extends downwardly from the bottom face of the sheet portion 12. A porous, or permeable, outer lamina overlies, or is bonded to, sheet portion 12. The outer lamina 16 is provided with apertures, such as the one indicated at 17, which are coaxially aligned with the passage 18 through collar portion 15. The described structural elements are repeated at fixed regular spacings in the manner shown in FIG. 1. The lamina 16 provides part of the desired flow resistance; the remaining part of the flow resistance is provided by sheet portion 12.
- FIG. 3 an alternative construction which is functionally the equivalent of the structure shown in FIG. 2.
- This embodiment comprises a twopart laminated sheet comprising flow resistive lamina 19 and 50 percent open perforate lamina 20.
- a rivetlike hollow tubular element 21 extends through the laminated sheet (19-20) and has its upper flange end 22 flush with the outer surface of lamina 19 and its lower end extending beyond the outer surface of lamina 20.
- the dependent end of the tubular element 2l may bel chamfered as shown in FIG. 3 to permit the element to be driven through the laminated sheet (19-20) by a suitable tool (not shown) in order to installthe element.
- suitable tool not shown
- Other suitable manufacturing techniques will be apparent to those versed in the art, it being only necessary that the effective length of the passage through the tubular element be considerablyv greater than the thickness of the laminated structure through which it extends.
- FIG. 4 The electrical network analog of an area of the sheet is shown in FIG. 4.
- a large resistance R1 is connected in parallel with several other circuit branches.
- Each of the circuit branches consists of a small resistance, nR2, in series with an inductance, nL2, when n is the number of such side branches (per unit area).
- the impedance of the nth resistance and inductance is the series combination of the two; therefore:
- the inductive side branches are all in parallel so the total impedance of the side branches per unit area is:
- R, and Z2 are also in parallel circuits and thus are combined by adding their admittances:
- the resistance is about R2 at low frequencies and about R1 at high frequencies.
- the inductance is also a function of frequency and tends to vanish at high frequency:
- the acoustic resistance of the permeable sheet l without the tubular collar 3 corresponds to R1
- the small acoustical resistance in each collared hole corresponds to nR2
- the acoustic nertance of the mass of air in the tubular passages (3) corresponds to nL2.
- Each acoustic resistance, nR2, is is series with nertance, nL2.
- the large acoustic resistance R1 is in parallel with all the side branches exactly as in the electrical analogy.
- the parallel branches need not be identical to each other.
- the essence of the invention is the paralleling of acoustic elements in the facing sheet such that the end effect is a resistance which increases with frequency.
- the decreasing value of net nertance is also a desirable characteristic since it means that, for example, a laminar absorber to be applied as a facing will have an unusually low first resonant frequency, but at higher frequencies the nertance will become small such that the high frequency performance is not impaired.
- the value R1 is controlled by the composition of the permeable sheet per se.
- the value nR2 is controlled by the size of the perforations (2) through the sheet (l) and their depth.
- the value nL2 is controlled by the size and length of the collared apertures (3). It is preferred that the perforations through the sheet (and their various coaxial passages) be quite closely spaced compared to a wavelength of the highest frequency of interest.
- Table I sets forth comparative test results which illustrate normal incidence sound absorption coefficients, as a function of frequency, obtained for various acoustical facings.
- the sound absorption coefficients were measured by means of a commercial Bruel and Kjaer Standing Wave Apparatus, using the standard test procedure set forth by ASTM C-3 84-5 8.
- the test specimens were assembled from the following components:
- a brass tubular collar having an inner diameter of 0.22 inch and a length 0.290 inch; and,
- the specimens were assembled into a standard Bruel and Kjaer variable depth specimen holder with the l inch deep fiberglass main body absorber being spaced first at 1A inch from the permeable facing sheet for the first series of tests, and then at l inch from the permeable facing sheet for the second series of tests.
- the l inch thick fiberglass material comprises the conventional main body absorber with which the novel facing sheet of the invention cooperates. This is the functional equivalent of the structure comprising elements 6-10.
- the following three test configurations are representative of three separate structural designs each intended to provide good low frequency absorption in a limited space.
- the first design identified as Type A, comprises a resistive permeable facing sheet overlaying a main-body absorber, and is typical of acoustical panels such as shown in U.S. Pat. No. 3,712,846.
- the second design identified as Type B, comprises an impermeable facing sheet with spaced apertures therethrough overlying a main-body absorber, and is typical of devices such as shown in U.S. Pat. No. 3,174,580.
- the third design identified as Type C, is constructed in accordance with the present invention.
- the facing sheet structure of the present invention comprises a collared aperture and the resistive facing sheet in acoustically parallel combination.
- the resulting absorption coefficient spectra shows a substantial improvement in low-frequency response as compared to the Type-A configuration, and also an improved high-frequency response as compared to either the Type-B configuration or the Type-A configuration. These improvements are equally apparent in the case of either the 2 inch depth or the 1.25 inch depth.
- the improved response of the present invention results directly from the fact that it provides both inertance and resistance that vary with frequency in a desirable and useful way.
- the inertance 1 of the Helmholtz resonator is constant.
- the constantly increasing reactance results in the rapid deterioration of the high-frequency absorption, because the large positive reactance reflects the sound and does not permit it to enter the cavity.
- the resistive facing alone broadens the frequency response of the fiberglass by extending it to lower frequencies but can do so only at the expense of higher frequency absorption.
- the present invention provides a large value of inertance to move the initial peak downward in frequency. As frequency increases, however, the inertance diminishes smoothly and rapidly such that the highfrequency response is not impaired.
