US2674336A - Acoustical panel - Google Patents

Acoustical panel Download PDF

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US2674336A
US2674336A US188682A US18868250A US2674336A US 2674336 A US2674336 A US 2674336A US 188682 A US188682 A US 188682A US 18868250 A US18868250 A US 18868250A US 2674336 A US2674336 A US 2674336A
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plate
plates
sound
panel
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US188682A
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Carl W Lemmerman
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C W LEMMERMAN Inc
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C W LEMMERMAN Inc
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    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64FGROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
    • B64F1/00Ground or aircraft-carrier-deck installations
    • B64F1/26Ground or aircraft-carrier-deck installations for reducing engine or jet noise; Protecting airports from jet erosion
    • GPHYSICS
    • G10MUSICAL INSTRUMENTS; ACOUSTICS
    • G10KSOUND-PRODUCING DEVICES; METHODS OR DEVICES FOR PROTECTING AGAINST, OR FOR DAMPING, NOISE OR OTHER ACOUSTIC WAVES IN GENERAL; ACOUSTICS NOT OTHERWISE PROVIDED FOR
    • G10K11/00Methods 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
    • G10K11/16Methods or devices for protecting against, or for damping, noise or other acoustic waves in general
    • G10K11/162Selection of materials
    • G10K11/168Plural layers of different materials, e.g. sandwiches

Definitions

  • an object of the present invention to provide an acoustical panel capable of absorbing sounds throughout a wide range of frequencies and capable of operating elciently when disposed in. an exhaust stream ofrelatively high temperature.
  • yAnother object cf this invention is to provide provide an acoustical panel for a sound absorbl ing muffler capable lof withstanding the temperature of a stream of exhaust gases introduced into the'muserverr.
  • Fig. 2 is a bottom plan view kon reduced scale of a panel similar to the panel of Fig. lywith to Fig. l is a transverse sectional view* throughan acoustical panel constructed in accordance parts broken away to illustrate details of con- ⁇ struction;
  • Fig. 4 ⁇ is a fragmentary side elevational view of the sound absorbing panel of Fig. 1, showing an expansion joint at the side of the frame of' the panel.
  • Fig. 5 is a fragmentary transverse sectional view of a muffler duct incorporating a plurality of panels similar to those illustrated in Figs. 1 to 3;
  • Fig. 6 is an end view of the muilier duct.
  • reference numeral II indicates generally an acoustic panel construction in'accordance with this invention to absorb sound waves directed thereagainst through a wide range of frequencies, toA resist heat encountered at relatively high temperatures and to materially reduce the temperatures of a stream of gases directed against its surfaces.
  • the panel I0 is housed or supported by a frame structure which includes side frame members I2 secured as by Welding to cross pieces I4 and to end frame members I6.
  • the members I2 and I5 may be formed from channel stock and are preferably assembled with the flanges of the sides I2 and ends I6 directed outwardly to provide securement surfaces for connecting a plurality of panels in the manner shown in Fig. 4.
  • the cross pieces I4 are formed of lighter channel stock and are transversely secured to side mem-- bers I2 in superimposed pairs, one such member I4 on either side of a plate to be described in detail hereinafter.
  • a perforate cover plate I8 covers the rectangula'r frame'of the panel I0 to provide the operatingl face for the panel and is secured at its marginal portions to the frame members I2 and I6 as by welding. The plate is also secured as by welding to one cross 'member I4 of each superimposed pair.
  • the cover plate I 8 provides a resonator for purposes of sound attenuation and absorption.
  • the thickness of the plate and the size and spacing of the perforations are all factors in determining the efficiency of the plate I8 as an instrument for this purpose.
  • the cover plate I8 is exposed to sound waves of various frequencies. The lower frequency, longer sound and shock waves, engages the plate I8 and causes it to vibrate between the-fraine elements as a diaphragm. The higher frequency, shorter waves, pass through the 'perforations to the spaces beyond the plate I8v asuste with layers of sound absorbing and heat resistant materials in side by side relationship.
  • the first such layer comprises a sheet 20 of asbestos fabricv oriibersI or the sheet 20 may be constructed of glass fibers or other similarly efiicient heat resisting elements.
  • the sheet 20 may be disposed elsewhere within the panel and will pass sound waves and, like any porous wall, will absorb some of the sound, but its main pur,-
  • the sheet 20 is suiciently thin to vibrate with the plate IB and provides a covering means to hold the other pack elements in place and not permit particles of the elements to pro'- ject through the perforations in the platev I8.
  • a pack 22 of relatively dense metallic tinsel is disposed.
  • metallic tinsel is used herein to denote tangled or interwoven strips. Ribbons or wire, including flattened wire sometimes referred. to in the field as "scrubble which is resistant to compression or packing and which has a lowv flow resistance compared with metal filaments or' fibrous material such as steel wool and similar sound-absorbing materials.
  • the metallic tinsel such as copper, stainless steel,
  • Monel metal or copper brass or the like serves to thepack 22 at the side opposite the sheet 20.
  • Thel sheet 24 is secured at its periphery to the side frames I2 and the end frames I6 and is disposed between the superimposed cross members I4 and ⁇ may be welded or riveted thereto.
  • the plate 24 is perforated for the same reasons mentioned in connection with plate I8' and here again the thickness ofthe plate and the size and number of perforations determine the resonating and sound 'ab-- sorbing qualitiesv of the plate.
  • the plate 24 will not be subjected to the temperatures encountered by plate IB and may therefore be formed of galvanized steel or materials having similar heat resistant characteristics.
  • the mineral wool pack 26 is resistant to heat, but its main purpose is to dissipate and absorb sound waves. Due to the porous nature of the mineral wool, the pack'26, as a result of frictional contact, converts much. of the kinetic energy of sound waves to heat energy. The pack 26 also absorbs vibration of the plate 24 caused by sound and shock waves striking thereagainst.
  • a third perforate plate 28 is disposed against the pack 2E and is secured to the frame elements in the same manner as the plate I8, but on the frequency sound waves.
  • the third plate 28 is perforated for the reasons mentioned in connection with the plates I 8 and 24 and the eiliciency of the plate can be predetermined by examining its thickness and size and frequency of its perforations.
  • the plate 28 may be constructed oi galvanized steel or similar material.
  • a final resonating chamber 3U is provided adjacent the plate 28 on the side opposite the pack 26 by securing an arcuate cover 32 to the side and end frame members I2 and I6.
  • a reenforcing rib 34 is longitudinally disposed within the panel I0 between the plate 28 and the cover 32 and is secured thereto. as by w'elding.
  • the resonating chamber 30 provides the last sound dissipating chamber in the panel I and dissipates those waves which pass ⁇ through the aforedescribed perforate plates and the associated chambers and packs.
  • the chamber 32 requires no pack to absorb the sound waves which should be encountered for most contemplated installations.
  • the panel I9 provides three banks of multiple resonators, each bank comprising a perforate plate and the enclosed resonating space behind the plate.
  • Each plate has a relatively large open area provided by the perforations and therebyA passes the higher fre-- quency sound waves for absorption by the asso- ⁇ ciated pack. All of the sound waves passed arenot absorbed by the initial pack, but some strike against the next perforate plate to vibrate it and some pass through the perforations in the plate.
  • the packs also provide shock walls for the plates which are contacted and vibrated by the lower
  • the band of wave frequencies which each bank or uni-t, comprising a plate and associated resonator, will absorb is limited by the size and number of perforationsf, the plate thickness, depth of the resonator and type of sound absorption pack used.
  • the overall wave band of the panel I0 may be substantially pre-r determined.
  • the following dimensional units were used:
  • the panel I0 may be used in mullier installations subjected to relatively high temperatures.
  • panels I0 are mounted in side abutting relationship, as shown in Figs. 5 and 6. It is. of course, necessary that the panels remain in their fitted relation and. donot warp when subjected to heat so, in accordance with this invention, heat expension joints
  • a series of 36 are spaced along the side mem-
  • the joints 36 comprise slots cut in the frame member I2 to provide for expansion of those members.
  • the spaced ends of the frame members I2 are supported at the joints 35 by means of a plate 38 welded to the under side of the top flange I2-a of one end section of the channel stock.
  • the plate 38 extends into the other end section engaging the under side of its upper flange in sliding relationship.
  • the frame remains rigid and cannot buckle at any of the heat expansion joints 3B.
  • the panels I are mounted in side abutting relationship within a cylindrical duct 40.
  • the panels l0 may also be joined in end to end relationship to provide a mufiier of any desired length.
  • the panels IIJ are secured in abutted relation within the duct 40 by means of a plurality of elongated T-shaped beam-like members 42 secured at the stem end to the inner surface of the duct 40.
  • the members 42 have angularly related head flanges 44 which engage the inner surfaces of the bottom flanges I2-b on the side frames I2 of two abutting panels I0.
  • a securing plate 46 having angularly related sides as shown in Fig. 5, may be either permanently or detachably connected in spaced relationship to the head flanges 44 of the T-shaped member 42 for purposes of engaging the side edges of the cover plates I8 of the adjacent panels mounted within the duct 40.
  • the engagement of the edge flanges of the side channel members I2 between each head flange 44 and the securing plate 46 is such as to permit limited sliding movement of the panels IU relative to each other and the T- shaped members 42.
  • the duct 4U is provided with one T-shaped member 42 between each adjacent pair of panels I0 and the spaces between the T-members 42 and the side channel members i2 on the panels Ill are preferably filled with mineral wool to prevent the ready transmission of heat and sound waves through said spaces.
  • the curved cover 32 which deiines the resonating chamber 3i] in each panel I0 conforms generally to the contour of the inner surface of the duct 40 and is disposed in sliding engagement with said inner surface of the duct, thus cooperating to position the panels I0 within the duct.
  • the duct 40 may be of any desired configuration, that is, the duct 4o may be provided with elbow sections to direct the exhaust stream at an angle so that the duct may terminate at any desired location.
  • the elbow sections and exit sections of the duct 4t may be provided with panels I0 in side and end abutting relationship, whereby the entire muiiier is lined with acoustical panels capable of absorbing and dissipating the sound produced by the exhaust of a jet engine.
  • a metallic end cover ring 48 conforming to the contours of the joined panels is secured within the duct 4l! to present a complete annular wall at the end of the muffler.
  • the panels I0 may be used to line walls such as an aircraft test cell for sound proofing the cell and for such installations the panels I need not incorporate the asbestos sheet 2D, as it is unlikely that the panels will be subjected to the temperatures encountered in the aforementioned muffler installations.
  • the side and end frame members I2 and I6 may be abutted in in-line condition, that is, with the flanges of the frame members abutting.v When so joined, the panels will provide a dat Aperforate wall capable of be- 6 ing painted in the manner that conventional'. acoustical wall panels are painted. 1
  • An accoustical panel comprising a plurality of perforate plates in stacked parallel relationship, a layer of sound dissipating packing disposed between each pair of said plates, each layer being formed of unwoven material and being of substantially greater thickness than the plates, and an arcuate imperforate cover member having marginal portions engaged by one of said plates and a body portion in spaced relationship thereto to be a resonating chamber.
  • An accoustical panel comprising a plurality of perforate plates in stacked parallel relationship, a layer of relatively densely packed metallic tinsel disposed between a pair of said plates, a layer of unwoven mineral wool disposed between another pair of said plates, and an imperforate cover member cooperating with the perforate plate farthest removed from said tinsel to define a resonating chamber.
  • An accoustical panel comprising theree perforate plates in spaced parallel relation, a layer of metallic tinsel disposed between the rst and second plates, a layer of mineral wool disposed" between the second and third plates, and an imperforate arcuate cover member having marginal portions adjacent said third plate and its body portion in spaced relation thereto, said layer of metallic tinsel and mineral wool being relatively thick compared to the perforate plates.
  • An accoustical panel comprising means defining an open ended frame structure, a iirst perforate plate covering one open end of the frame, a second perforate plate inwardly disposed in spaced relation to said rst perforate plate, a layer of metallic tinsel disposed between said rst and second perforate plates, a thirdr perforate plate covering the other end of the frame, a layer of unwoven mineral wool disposed between said second and third perforate plates, and an imperforate arcuate cover member having marginal portions adjacent said third ⁇ perforate plate and a body portion in spaced relation thereto.