- the resistance of the present invention asymptotically rises to that of the facing hseet alone as its inertance vanishes. Note in the date of Table l that the absorption coefficients of the Type-C and the Type-A converge at the highest frequency.
- FIGS. 1-3 apparatus having broadband absorption extending to moderately low frequencies and for which the allowable space is constrained.
- each of said passage providing means comprises:
- each of said passage providing means comprises:
- R +jwL finite lumped acoustic impedance of said facing
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Abstract
An acoustical facing sheet comprising a permeable member having perforations therethrough and tubular elements extending therefrom on one side in register with said perforations. The structure provides a lumped acoustic impedance having an acoustic resistance proportional to frequency, and an acoustic inertance that is inversely proportional to frequency. It permits the design of highly efficient laminar-type sound attenuating panel structures having an unusually low first resonant frequency without impairing performance at the higher frequencies, and occupying smaller volume than prior devices.
Description
[45] June 25, 1974 United States Patent [191 Wirt et al.
XXX GGG 333 333 S UHU N www@ NUT m m m A mmmme.. W H :MP A .m m m R O mm n amaN HJD E T mmmA 999 P Mmmm m O F [54] CONTROLLABLE LAMINAR SOUND 3,525,663 ABSORPTIVE STRUCTURE /gg [75] Inventors: Leslie Spencer Wirt, Newhall; 7
Duane Lloyd Morrow, Saugus, both of Calif.
[73] Assignee: Lockheed Aircraft Corporation,
Burbank, Calif.
Apr. 27, 1973 Appl. No.: 355,161
Assistant Examiner-Vit W. Miska [22] Filed:
Attorney, Agent, or Firm-Billy G. Corber; Ralph M. Flygare ABSTRACT [52] U.S. 181/33 G,
l CONTROLLABLE LAMINAR SOUND ABSORPTIVE STRUCTURE BACKGROUND OF THE INVENTION Permeable sheet materials are widely used in the construction of sound absorptive panels. When used as a facing over a compartmented airspace, such materials are known as laminar absorbers. Such a structure has the property that the resistive component of its acoustic impedance is essentially constant and is not a function of frequency.
It has been discovered from an examination of the solutions to certain wave equations that attenuation in acoustically treated ducts could be singifcantly improved if the acoustic resistance of the duct walls were a particular function of the frequency to be attenuated. The optimum value of the resistance starts at a predetermined value at low frequencies and increases uniformly with increasing frequency to within a predetermined value at the maximum frequency of interest. In the case of an aircraft turbine-engine inlet, to attenuate the highest frequency the resistance desired may be eight times the resistance desired to attenuate the lowest frequency, Materials of the prior art have not been able to provide these properties.
Typical laminar sound absorbers of the prior art are disclosed in U.S. Pat. Nos. 3,502,171 to Cowan and 3,507,355 to Lawson. A typical acoustic face sheet is also shown in U.S. Pat. No. 3,700,067 to Dobbs et al. These prior art devices do not yield the desired, previously-discussed, property whereby the resistance component of the acoustic impedance is a desired function of frequency.
SUMMARY OF THE PRESENT INVENTION There is provided by the present invention an apertured facing sheet in which the resistance component of the acoustic impedance is completely controllable. Thus, it may be tailored to be optimum for any given application. The structure comprises apermeable facing sheet modified by the addition of an array of ducted ports of specified dimensions. This facing, used over any of several types of air-cavity structures, provides a lower tuning frequency without the usual highfrequency rolloff penalty. It closely follows an ideal facing sheet in that it is characterized by a resistance that increases with frequency and a large initial inertance (inductance) that decreases rapidly toward zero as frequency increases.
BRIEF DESCRIPTION OF THE DRAWINGS FIG. l is a perspective view of a first embodiment showing the facing Asheet constructed in accordance with the invention together with a back panel and a cavity-type structure interposed therebetween.
FIG. 2 is a side cross-sectional view of a single collared aperture, constructed in accordance with a second embodiment of the invention.
FIG. 3 is a side cross-sectional view of a third embodiment of the invention.
FIG. 4'is a schematic diagram of an equivalent electrical circuit network, useful in the exposition of the invention.
DETAILED DESCRIPTION OF ILLUSTRATIVE EMBODIMENTS Referring to the structure shown in FIG. l, a typical embodiment comprises a sheet l of permeable material having a relatively large flow resistance. Typically the flow resistance is ten times the characteristic impedance of the fluid in which the device is to operate. The permeable sheet l may be fabricated from sintered or felted metal, paper, woven or felted fibers, or other similar porous materials. The sheet l is provided with regularly-spaced apertures or perforations therethrough, a typical one of which is indicated at 2. Although the exemplary embodiment of FIG. l shows a pattern of perforations arrayed in an orthogonal grid, it should be understood that other patterns or even random arrangements of the perforations may be employed. Also, the percentage of open area is a design parameter that may vary over a considerable range. The perforations, whether they be in a straight or staggered line may be of various shapes such as round, square, slotted, or of complex decorative shape. Each perforation (2) is provided with a tubular collar such as shown at 3 which extends from one side of the sheet and in registration with the corresponding perforation. Thus, each straight-through passage in the sheet l has an effective length 4 which is considerably greater than the thickness 5 of the sheet 1.
The facing sheet with its integral collared apertures comprises the essence of the invention; however, it should be understood that the invention is especially useful in conjunction with a laminar absorber, or other compartmented airspace type of sound absorber, such as shown in U.S. Pat. No. 3,734,234 entitled Sound Absorption Structure, of common assignee herewith.