  • An acoustical panel for installations subjected to high temperature comprising a frame structure, a rst perforate plate covering the frame and secured thereto at its marginal por- ⁇ tions, a sheet of incombustible fabric disposed adjacent the inner surface of said rst plate, a layer of heat resistant metallic tinsel disposed adjacent said fabric, a second perforate plate disposed adjacent said tinsel, a layer of mineral wool disposed adjacent said second perforateV plate, a third perforate plate disposed adjacent said wool, closing said frame and secured thereto,- at its marginal portions, and an imperforate. arcuate cover ⁇ member secured to said frame with its body inspaced relation to said third perforate plate.
  • a ⁇ sound panel for installations subjected to high temperatures comprising a frame structure having open ends, a rst perforate plate covering one open end of said frame and secured thereto at its marginal portions, an asbestos sheet d'mposed adjacent the inner surface of said plate. a layer of copper tinsel disposed inwardly of said sheet, a second perforate plate adjacent said tinsel secured to the frame, a layer of mineral wool disposed inwardly of said second perforate plate, a third perforate plate closing the open end of the frame and secured thereto at its marginal portions, an imperforate arcuate cover member secured to said frame with its body in spaced relation to said third perforate plate, and reinforcing means transversely disposed in said frame and secured thereto.
  • Anacoustic panel comprising an open ended frame stnuc-ture, three perforate plates disposed in the frame in spaced parallel relationship cooperating with the frame to define a pair of resonating chambers in side-by-side relationship, the outermost plates closing the ends of salid frame, a layer of fine copper tinsel disposed in the first of said resonating chambers, a layer of mineral Wool in the second of said resonat-ing chambers, reinforcing means transversely secured to said frame in each of said resonating chambers, an ixnperforate arcuate cover member secured to said frame having a body portion in spaced relationship to one of said perforate plates to define a third resonating chamber therewith in side-by-side relationship to the second resonating chamber, and reinforcing means secured to said frame in said third resonating chamber.
  • An acoustical panel capable of ⁇ dissipating sounds over a relatively wide band of mingled frequencies comprising a plurality of perforate plates in stacked parallel relationship, a relatively thlick layer of sound dissipating packing disposed between each pair of said plates, and an imperforate arcuate cover member having marginal portions engaged by one of said plates, said plates being formed of sheet metal of varying thicknesses, and having perforations of predetermined size and spacing varying from plate to plate whereby each plate and associated packing element as a unit is capable of dissipating sound waves of frequencies within a predetermined band differing from the band of each other plate and associated packing element.
  • a duct forming a passageway for the exhaust stream, and a lining for said duct comprising an acoustical panel in the duct having a plurality of relatively rigid perforated metal plates arranged in spaced apart parallel relationship disposed with an outer plate in contact with and parallel to the flow of the exhaust stream through the duct, a relatively thick layer of unwoven inorganic fibrous material between said plates, and a layer of metallic tinsel for protecting the layer of fibrous material disposed along the interior surface of the said outer plate.
  • An acoustical panel for use in sound-absorbing ducts and the like and capable of withstanding the extreme velocity and temperature conditions encountered in the exhaust stream of a jet engine and effective for attenuating sound varying over a wide frequency range comprising a rectangular frame, front and back cover plates on said frame comprising nat and rigid metallic plates of relatively heavy gage for withstanding said velocity and temperature conditions, both of said plates having spaced apart perforations therein for the passage of sound waves therethrough, and a filler between said plates capable of withstanding said velocity and temperature conditions and attenuating soundcomprising ⁇ a relatively thick layer of metallic tinsel adjacent the front cover plate and a relatively thick layer of unwoven inorganic fibrous material behind the layer of tinsel.
  • An acoustical panel capable of withstanding the extreme velocity and temperature conditions encountered in the exhaust stream of a jet engine and capable of dissipating sounds over a relatively wide band of mingled frequencies, comprising a front sheet metal plate for facing the exhaust stream and at least two additional flat sheet metal plates rearwardly thereof in spacedapart parallel relationship, said sheet metal plates being perforated throughout and at least one of said plates being of different gage, a porous filler of sinuously arranged inorganic material which is pervious to sound but resistant to gas flow disposed between the front plate and the next adjacent rear plate, and a. layer of acoustically absorbent unwoven inorganic fibrous material between the two rear sheet metal plates.
  • An acoustical panel capable of withstanding the extreme velocity and temperature con ditions encountered in the exhaust stream of a jet engine and capable of dissipating soundsover a relatively wide band of mingled frequencies, comprising a front sheet metal plate for facing the'exhaust stream and at least two additional flat sheet metal plates rearwardly thereof in spaced-apart parallel relationship, said sheet metal plates being perforated throughout and at least one of said plates having perforations of different size, a porous iiller of sinuously arranged inorganic material which is pervious to sound but resistant to gas flow disposed between and a layer of acoustically absorbent unwoven inorganic fibrous material between the two rear sheet metal plates.
  • An acoustical panel capable of withstanding the extreme velocity and .temperature conditions encountered in the exhaust stream of a jetl engine and capable of dissipating sounds over a relatively wide band of mingled frequencies, comprising a front sheet metal plate for facing the exhaust stream and at least two additional flat sheet metal plates rearwardly thereof in spaced-apart parallel relationship, said sheet metal plates being formed of sheet metal of varying thicknesses and having perforations of predetermined size and spacing vvarying from plate" to plate, a porous filler of sinuously arranged in-4 organic material which is pervious to sound but resistant to gas flow disposed between the frontv plate and the next adjacent rear plate, and a layer of acoustically absorbent unwoven inor-A comprising a front sheet metal plate forfacing the exhaust stream and at least two additional flat sheet metal plates rearwardly thereof in spaced-apart parallel relationship, said sheet metal plates being perforated throughout, a porous ller of sinuously arranged inorganic material which is pervious to sound but resistant
  • a duct forming a passageway for the exhaust stream, and a lining for said duct comprising an acoustical panel adjacent the periphery of the duct having an outer sheet metal plate in contact with and parallel to the flow of the exhaust stream through the duct and at least two additional iiat sheet metal plates rearwardly thereof in spaced-apart parallel relationship, said sheet metal plates being formed of sheet metal of varying thicknesses having perforations of predetermined size and spacing varying from plate to plate, a porous filler of sinuousl7 arranged inorganic material which is pervous to sound but resistant to gas flow disposed between the outer plate and the next adjacent rear plate and a layer of acoustically absorbent unwoven inorganic fibrous material between the two rear sheet metal plates.