FIG. l shows the present invention as used in conjunction with the aforesaid compartmented sound absorber. This assembly comprises impermeable backing sheet 6, impermeable wall members (typically such as those indicated at 7 and 8) which divide the device into a plurality of cellular compartments, and oblique permeable partitions 9 and l0 located within a compartment. The structure comprising elements 6-10 has the properties that the resistive component of its acoustic impedance is essentially constant and is not a function of frequency. This is in contradistinction to the property of the present invention wherein the acoustic resistance is proportional to frequency and the acoustic inertance is inversely proportional to frequency.
The acoustical behavior of the above-described assembly may be best understood in terms of its acoustical elements and their electrical analogs. Circuit elements and their acoustic analogs are listed below:
Electrical Acoustical Common Symbol Resistance Resistance R lnductance lnertance L Capacitance Capacitance C meable facing sheets, R and L are approximate constants, independent of frequency.
There is shown in FIG. 2 a detailed portion of a second embodiment of the invention comprising a perforated structure having 50 percent open perforations in the planar, or sheet portion 12 of the structure. Typical perforations are indicated at 13 and 14. At spaced intervals, a depending hollow collar portion 15 extends downwardly from the bottom face of the sheet portion 12. A porous, or permeable, outer lamina overlies, or is bonded to, sheet portion 12. The outer lamina 16 is provided with apertures, such as the one indicated at 17, which are coaxially aligned with the passage 18 through collar portion 15. The described structural elements are repeated at fixed regular spacings in the manner shown in FIG. 1. The lamina 16 provides part of the desired flow resistance; the remaining part of the flow resistance is provided by sheet portion 12.
There is shownin FIG. 3 an alternative construction which is functionally the equivalent of the structure shown in FIG. 2. This embodiment comprises a twopart laminated sheet comprising flow resistive lamina 19 and 50 percent open perforate lamina 20. A rivetlike hollow tubular element 21 extends through the laminated sheet (19-20) and has its upper flange end 22 flush with the outer surface of lamina 19 and its lower end extending beyond the outer surface of lamina 20. The dependent end of the tubular element 2l may bel chamfered as shown in FIG. 3 to permit the element to be driven through the laminated sheet (19-20) by a suitable tool (not shown) in order to installthe element. Other suitable manufacturing techniques will be apparent to those versed in the art, it being only necessary that the effective length of the passage through the tubular element be considerablyv greater than the thickness of the laminated structure through which it extends.
The electrical network analog of an area of the sheet is shown in FIG. 4. A large resistance R1 is connected in parallel with several other circuit branches. Each of the circuit branches consists of a small resistance, nR2, in series with an inductance, nL2, when n is the number of such side branches (per unit area).
The impedance of the nth resistance and inductance is the series combination of the two; therefore:
The inductive side branches are all in parallel so the total impedance of the side branches per unit area is:
But, R, and Z2 are also in parallel circuits and thus are combined by adding their admittances:
The trends of the circuit response may be visualized by noting the limiting cases:
w 00 Thus, the resistance is about R2 at low frequencies and about R1 at high frequencies. The inductance is also a function of frequency and tends to vanish at high frequency:
and for R, R2
Lim L L2 and for all values of R1 Lim L 0 By direct analogy, the acoustic resistance of the permeable sheet l without the tubular collar 3 (as shown in FIG. l) corresponds to R1, the small acoustical resistance in each collared hole corresponds to nR2 and the acoustic nertance of the mass of air in the tubular passages (3) corresponds to nL2. Each acoustic resistance, nR2, is is series with nertance, nL2. The large acoustic resistance R1 is in parallel with all the side branches exactly as in the electrical analogy.
Thus, it will be seen that a wide range of variations is possible. For example, in a practical construction permeable sheet materials may be fabricated which actually contain a small series inertance which has been neglected in the above-discussed analysis for the sake of simplicity.
The parallel branches need not be identical to each other. The essence of the invention is the paralleling of acoustic elements in the facing sheet such that the end effect is a resistance which increases with frequency. The decreasing value of net nertance is also a desirable characteristic since it means that, for example, a laminar absorber to be applied as a facing will have an unusually low first resonant frequency, but at higher frequencies the nertance will become small such that the high frequency performance is not impaired. By separately designing R1, and nR2, and nL2, a wide range of characteristics may be obtained.
The value R1 is controlled by the composition of the permeable sheet per se. The value nR2 is controlled by the size of the perforations (2) through the sheet (l) and their depth. The value nL2 is controlled by the size and length of the collared apertures (3). It is preferred that the perforations through the sheet (and their various coaxial passages) be quite closely spaced compared to a wavelength of the highest frequency of interest.
Table I below sets forth comparative test results which illustrate normal incidence sound absorption coefficients, as a function of frequency, obtained for various acoustical facings. The sound absorption coefficients were measured by means of a commercial Bruel and Kjaer Standing Wave Apparatus, using the standard test procedure set forth by ASTM C-3 84-5 8. The test specimens were assembled from the following components:
l. Permeable felted metal facing having a throughflow resistance of cgs rayls;
2. A brass tubular collar having an inner diameter of 0.22 inch and a length 0.290 inch; and,
3. An absorptive main body of l inch thick fiberglass.
The specimens were assembled into a standard Bruel and Kjaer variable depth specimen holder with the l inch deep fiberglass main body absorber being spaced first at 1A inch from the permeable facing sheet for the first series of tests, and then at l inch from the permeable facing sheet for the second series of tests. The l inch thick fiberglass material comprises the conventional main body absorber with which the novel facing sheet of the invention cooperates. This is the functional equivalent of the structure comprising elements 6-10.