  • An acoustical panel capable of withstanding the extreme velocity and temperature conditions encountered in the exhaust stream of a jet engine and capable of dissipating sounds over a wide band of mingled frequencies
  • acoustical panel capable of withstanding the extreme velocity and temperature conditions encountered in the exhaust stream of a jet engine and capable of dissipating sounds over a wide band of mingled frequencies
  • parallel front and rear cover plates formed of sheet metal of relatively heavy gage and perforated throughout, a relatively thick layer of acoustically absorbent unwoven inorganic brous material disposed at the inner face of the rear cover plate, a perforate retaining wall for the said layer spaced from and parallel to the rear cover plate, and a porous layer of sinuously arranged inorganic material pervious to sound but having high resistance to gas ow disposed between the front cover plate and said retaining wall including a glass ber sheet.

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  • Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Acoustics & Sound (AREA)
  • Multimedia (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Soundproofing, Sound Blocking, And Sound Damping (AREA)

Description

C. w. LEMMERMAN ACOUSTICAL PANEL Filed oct. e, 1950 F/GZ .ff/G2 ff April 6, 1954 Patented Apr. 6, 1954 UNITED STATES PATENT OFFICE ACOUSTICAL PANEL Carl W. Lemmerman, West Hartford, Conn., as-
signor to C. W. Lemmerman, Inc., Hartford, Conn., a corporation of Connecticut Application October 6, 1950, ,Serial No. 188,682
17 Claims. (Q1. 181-42) high temperatures and extreme velocities of the exhaust stream.
The development of jet engines has posed a serious problem relating to mufing ofexhaust sounds while the engine or aircraft is under- The sound muilling diffrgoing ground` tests. culties are particularly acute in test cell installations, since the conventional mufer constructions utilized with the test cell for reciprocating engines are not capable of eillcient operation atv the high temperatures' encountered in jet engine operation. It has also been found thatv the jet engine develops a wider range-of mingled sound frequencies than do conventional reciproeating engines.
Accordingly, it is an object of the present invention to provide an acoustical panel capable of absorbing sounds throughout a wide range of frequencies and capable of operating elciently when disposed in. an exhaust stream ofrelatively high temperature.
yAnother object cf this invention is to provide provide an acoustical panel for a sound absorbl ing muffler capable lof withstanding the temperature of a stream of exhaust gases introduced into the'muiiler.
Other objects will be in part obvious and in part pointed out more in detailhereinafter The invention accordingly consists in the 'features of construction, combination of elements and arrangement of parts which will be exemplifled in the construction hereafter set forthl and the scope of the application of which will be indicated in the appended claims.
In the drawings:
with this invention;
Fig. 2 is a bottom plan view kon reduced scale of a panel similar to the panel of Fig. lywith to Fig. l is a transverse sectional view* throughan acoustical panel constructed in accordance parts broken away to illustrate details of con-` struction;
'Fig'. 3? isv a` side elevational view of the panel illustrated in Fig. 2;
Fig. 4` is a fragmentary side elevational view of the sound absorbing panel of Fig. 1, showing an expansion joint at the side of the frame of' the panel.
Fig. 5 is a fragmentary transverse sectional view of a muffler duct incorporating a plurality of panels similar to those illustrated in Figs. 1 to 3; and
Fig. 6 is an end view of the muilier duct.
Referring to the drawings in detail, reference numeral II) indicates generally an acoustic panel construction in'accordance with this invention to absorb sound waves directed thereagainst through a wide range of frequencies, toA resist heat encountered at relatively high temperatures and to materially reduce the temperatures of a stream of gases directed against its surfaces.
The panel I0 is housed or supported by a frame structure which includes side frame members I2 secured as by Welding to cross pieces I4 and to end frame members I6. The members I2 and I5 may be formed from channel stock and are preferably assembled with the flanges of the sides I2 and ends I6 directed outwardly to provide securement surfaces for connecting a plurality of panels in the manner shown in Fig. 4. The cross pieces I4 are formed of lighter channel stock and are transversely secured to side mem-- bers I2 in superimposed pairs, one such member I4 on either side of a plate to be described in detail hereinafter. y
A perforate cover plate I8 covers the rectangula'r frame'of the panel I0 to provide the operatingl face for the panel and is secured at its marginal portions to the frame members I2 and I6 as by welding. The plate is also secured as by welding to one cross 'member I4 of each superimposed pair.
The cover plate I 8 provides a resonator for purposes of sound attenuation and absorption. The thickness of the plate and the size and spacing of the perforations are all factors in determining the efficiency of the plate I8 as an instrument for this purpose. In practice, the cover plate I8 is exposed to sound waves of various frequencies. The lower frequency, longer sound and shock waves, engages the plate I8 and causes it to vibrate between the-fraine elements as a diaphragm. The higher frequency, shorter waves, pass through the 'perforations to the spaces beyond the plate I8v asuste with layers of sound absorbing and heat resistant materials in side by side relationship. In the illustrated embodiment, the first such layer comprises a sheet 20 of asbestos fabricv oriibersI or the sheet 20 may be constructed of glass fibers or other similarly efiicient heat resisting elements. The sheet 20 may be disposed elsewhere within the panel and will pass sound waves and, like any porous wall, will absorb some of the sound, but its main pur,-
pose isto materially reduce the temperatures of a stream of gases inwardly directed through the` plate I8. The sheet 20 is suiciently thin to vibrate with the plate IB and provides a covering means to hold the other pack elements in place and not permit particles of the elements to pro'- ject through the perforations in the platev I8.