The following three test configurations are representative of three separate structural designs each intended to provide good low frequency absorption in a limited space. The first design, identified as Type A, comprises a resistive permeable facing sheet overlaying a main-body absorber, and is typical of acoustical panels such as shown in U.S. Pat. No. 3,712,846. The second design, identified as Type B, comprises an impermeable facing sheet with spaced apertures therethrough overlying a main-body absorber, and is typical of devices such as shown in U.S. Pat. No. 3,174,580. The third design, identified as Type C, is constructed in accordance with the present invention.
PRIOR ART TYPE B An alternate, and well-known, approach to a low frequency problem is the Helmholtz resonator such as shown in U.S. Pat. No. 3,174,580 to Schultz. The resonator contains supplemental resistive material such as fiberglass in the cavity. An example of the large inertance (acoustical inertia) in the collared hole in series combination with the resonator airspace provides a low frequency absorption peak, but results in a nearly total loss of high frequency absorption. This is clearly illustrated in the data of Table I. The absorption spectra consists of single peaks a 0.86 at 400 Hz for the 2 inch depth and a 0.99 at 500 Hz for the 1.25 inch depth. Clearly such prior art design is most useful for the absorption of a single pure tone.
PRESENT INVENTION TYPE C The facing sheet structure of the present invention comprises a collared aperture and the resistive facing sheet in acoustically parallel combination. The resulting absorption coefficient spectra, as indicated in Table l, shows a substantial improvement in low-frequency response as compared to the Type-A configuration, and also an improved high-frequency response as compared to either the Type-B configuration or the Type-A configuration. These improvements are equally apparent in the case of either the 2 inch depth or the 1.25 inch depth.
The improved response of the present invention (Type-C) results directly from the fact that it provides both inertance and resistance that vary with frequency in a desirable and useful way. The inertance 1 of the Helmholtz resonator is constant. As a result, the positive reactance wl (w 21rf, f= frequency) increases in direct proportion to frequency. At some value of frequency this reactance cancels the negative reactance of the airspace and creates a resonant response. At all higher frequencies the constantly increasing reactance results in the rapid deterioration of the high-frequency absorption, because the large positive reactance reflects the sound and does not permit it to enter the cavity.
The resistive facing alone broadens the frequency response of the fiberglass by extending it to lower frequencies but can do so only at the expense of higher frequency absorption.
The present invention provides a large value of inertance to move the initial peak downward in frequency. As frequency increases, however, the inertance diminishes smoothly and rapidly such that the highfrequency response is not impaired. The resistance of the present invention asymptotically rises to that of the facing hseet alone as its inertance vanishes. Note in the date of Table l that the absorption coefficients of the Type-C and the Type-A converge at the highest frequency.
In summary, there is provided by the structures shown in FIGS. 1-3, apparatus having broadband absorption extending to moderately low frequencies and for which the allowable space is constrained.
It will be apparent to those versed in the art that various modifications may be made to the representative embodiments of the invention shown and described above.
What is claimed is:
l. An acoustical facing for a laminar sound absorber of the type comprising an array of open-ended resonant compartments, said facing comprising:
a sheet of permeable material through which have been fonned a multiplicity of holes, said holes '7 being smaller than the open ends of said compartments and spaced apart for registration with said open ends; and,
a multiplicity of means for providing a passage which extends from each of said holes into a corresponding compartment of said array.
2. An acoustical facing as defined in claim 1 wherein the material comprising said permeable sheet is characterized by having a finite lumped acoustic impedance which is predominantly resistive.
3. An acoustical facing as defined in claim l wherein said passage providing means are characterized by having a lumped acoustic impedance which is partly resistive and partly positive reactive.
4. An acoustical facing as defined in claim l wherein the material comprising said permeable sheet is characterized by having a finite lumped acoustic impedance which is predominantly resistive, and wherein said passage providing means are characterized by having a lumped acoustic impedance which is partly resistive and partly positive reactive, and whereby the lumped acoustic impedances of said permeable sheet and said passage providing means are in parallel to the flow of acoustic energy.
5. An acoustical facing as defined in claim l wherein said sheet of permeable material comprises:
a first planar lamina of porous material; and
a second lamina, co-planar with said first lamina,
having open perforations therethrough.
6. An acoustical facing as defined in claim 5 wherein 8 i i each of said passage providing means comprises:
an outwardly extending hollow collar integral with said second lamina.
7. An acoustical facing as defined in claim 5 wherein each of said passage providing means comprises:
a hollow tubular element extending through said first and second laminae.
8. An acoustical facing as defined in claim 1 wherein the cross-sectional area of each of said passage providing means is substantially coextensive with the crosssectional area of its corresponding hole.
9. An acoustical facing as defined in claim l wherein the axis of the passage through each of said passage providing means is normal to said sheet.
10. An acoustical facing as defined in claim l wherein said holes are of uniform size.
1l. An acoustical facing as defined in claim 1 wherein said holes are circular and said passage providing means are cylindrical.
12. An acoustical facing as defined in claim l wherein the finite lumped acoustic impedance of said facing, defined as R +jwL, is a predetermined function of the angular frequency w such that R increases monotonically with frequency and wL first increases, and then decreases as frequency increases; where R is the resistive component of said impedance, j is l, w is two 1r times the frequency of interest, and L is the acoustic inertance of said facing.
Claims (12)
1. An acoustical facing for a laminar sound absorber of the type comprising an array of open-ended resonant compartments, said facing comprising: a sheet of permeable material through which have been formed a multiplicity of holes, said holes being smaller than the open ends of said compartments and spaced apart for registration with said open ends; and, a multiplicity of means for providing a passage which extends from each of said holes into a corresponding compartment of said array.
2. An acoustical facing as defined in claim 1 wherein the material comprising said permeable sheet is characterized by having a finite lumped acoustic impedance which is predominantly resistive.
3. An acoustical facing as defined in claim 1 wherein said passage providing means are characterized by having a lumped acoustic impedance which is partly resistive and partly positive reactive.
4. An acoustical facing as defined in claim 1 wherein the material comprising said permeable sheet is characterized by having a finite lumped acoustic impedance which is predominantly resistive, and wherein said passage providing means are characterized by having a lumped acoustic impedance which is partly resistive and partly positive reactive, and whereby the lumped acoustic impedances of said permeable sheet and said passage providing means are in parallel to the flow of acoustic energy.
5. An acoustical facing as defined in claim 1 wherein said sheet of permeable material comprises: a first planar lamina of porous material; and a second lamina, co-planar with said first lamina, having open perforations therethrough.
6. An acoustical facing as defined in claim 5 wherein each of said passage providing means comprises: an outwardly extending hollow collar integral with said second lamina.
7. An acoustical facing as defined in claim 5 wherein each of said passage providing means comprises: a hollow tubular element extending through said first and second laminae.
8. An acoustical facing as defined in claim 1 wherein the cross-sectional area of each of said passage providing means is substantially coextensive with the cross-sectional area of its corresponding hole.
9. An acoustical facing as defined in claim 1 wherein the axis of the passage through each of said passage providing means is normal to said sheet.
10. An acoustical facing as defined in claim 1 wherein said holes are of uniform size.
11. An acoustical facing as defined in claim 1 wherein said holes are circular and said passage providing means are cylindrical.
12. An acoustical facing as defined in claim 1 wherein the finite lumped acoustic impedance of said facing, defined as R + j omega L, is a predetermined function of the angular frequency omega such that R increases monotonically with frequency and omega L first increases, and then decreases as frequency increases; Where R is the resistive component of said impedance, j is Square Root -1, omega is two pi times the frequency of interest, and L is the acoustic inertance of said facing.
Priority Applications (1)
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US00355161A US3819007A (en) | 1973-04-27 | 1973-04-27 | Controllable laminar sound absorptive structure |
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US00355161A US3819007A (en) | 1973-04-27 | 1973-04-27 | Controllable laminar sound absorptive structure |
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US3819007A true US3819007A (en) | 1974-06-25 |
Family
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US00355161A Expired - Lifetime US3819007A (en) | 1973-04-27 | 1973-04-27 | Controllable laminar sound absorptive structure |
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FR2362461A1 (en) * | 1976-08-19 | 1978-03-17 | United Technologies Corp | ACOUSTIC COATINGS TO ABSORB SOUNDS |
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US4100993A (en) * | 1976-04-15 | 1978-07-18 | United Technologies Corporation | Acoustic liner |
US4150732A (en) * | 1977-01-11 | 1979-04-24 | Societe Nationale D'etude Et De Construction De Moteurs D'aviation | Resonant cavity devices for reducing noise within a duct in the presence of a gaseous fluid |
US4189027A (en) * | 1976-08-19 | 1980-02-19 | United Technologies Corporation | Sound suppressor liners |
US4231447A (en) * | 1978-04-29 | 1980-11-04 | Rolls-Royce Limited | Multi-layer acoustic linings |
US4319661A (en) * | 1978-09-20 | 1982-03-16 | The Proudfoot Company, Inc. | Acoustic space absorber unit |
EP0352993A1 (en) * | 1988-07-25 | 1990-01-31 | Short Brothers Plc | Noise attenuation panel |
US4944362A (en) * | 1988-11-25 | 1990-07-31 | General Electric Company | Closed cavity noise suppressor |
US5100730A (en) * | 1989-11-16 | 1992-03-31 | Lambers Thomas J | Structural reinforcement apparatus and method of making same |