Immediately adjacent the other surface of the sheet 2|)v a pack 22 of relatively dense metallic tinsel is disposed. The term metallic tinsel is used herein to denote tangled or interwoven strips. ribbons or wire, including flattened wire sometimes referred. to in the field as "scrubble which is resistant to compression or packing and which has a lowv flow resistance compared with metal filaments or' fibrous material such as steel wool and similar sound-absorbing materials. The metallic tinsel such as copper, stainless steel,
Monel metal or copper brass or the like serves to thepack 22 at the side opposite the sheet 20. Thel sheet 24 is secured at its periphery to the side frames I2 and the end frames I6 and is disposed between the superimposed cross members I4 and` may be welded or riveted thereto. The plate 24 is perforated for the same reasons mentioned in connection with plate I8' and here again the thickness ofthe plate and the size and number of perforations determine the resonating and sound 'ab-- sorbing qualitiesv of the plate. The plate 24 will not be subjected to the temperatures encountered by plate IB and may therefore be formed of galvanized steel or materials having similar heat resistant characteristics.
A second pack 26 of. mineral wool or the like, less densly packed than the metallic tinsel, is dis-v posed adjacent the surface of the plate 24 opposite the pack 22. The mineral wool pack 26 is resistant to heat, but its main purpose is to dissipate and absorb sound waves. Due to the porous nature of the mineral wool, the pack'26, as a result of frictional contact, converts much. of the kinetic energy of sound waves to heat energy. The pack 26 also absorbs vibration of the plate 24 caused by sound and shock waves striking thereagainst.
A third perforate plate 28 is disposed against the pack 2E and is secured to the frame elements in the same manner as the plate I8, but on the frequency sound waves.
bers l2.
opposite open end of the frame. The third plate 28 is perforated for the reasons mentioned in connection with the plates I 8 and 24 and the eiliciency of the plate can be predetermined by examining its thickness and size and frequency of its perforations. The plate 28 may be constructed oi galvanized steel or similar material.
A final resonating chamber 3U is provided adjacent the plate 28 on the side opposite the pack 26 by securing an arcuate cover 32 to the side and end frame members I2 and I6. A reenforcing rib 34 is longitudinally disposed within the panel I0 between the plate 28 and the cover 32 and is secured thereto. as by w'elding. The resonating chamber 30 provides the last sound dissipating chamber in the panel I and dissipates those waves which pass` through the aforedescribed perforate plates and the associated chambers and packs. The chamber 32 requires no pack to absorb the sound waves which should be encountered for most contemplated installations.
VIt will thus be seen that the panel I9 provides three banks of multiple resonators, each bank comprising a perforate plate and the enclosed resonating space behind the plate. Each plate has a relatively large open area provided by the perforations and therebyA passes the higher fre-- quency sound waves for absorption by the asso-` ciated pack. All of the sound waves passed arenot absorbed by the initial pack, but some strike against the next perforate plate to vibrate it and some pass through the perforations in the plate.
The packs also provide shock walls for the plates which are contacted and vibrated by the lower The band of wave frequencies which each bank or uni-t, comprising a plate and associated resonator, will absorb is limited by the size and number of perforationsf, the plate thickness, depth of the resonator and type of sound absorption pack used.
By varying the aforedescrilcied determinants of efliciency and frequency band width for each unit or bank making up the panel I0, the overall wave band of the panel I0 may be substantially pre-r determined. As a typical example of a construction which has been found to dissipate sound, over a relatively wide frequency band, the following dimensional units were used:
Plate I8-14 gauge stainless steel spaced 2" from plate 24 with .140 perforations on .218 center lines Plate 24-22 gauge galvanized steel spaced 3" with .090" perforations on .125"l center lines Plate 28 -20 gauge galvanized steel spaced 3 from'the center line of cover member 32 with .108" perforations on .1875" center lines Cover plate 32--16 gauge galvanized steel v Peripheral dimensions of panel-8 ft. x 3 ft.
In the preferred form which incorporates the heat resistant sheet 20, the panel I0 may be used in mullier installations subjected to relatively high temperatures. panels I0 are mounted in side abutting relationship, as shown in Figs. 5 and 6. It is. of course, necessary that the panels remain in their fitted relation and. donot warp when subjected to heat so, in accordance with this invention, heat expension joints For such adaptation, a series of 36 are spaced along the side mem- The joints 36 comprise slots cut in the frame member I2 to provide for expansion of those members. The spaced ends of the frame members I2 are supported at the joints 35 by means of a plate 38 welded to the under side of the top flange I2-a of one end section of the channel stock. The plate 38 extends into the other end section engaging the under side of its upper flange in sliding relationship. Thus, the frame remains rigid and cannot buckle at any of the heat expansion joints 3B.
In a muiiler arrangement, as previously mentioned, the panels I are mounted in side abutting relationship within a cylindrical duct 40. The panels l0 may also be joined in end to end relationship to provide a mufiier of any desired length.
The panels IIJ are secured in abutted relation within the duct 40 by means of a plurality of elongated T-shaped beam-like members 42 secured at the stem end to the inner surface of the duct 40. The members 42 have angularly related head flanges 44 which engage the inner surfaces of the bottom flanges I2-b on the side frames I2 of two abutting panels I0. A securing plate 46, having angularly related sides as shown in Fig. 5, may be either permanently or detachably connected in spaced relationship to the head flanges 44 of the T-shaped member 42 for purposes of engaging the side edges of the cover plates I8 of the adjacent panels mounted within the duct 40. Preferably, the engagement of the edge flanges of the side channel members I2 between each head flange 44 and the securing plate 46 is such as to permit limited sliding movement of the panels IU relative to each other and the T- shaped members 42.
The duct 4U is provided with one T-shaped member 42 between each adjacent pair of panels I0 and the spaces between the T-members 42 and the side channel members i2 on the panels Ill are preferably filled with mineral wool to prevent the ready transmission of heat and sound waves through said spaces. The curved cover 32 which deiines the resonating chamber 3i] in each panel I0 conforms generally to the contour of the inner surface of the duct 40 and is disposed in sliding engagement with said inner surface of the duct, thus cooperating to position the panels I0 within the duct.