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US5491307A (en) * | 1990-10-05 | 1996-02-13 | Mcdonnell Douglas Corporation | Porous single expansion ramp |
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US6371240B1 (en) * | 2000-03-18 | 2002-04-16 | Austin Acoustic Systems, Inc. | Anechoic chamber |
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US9978354B2 (en) * | 2016-04-15 | 2018-05-22 | Rohr, Inc. | Acoustic panel with vertical stiffeners |
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US10280839B2 (en) * | 2014-09-24 | 2019-05-07 | Safran Aircraft Engines | Acoustic treatment panel |
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US11242822B2 (en) | 2018-12-14 | 2022-02-08 | Rohr, Inc. | Structured panel with multi-panel structure(s) |
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US11434826B2 (en) * | 2018-09-10 | 2022-09-06 | Safran Aircraft Engines | Acoustic treatment panel for a turbojet engine |
US20220389882A1 (en) * | 2021-06-03 | 2022-12-08 | General Electric Company | Acoustic cores and tools and methods for forming the same |
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Citations (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2280631A (en) * | 1938-06-16 | 1942-04-21 | Burgess Battery Co | Facing sheet for sound absorbing material |
GB732079A (en) * | 1951-12-18 | 1955-06-15 | Eugene Carl Henry Becker | Improvements in a panel for absorbing acoustic energy |
US2755882A (en) * | 1952-04-22 | 1956-07-24 | Maccaferri Mario | Acoustic tiles |
US2984312A (en) * | 1959-04-24 | 1961-05-16 | Owens Corning Fiberglass Corp | Acoustical wall board |
US3161385A (en) * | 1960-06-15 | 1964-12-15 | Coleman Kramer Inc | Means and method for stabilizing laminar boundary layer flow |
US3174580A (en) * | 1961-04-28 | 1965-03-23 | Kurt W Schulz | Acoustical tile construction |
US3227598A (en) * | 1960-12-02 | 1966-01-04 | Wayne F Robb | Core structure |
US3231454A (en) * | 1961-04-14 | 1966-01-25 | Cadillac Products | Cushioning material |
GB1147492A (en) * | 1967-04-07 | 1969-04-02 | Acoustics And Architecture Ltd | Sound absorbing device |
US3525663A (en) * | 1967-03-09 | 1970-08-25 | Jesse R Hale | Anticlastic cellular core structure having biaxial rectilinear truss patterns |
US3622430A (en) * | 1969-11-24 | 1971-11-23 | Peter L Jurisich | Dimpled sheet structural laminate |
US3712846A (en) * | 1971-06-23 | 1973-01-23 | Carpenter L & Co | Acoustical panel |
-
1973
- 1973-04-27 US US00355161A patent/US3819007A/en not_active Expired - Lifetime
Patent Citations (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2280631A (en) * | 1938-06-16 | 1942-04-21 | Burgess Battery Co | Facing sheet for sound absorbing material |
GB732079A (en) * | 1951-12-18 | 1955-06-15 | Eugene Carl Henry Becker | Improvements in a panel for absorbing acoustic energy |
US2755882A (en) * | 1952-04-22 | 1956-07-24 | Maccaferri Mario | Acoustic tiles |
US2984312A (en) * | 1959-04-24 | 1961-05-16 | Owens Corning Fiberglass Corp | Acoustical wall board |
US3161385A (en) * | 1960-06-15 | 1964-12-15 | Coleman Kramer Inc | Means and method for stabilizing laminar boundary layer flow |
US3227598A (en) * | 1960-12-02 | 1966-01-04 | Wayne F Robb | Core structure |
US3231454A (en) * | 1961-04-14 | 1966-01-25 | Cadillac Products | Cushioning material |
US3174580A (en) * | 1961-04-28 | 1965-03-23 | Kurt W Schulz | Acoustical tile construction |
US3525663A (en) * | 1967-03-09 | 1970-08-25 | Jesse R Hale | Anticlastic cellular core structure having biaxial rectilinear truss patterns |
GB1147492A (en) * | 1967-04-07 | 1969-04-02 | Acoustics And Architecture Ltd | Sound absorbing device |
US3622430A (en) * | 1969-11-24 | 1971-11-23 | Peter L Jurisich | Dimpled sheet structural laminate |
US3712846A (en) * | 1971-06-23 | 1973-01-23 | Carpenter L & Co | Acoustical panel |
Cited By (89)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4084367A (en) * | 1975-11-14 | 1978-04-18 | Haworth Mfg., Inc. | Sound absorbing panel |
US4084366A (en) * | 1975-11-14 | 1978-04-18 | Haworth Mfg., Inc. | Sound absorbing panel |
US4100993A (en) * | 1976-04-15 | 1978-07-18 | United Technologies Corporation | Acoustic liner |
FR2362461A1 (en) * | 1976-08-19 | 1978-03-17 | United Technologies Corp | ACOUSTIC COATINGS TO ABSORB SOUNDS |
US4135603A (en) * | 1976-08-19 | 1979-01-23 | United Technologies Corporation | Sound suppressor liners |
US4189027A (en) * | 1976-08-19 | 1980-02-19 | United Technologies Corporation | Sound suppressor liners |
US4150732A (en) * | 1977-01-11 | 1979-04-24 | Societe Nationale D'etude Et De Construction De Moteurs D'aviation | Resonant cavity devices for reducing noise within a duct in the presence of a gaseous fluid |
US4231447A (en) * | 1978-04-29 | 1980-11-04 | Rolls-Royce Limited | Multi-layer acoustic linings |
US4319661A (en) * | 1978-09-20 | 1982-03-16 | The Proudfoot Company, Inc. | Acoustic space absorber unit |
US5543198A (en) * | 1988-07-25 | 1996-08-06 | Short Brothers Plc | Noise attenuation panel |
WO1990000968A1 (en) * | 1988-07-25 | 1990-02-08 | Short Brothers Plc | Noise attenuation panel |
EP0352993A1 (en) * | 1988-07-25 | 1990-01-31 | Short Brothers Plc | Noise attenuation panel |
US4944362A (en) * | 1988-11-25 | 1990-07-31 | General Electric Company | Closed cavity noise suppressor |
US5100730A (en) * | 1989-11-16 | 1992-03-31 | Lambers Thomas J | Structural reinforcement apparatus and method of making same |
US5491310A (en) * | 1990-08-16 | 1996-02-13 | Jen; Wang H. | Acoustic board |
US5491307A (en) * | 1990-10-05 | 1996-02-13 | Mcdonnell Douglas Corporation | Porous single expansion ramp |
WO1992012854A1 (en) * | 1991-01-22 | 1992-08-06 | Short Brothers Plc | Structural cellular component |
US5310586A (en) * | 1993-02-05 | 1994-05-10 | Eldim, Inc. | Angled I-beam honeycomb structure |
US5512715A (en) * | 1993-06-15 | 1996-04-30 | Matsushita Electric Industrial Co., Ltd. | Sound absorber |
US5723831A (en) * | 1994-12-20 | 1998-03-03 | Herman Miller Inc. | Tackable acoustical barrier panel |
US5962823A (en) * | 1995-05-17 | 1999-10-05 | Nissan Motor Co., Ltd. | Noise insulating wall structure |
US6360844B2 (en) | 1996-06-13 | 2002-03-26 | The Boeing Company | Aircraft engine acoustic liner and method of making the same |
US5782082A (en) * | 1996-06-13 | 1998-07-21 | The Boeing Company | Aircraft engine acoustic liner |
US6209679B1 (en) | 1996-06-13 | 2001-04-03 | The Boeing Company | Aircraft engine acoustic liner and method of making same |
US6012543A (en) * | 1997-03-07 | 2000-01-11 | Nissan Motor Co., Ltd. | Sound isolation plate structure |
US6371240B1 (en) * | 2000-03-18 | 2002-04-16 | Austin Acoustic Systems, Inc. | Anechoic chamber |
US6509081B1 (en) | 2000-09-28 | 2003-01-21 | The Boeing Company | No-septum acoustic sandwich panel, and apparatus and method for suppressing noise in a nozzle |
US20030072934A1 (en) * | 2001-08-31 | 2003-04-17 | Rem Koolhaas | Panel for architectural design |
US6817442B2 (en) * | 2002-03-29 | 2004-11-16 | Intel Corporation | Acoustically insulated bezel |
US20050241877A1 (en) * | 2002-06-25 | 2005-11-03 | Czerny Hans R | Sound absorber comprising two parts delimiting a hollow space |
EP1662480A1 (en) * | 2003-09-05 | 2006-05-31 | Kabushiki Kaisha Kobe Seiko Sho | Sound absorbing structure and method of producing the same |
EP1662480A4 (en) * | 2003-09-05 | 2013-01-23 | Kobe Steel Ltd | Sound absorbing structure and method of producing the same |
US7819224B2 (en) * | 2004-03-17 | 2010-10-26 | Eads Deutschland Gmbh | Assembly for reducing noise in turbofan engines |
US20080308345A1 (en) * | 2004-03-17 | 2008-12-18 | Eads Deutschland Gmbh | Assembly for Reducing Noise in Turbofan Engines |
US7033137B2 (en) | 2004-03-19 | 2006-04-25 | Ametek, Inc. | Vortex blower having helmholtz resonators and a baffle assembly |
US20060059801A1 (en) * | 2004-09-15 | 2006-03-23 | Quality Research Development & Consulting, Inc. | Acoustically intelligent structures with resonators |
US20070042156A1 (en) * | 2005-08-22 | 2007-02-22 | Rockwell Anthony L | Die cut insulation blanket and method for producing same |
US7923092B2 (en) | 2005-08-22 | 2011-04-12 | Owens Corning Intellectual Capital, Llc | Die cut insulation blanket and method for producing same |
US8133568B2 (en) | 2005-08-22 | 2012-03-13 | Owens Corning Intellectual Capital, Llc | Die cut insulation blanket |
US7552796B2 (en) * | 2006-04-27 | 2009-06-30 | United Technologies Corporation | Turbine engine tailcone resonator |
US20070251760A1 (en) * | 2006-04-27 | 2007-11-01 | United Technologies Corporation | Turbine engine tailcone resonator |
US20110048850A1 (en) * | 2008-05-05 | 2011-03-03 | Alexander Jonathan H | Acoustic composite |
US8381872B2 (en) * | 2008-05-05 | 2013-02-26 | 3M Innovative Properties Company | Acoustic composite |
RU2526215C2 (en) * | 2008-06-25 | 2014-08-20 | Эрсель | Sound-absorbing panel for ejector nozzle |
US8205287B2 (en) | 2008-08-04 | 2012-06-26 | Owens Corning Intellectual Capital, Llc | Insulation element for an electrical appliance such as a dishwasher |
US20100024851A1 (en) * | 2008-08-04 | 2010-02-04 | Rockwell Anthony L | Insulation Element For An Electrical Appliance Such As A Dishwasher |
WO2011082510A1 (en) * | 2010-01-08 | 2011-07-14 | 中国科学院声学研究所 | Compound sound absorption device with built-in resonant cavity |
US20120247867A1 (en) * | 2010-01-08 | 2012-10-04 | Jun Yang | Composite sound-absorbing device with built in resonant cavity |
US20130082194A1 (en) * | 2010-06-16 | 2013-04-04 | Daisuke Muto | Charged particle radiation device and soundproof cover |
US8835883B2 (en) * | 2010-06-16 | 2014-09-16 | Hitachi High-Technologies Corporation | Charged particle radiation device and soundproof cover |