The duct 40 may be of any desired configuration, that is, the duct 4o may be provided with elbow sections to direct the exhaust stream at an angle so that the duct may terminate at any desired location. The elbow sections and exit sections of the duct 4t may be provided with panels I0 in side and end abutting relationship, whereby the entire muiiier is lined with acoustical panels capable of absorbing and dissipating the sound produced by the exhaust of a jet engine. A metallic end cover ring 48 conforming to the contours of the joined panels is secured within the duct 4l! to present a complete annular wall at the end of the muffler.
The panels I0 may be used to line walls such as an aircraft test cell for sound proofing the cell and for such installations the panels I need not incorporate the asbestos sheet 2D, as it is unlikely that the panels will be subjected to the temperatures encountered in the aforementioned muffler installations. For adapting the panels I0 for use in flat walls, the side and end frame members I2 and I6 may be abutted in in-line condition, that is, with the flanges of the frame members abutting.v When so joined, the panels will provide a dat Aperforate wall capable of be- 6 ing painted in the manner that conventional'. acoustical wall panels are painted. 1
As many changes could be made in the above construction and many apparently widely different embodiments of this invention could be made without departing from the scope thereof, it is intended that all matter contained in theabove description or shown in the accompanying drawings shall be interpreted as illustrative and not in a limiting sense.
It is also to be understood that the language used in the following claims is intended to cover all of the generic and specific features of the invention herein described and all statements of the scope of the invention which, as a matter of language, might be said to fall therebetween.
I claim as my invention:
l. An accoustical panel comprising a plurality of perforate plates in stacked parallel relationship, a layer of sound dissipating packing disposed between each pair of said plates, each layer being formed of unwoven material and being of substantially greater thickness than the plates, and an arcuate imperforate cover member having marginal portions engaged by one of said plates and a body portion in spaced relationship thereto to denne a resonating chamber.
2. An accoustical panel comprising a plurality of perforate plates in stacked parallel relationship, a layer of relatively densely packed metallic tinsel disposed between a pair of said plates, a layer of unwoven mineral wool disposed between another pair of said plates, and an imperforate cover member cooperating with the perforate plate farthest removed from said tinsel to define a resonating chamber.
3. An accoustical panel comprising theree perforate plates in spaced parallel relation, a layer of metallic tinsel disposed between the rst and second plates, a layer of mineral wool disposed" between the second and third plates, and an imperforate arcuate cover member having marginal portions adjacent said third plate and its body portion in spaced relation thereto, said layer of metallic tinsel and mineral wool being relatively thick compared to the perforate plates.
4. An accoustical panel comprising means defining an open ended frame structure, a iirst perforate plate covering one open end of the frame, a second perforate plate inwardly disposed in spaced relation to said rst perforate plate, a layer of metallic tinsel disposed between said rst and second perforate plates, a thirdr perforate plate covering the other end of the frame, a layer of unwoven mineral wool disposed between said second and third perforate plates, and an imperforate arcuate cover member having marginal portions adjacent said third` perforate plate and a body portion in spaced relation thereto.
5. An acoustical panel for installations subjected to high temperature comprising a frame structure, a rst perforate plate covering the frame and secured thereto at its marginal por-` tions, a sheet of incombustible fabric disposed adjacent the inner surface of said rst plate, a layer of heat resistant metallic tinsel disposed adjacent said fabric, a second perforate plate disposed adjacent said tinsel, a layer of mineral wool disposed adjacent said second perforateV plate, a third perforate plate disposed adjacent said wool, closing said frame and secured thereto,- at its marginal portions, and an imperforate. arcuate cover` member secured to said frame with its body inspaced relation to said third perforate plate.
6. A `sound panel for installations subjected to high temperatures comprising a frame structure having open ends, a rst perforate plate covering one open end of said frame and secured thereto at its marginal portions, an asbestos sheet d'mposed adjacent the inner surface of said plate. a layer of copper tinsel disposed inwardly of said sheet, a second perforate plate adjacent said tinsel secured to the frame, a layer of mineral wool disposed inwardly of said second perforate plate, a third perforate plate closing the open end of the frame and secured thereto at its marginal portions, an imperforate arcuate cover member secured to said frame with its body in spaced relation to said third perforate plate, and reinforcing means transversely disposed in said frame and secured thereto.
7. Anacoustic panel comprising an open ended frame stnuc-ture, three perforate plates disposed in the frame in spaced parallel relationship cooperating with the frame to define a pair of resonating chambers in side-by-side relationship, the outermost plates closing the ends of salid frame, a layer of fine copper tinsel disposed in the first of said resonating chambers, a layer of mineral Wool in the second of said resonat-ing chambers, reinforcing means transversely secured to said frame in each of said resonating chambers, an ixnperforate arcuate cover member secured to said frame having a body portion in spaced relationship to one of said perforate plates to define a third resonating chamber therewith in side-by-side relationship to the second resonating chamber, and reinforcing means secured to said frame in said third resonating chamber.
8. An acoustical panel capable of `dissipating sounds over a relatively wide band of mingled frequencies comprising a plurality of perforate plates in stacked parallel relationship, a relatively thlick layer of sound dissipating packing disposed between each pair of said plates, and an imperforate arcuate cover member having marginal portions engaged by one of said plates, said plates being formed of sheet metal of varying thicknesses, and having perforations of predetermined size and spacing varying from plate to plate whereby each plate and associated packing element as a unit is capable of dissipating sound waves of frequencies within a predetermined band differing from the band of each other plate and associated packing element.
9. In a sound muler for attenuating the sound of an engine exhaust stream, a duct forming a passageway for the exhaust stream, and a lining for said duct comprising an acoustical panel in the duct having a plurality of relatively rigid perforated metal plates arranged in spaced apart parallel relationship disposed with an outer plate in contact with and parallel to the flow of the exhaust stream through the duct, a relatively thick layer of unwoven inorganic fibrous material between said plates, and a layer of metallic tinsel for protecting the layer of fibrous material disposed along the interior surface of the said outer plate.