US20130306401A1 (en) * | 2011-01-19 | 2013-11-21 | Rolls-Royce Deutschland Ltd & Co Kg | Sound absorber for a gas turbine exhaust cone, and method for the production thereof |
US8783412B2 (en) * | 2011-01-19 | 2014-07-22 | Rolls-Royce Deutschland Ltd & Co Kg | Sound absorber for a gas turbine exhaust cone, and method for the production thereof |
US8689936B2 (en) * | 2011-12-13 | 2014-04-08 | Rolls-Royce Deutschland Ltd & Co Kg | Acoustic absorber having conical inserts |
US20150090526A1 (en) * | 2012-06-04 | 2015-04-02 | 3M Innovative Properties Company | Sound absorbing (acoustic) board |
US20150027629A1 (en) * | 2013-07-29 | 2015-01-29 | The Boeing Company | Septumization of Honeycomb Sandwiches |
US10363726B2 (en) | 2013-07-29 | 2019-07-30 | The Boeing Company | Septumization of honeycomb sandwiches |
US9643392B2 (en) * | 2013-07-29 | 2017-05-09 | The Boeing Company | Septumization of honeycomb sandwiches |
TWI573470B (en) * | 2014-01-11 | 2017-03-01 | 鴻海精密工業股份有限公司 | Method for manufacturing sound holes of electronic device |
US9909471B2 (en) * | 2014-07-21 | 2018-03-06 | United Technologies Corporation | Noise attenuating acoustic panel |
US20160017775A1 (en) * | 2014-07-21 | 2016-01-21 | United Technologies Corporation | Noise attenuating acoustic panel |
US10280839B2 (en) * | 2014-09-24 | 2019-05-07 | Safran Aircraft Engines | Acoustic treatment panel |
US20180030896A1 (en) * | 2015-02-18 | 2018-02-01 | Mra Systems, Inc. | Acoustic liners and method of shaping an inlet of an acoustic liner |
US10563578B2 (en) * | 2015-02-18 | 2020-02-18 | Mra Systems, Llc | Acoustic liners and method of shaping an inlet of an acoustic liner |
CN105118497A (en) * | 2015-09-18 | 2015-12-02 | 贵州大学 | Tube-bundle perforated panel and spring cyclic structure sound absorption apparatus |
RU2613061C1 (en) * | 2016-01-18 | 2017-03-15 | Олег Савельевич Кочетов | Sound-absorbing element of kochetov with resonant inserts |
US20170229106A1 (en) * | 2016-02-10 | 2017-08-10 | Rohr, Inc. | Acoustic panel with angled corrugated core structures |
US9761216B2 (en) * | 2016-02-10 | 2017-09-12 | Rohr, Inc. | Acoustic panel with angled corrugated core structures |
US9704467B1 (en) * | 2016-04-15 | 2017-07-11 | Rohr, Inc. | Acoustic panel with corrugated baffles and septums |
US9978354B2 (en) * | 2016-04-15 | 2018-05-22 | Rohr, Inc. | Acoustic panel with vertical stiffeners |
US10253727B2 (en) * | 2016-05-12 | 2019-04-09 | Rohr, Inc. | Backside acoustic treatment of nacelle structural fittings |
US20170328281A1 (en) * | 2016-05-12 | 2017-11-16 | Rohr Inc. | Backside acoustic treatment of nacelle structural fittings |
US10578115B2 (en) * | 2016-05-19 | 2020-03-03 | Rolls-Royce Plc | Composite component with hollow reinforcing pins |
US20170335856A1 (en) * | 2016-05-19 | 2017-11-23 | Rolls-Royce Plc | Composite component |
RU2627508C1 (en) * | 2016-07-05 | 2017-08-08 | Олег Савельевич Кочетов | Kochetov`s sound absorption device for industrial premises lining |
RU2648127C1 (en) * | 2017-03-07 | 2018-03-22 | Олег Савельевич Кочетов | Sound-absorbing structure with resonant inserts |
US10369763B2 (en) | 2017-04-19 | 2019-08-06 | The Boeing Company | Segmented acoustic insert |
US10851713B2 (en) * | 2017-08-29 | 2020-12-01 | Mra Systems, Llc. | Acoustic liner having internal structure |
US20190063318A1 (en) * | 2017-08-29 | 2019-02-28 | Mra Systems, Llc. | Acoustic liner having internal structure |
US11208193B2 (en) * | 2017-11-28 | 2021-12-28 | Airbus Operations Sas | Sound attenuation panel for an aircraft |
RU2695723C1 (en) * | 2018-02-22 | 2019-07-25 | федеральное государственное бюджетное образовательное учреждение высшего образования "Пермский национальный исследовательский политехнический университет" | Acoustic plate |
US10906659B2 (en) | 2018-04-03 | 2021-02-02 | Rohr, Inc. | Structured panel with structural reinforcement(s) |
US11434826B2 (en) * | 2018-09-10 | 2022-09-06 | Safran Aircraft Engines | Acoustic treatment panel for a turbojet engine |
CN109147750A (en) * | 2018-11-15 | 2019-01-04 | 中车株洲电力机车有限公司 | A kind of low frequency coupling sound absorption structure |
US11242822B2 (en) | 2018-12-14 | 2022-02-08 | Rohr, Inc. | Structured panel with multi-panel structure(s) |
US11398214B2 (en) | 2018-12-14 | 2022-07-26 | Rohr, Inc. | Forming a structured panel with one or more structural reinforcements |
US20230252966A1 (en) * | 2020-06-23 | 2023-08-10 | Safran | Acoustic panel and associated manufacturing method |
US12211477B2 (en) * | 2020-06-23 | 2025-01-28 | Safran | Acoustic panel and associated manufacturing method |
US20220389882A1 (en) * | 2021-06-03 | 2022-12-08 | General Electric Company | Acoustic cores and tools and methods for forming the same |
US11970992B2 (en) * | 2021-06-03 | 2024-04-30 | General Electric Company | Acoustic cores and tools and methods for forming the same |
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