10. An acoustical panel for use in sound-absorbing ducts and the like and capable of withstanding the extreme velocity and temperature conditions encountered in the exhaust stream of a jet engine and effective for attenuating sound varying over a wide frequency range comprising a rectangular frame, front and back cover plates on said frame comprising nat and rigid metallic plates of relatively heavy gage for withstanding said velocity and temperature conditions, both of said plates having spaced apart perforations therein for the passage of sound waves therethrough, and a filler between said plates capable of withstanding said velocity and temperature conditions and attenuating soundcomprising `a relatively thick layer of metallic tinsel adjacent the front cover plate and a relatively thick layer of unwoven inorganic fibrous material behind the layer of tinsel.
11. A duct as defined in claim 9, in which said acoustical panel lining is spaced from the duct wall to form a resonating chamber therebetween.
12. An acoustical panel capable of withstanding the extreme velocity and temperature conditions encountered in the exhaust stream of a jet engine and capable of dissipating sounds over a relatively wide band of mingled frequencies, comprising a front sheet metal plate for facing the exhaust stream and at least two additional flat sheet metal plates rearwardly thereof in spacedapart parallel relationship, said sheet metal plates being perforated throughout and at least one of said plates being of different gage, a porous filler of sinuously arranged inorganic material which is pervious to sound but resistant to gas flow disposed between the front plate and the next adjacent rear plate, and a. layer of acoustically absorbent unwoven inorganic fibrous material between the two rear sheet metal plates.
13. An acoustical panel capable of withstanding the extreme velocity and temperature con ditions encountered in the exhaust stream of a jet engine and capable of dissipating soundsover a relatively wide band of mingled frequencies, comprising a front sheet metal plate for facing the'exhaust stream and at least two additional flat sheet metal plates rearwardly thereof in spaced-apart parallel relationship, said sheet metal plates being perforated throughout and at least one of said plates having perforations of different size, a porous iiller of sinuously arranged inorganic material which is pervious to sound but resistant to gas flow disposed between and a layer of acoustically absorbent unwoven inorganic fibrous material between the two rear sheet metal plates.
14. An acoustical panel capable of withstanding the extreme velocity and .temperature conditions encountered in the exhaust stream of a jetl engine and capable of dissipating sounds over a relatively wide band of mingled frequencies, comprising a front sheet metal plate for facing the exhaust stream and at least two additional flat sheet metal plates rearwardly thereof in spaced-apart parallel relationship, said sheet metal plates being formed of sheet metal of varying thicknesses and having perforations of predetermined size and spacing vvarying from plate" to plate, a porous filler of sinuously arranged in-4 organic material which is pervious to sound but resistant to gas flow disposed between the frontv plate and the next adjacent rear plate, and a layer of acoustically absorbent unwoven inor-A comprising a front sheet metal plate forfacing the exhaust stream and at least two additional flat sheet metal plates rearwardly thereof in spaced-apart parallel relationship, said sheet metal plates being perforated throughout, a porous ller of sinuously arranged inorganic material which is pervious to sound but resistant to gas flow disposed between the front plate and the next adjacent rear plate, a layer oi' acoustically absorbent unwoven inorganic fibrous material between the two rear sheet metal plates, and an imperforate rear cover member spaced from the rearmost perforated plate and cooperating therewith to form a resonating chamber therebetween.
16. In a sound muiiier for attenuating the sound oi an exhaust stream, a duct forming a passageway for the exhaust stream, and a lining for said duct comprising an acoustical panel adjacent the periphery of the duct having an outer sheet metal plate in contact with and parallel to the flow of the exhaust stream through the duct and at least two additional iiat sheet metal plates rearwardly thereof in spaced-apart parallel relationship, said sheet metal plates being formed of sheet metal of varying thicknesses having perforations of predetermined size and spacing varying from plate to plate, a porous filler of sinuousl7 arranged inorganic material which is pervous to sound but resistant to gas flow disposed between the outer plate and the next adjacent rear plate and a layer of acoustically absorbent unwoven inorganic fibrous material between the two rear sheet metal plates.
17. An acoustical panel capable of withstanding the extreme velocity and temperature conditions encountered in the exhaust stream of a jet engine and capable of dissipating sounds over a wide band of mingled frequencies comprising parallel front and rear cover plates formed of sheet metal of relatively heavy gage and perforated throughout, a relatively thick layer of acoustically absorbent unwoven inorganic brous material disposed at the inner face of the rear cover plate, a perforate retaining wall for the said layer spaced from and parallel to the rear cover plate, and a porous layer of sinuously arranged inorganic material pervious to sound but having high resistance to gas ow disposed between the front cover plate and said retaining wall including a glass ber sheet.
References Cited in the file of this patent UNITED STATES PATENTS Number Name Date 1,006,595 Red Oct. 24, 1911 1,229,434 Flockhart June 12, 1917 1,952,975 Davy Mar. 27, 1934 2,037,884 Day Apr. 21, 1936 2,061,903 Hartsock Nov. 24, 1936 2,089,492 Lambert Aug. 16, 1937 2,138,510 Rauen Nov. 28, 1938 2,161,708 Heerwagen June 6, 1939 2,308,869 Eckhardt June 19, 1943 2,519,160 Tucker Aug. 15, 1950 FOREIGN PATENTS Number Country Date 28,031 Great Britain Dec. 13, 1912 348,928 Great Britain May 21, 1931 498,533 Great Britain Jan. 10, 1939
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Cited By (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2826261A (en) * 1956-08-30 1958-03-11 Oliver C Eckel Acoustical control apparatus
US2840180A (en) * 1955-03-23 1958-06-24 Worthington Corp Means for reducing acoustical energy in a fluid translating system
US2842222A (en) * 1954-09-14 1958-07-08 Burnett Estes Acoustical test cell structures
US2909235A (en) * 1955-11-03 1959-10-20 Gen Dynamics Corp Muffler
US2915135A (en) * 1957-09-12 1959-12-01 C W Lemmerman Inc Acoustical panel
US2918984A (en) * 1953-10-08 1959-12-29 Koppers Co Inc Sound control shroud for aircraft engines
US2958387A (en) * 1955-09-29 1960-11-01 Richard M Greff Silencer for compressible fluid devices
US2989136A (en) * 1959-04-14 1961-06-20 Wohlberg George Sound attenuation
US3235029A (en) * 1958-07-02 1966-02-15 C W Lemmerman Inc Sound attenuating panel with vibrating damping plate
US3265154A (en) * 1964-07-09 1966-08-09 Insul Coustic Corp Acoustical panels with spaced layers
DE2108662A1 (en) * 1970-02-25 1971-09-09 Cav Ltd Metal shield
US3688865A (en) * 1970-11-17 1972-09-05 Cloyd D Smith Jet engine noise suppressor
US3762498A (en) * 1971-07-22 1973-10-02 Gen Electric Gas turbine exhaust silencer
US4161231A (en) * 1973-10-31 1979-07-17 Rolls-Royce Limited Metal cavitated sandwich structures
US4163479A (en) * 1976-07-15 1979-08-07 Messerschmitt-Bolkow-Blohm Gmbh Noise absorbing device
US4926963A (en) * 1987-10-06 1990-05-22 Uas Support, Inc. Sound attenuating laminate for jet aircraft engines
US20080202848A1 (en) * 2005-08-08 2008-08-28 Alstom Technology Ltd Sound absorber for gas turbine installations
US20150267404A1 (en) * 2014-03-20 2015-09-24 Vanair Design Inc. Panel and panel structure for ventilation and both reactive and dissipative sound dampening

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US1006595A (en) * 1910-11-02 1911-10-24 Charles Red Muffler.
US1229434A (en) * 1916-04-14 1917-06-12 James Flockhart Silencer.
GB348928A (en) * 1930-06-19 1931-05-21 William James Davy An improved method of and means for sound proofing ceilings, walls, partitions and the like
US1952975A (en) * 1930-06-19 1934-03-27 Davy William James Soundproof ceiling, wall, partition, and the like
US2037884A (en) * 1932-11-11 1936-04-21 Burgess Lab Inc C F Silencer
US2061903A (en) * 1929-08-24 1936-11-24 Burgess Lab Inc C F Carburetor muffler
US2089492A (en) * 1935-07-06 1937-08-10 American Radiator Co Duct
US2138510A (en) * 1930-02-10 1938-11-29 Carl F Rauen Muffler
GB498533A (en) * 1937-07-30 1939-01-10 Francois Cementation Co Ltd Improvements in or relating to silencers for exhaust and other gaseous currents
US2161708A (en) * 1937-07-29 1939-06-06 Paul M Heerwagen Acoustic surfacing for walls, ceilings, partitions, or the like
US2308869A (en) * 1940-05-11 1943-01-19 Bell Telephone Labor Inc Acoustic wall panel
US2519160A (en) * 1942-12-05 1950-08-15 Belle Weather Inc Testing apparatus with sound absorbing panels forming air passages

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Publication number Priority date Publication date Assignee Title
US1006595A (en) * 1910-11-02 1911-10-24 Charles Red Muffler.
US1229434A (en) * 1916-04-14 1917-06-12 James Flockhart Silencer.
US2061903A (en) * 1929-08-24 1936-11-24 Burgess Lab Inc C F Carburetor muffler
US2138510A (en) * 1930-02-10 1938-11-29 Carl F Rauen Muffler
GB348928A (en) * 1930-06-19 1931-05-21 William James Davy An improved method of and means for sound proofing ceilings, walls, partitions and the like
US1952975A (en) * 1930-06-19 1934-03-27 Davy William James Soundproof ceiling, wall, partition, and the like
US2037884A (en) * 1932-11-11 1936-04-21 Burgess Lab Inc C F Silencer
US2089492A (en) * 1935-07-06 1937-08-10 American Radiator Co Duct
US2161708A (en) * 1937-07-29 1939-06-06 Paul M Heerwagen Acoustic surfacing for walls, ceilings, partitions, or the like
GB498533A (en) * 1937-07-30 1939-01-10 Francois Cementation Co Ltd Improvements in or relating to silencers for exhaust and other gaseous currents
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Cited By (20)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2918984A (en) * 1953-10-08 1959-12-29 Koppers Co Inc Sound control shroud for aircraft engines
US2842222A (en) * 1954-09-14 1958-07-08 Burnett Estes Acoustical test cell structures
US2840180A (en) * 1955-03-23 1958-06-24 Worthington Corp Means for reducing acoustical energy in a fluid translating system
US2958387A (en) * 1955-09-29 1960-11-01 Richard M Greff Silencer for compressible fluid devices
US2909235A (en) * 1955-11-03 1959-10-20 Gen Dynamics Corp Muffler
US2826261A (en) * 1956-08-30 1958-03-11 Oliver C Eckel Acoustical control apparatus
US2915135A (en) * 1957-09-12 1959-12-01 C W Lemmerman Inc Acoustical panel
US3235029A (en) * 1958-07-02 1966-02-15 C W Lemmerman Inc Sound attenuating panel with vibrating damping plate
US2989136A (en) * 1959-04-14 1961-06-20 Wohlberg George Sound attenuation
US3265154A (en) * 1964-07-09 1966-08-09 Insul Coustic Corp Acoustical panels with spaced layers
DE2108662A1 (en) * 1970-02-25 1971-09-09 Cav Ltd Metal shield
US3688865A (en) * 1970-11-17 1972-09-05 Cloyd D Smith Jet engine noise suppressor
US3762498A (en) * 1971-07-22 1973-10-02 Gen Electric Gas turbine exhaust silencer
US4161231A (en) * 1973-10-31 1979-07-17 Rolls-Royce Limited Metal cavitated sandwich structures
US4163479A (en) * 1976-07-15 1979-08-07 Messerschmitt-Bolkow-Blohm Gmbh Noise absorbing device
US4926963A (en) * 1987-10-06 1990-05-22 Uas Support, Inc. Sound attenuating laminate for jet aircraft engines
US20080202848A1 (en) * 2005-08-08 2008-08-28 Alstom Technology Ltd Sound absorber for gas turbine installations
US7832524B2 (en) * 2005-08-08 2010-11-16 Alstom Technology Ltd Sound absorber for gas turbine installations
US20150267404A1 (en) * 2014-03-20 2015-09-24 Vanair Design Inc. Panel and panel structure for ventilation and both reactive and dissipative sound dampening
US9493949B2 (en) * 2014-03-20 2016-11-15 Vanair Design Panel and panel structure for ventilation and both reactive and dissipative sound dampening

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