US3159238A - Diffuser screen with heat-insulating rungs for exhaust noise suppressor for reactionengines - Google Patents

Diffuser screen with heat-insulating rungs for exhaust noise suppressor for reactionengines Download PDF

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US3159238A
US3159238A US72891A US7289160A US3159238A US 3159238 A US3159238 A US 3159238A US 72891 A US72891 A US 72891A US 7289160 A US7289160 A US 7289160A US 3159238 A US3159238 A US 3159238A
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rungs
rod
exhaust
screen
noise suppressor
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Wayne B Shearer
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Curtiss Wright Corp
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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

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  • SHEARER AGENT 1 1964 w. a. SHEARER DIFFUSER SCREEN WITH HEAT-INSULATING RUNGS FOR EXHAUST NOISE SUPPRESSOR FOR REACTION ENGINES Filed Decl, 1960 3 Sheets-Sheet 2 1964 w. B. SHEARER 3,159,238
  • Thisinvention relates to a three-dimensional labyrinthine cribworlc diffusing screen, and more particularly to an improvement ,on such a screen as described in the copending application of Maron L. Morris and lohn A. Sobel Ill, Exhaust Noist Suppressor for Reaction En ines, Serial'No. 65, 389, filed October 27, 1960, now Patent No. 3,120,877, patented February 11, 1964, and assigned to the same assignee.
  • such an exhaust noise suppressor comprises in part a large chan berin which the exhaust from a reaction engine can expand, after first passing through a diffusing screen comprising a labyrinthine cribworlc of rungs disposed -transversely to the axis of discharge of the exhaust stream, the cribwork having considerable extension in. the. axial direction, whereby staged diffusion. is provided in a plurality of planes at various distances from the engine nozzle, as the exhaust stream strikes the rungs of the cribwork and iabroken up thereby.
  • a diffusing screen when formed .of corrosionresistant carbon steel rungs, will satisfactorily withstand the exhaust temperature of the usual jet engine, of the order of ll50 F.
  • Stillanother object is the provision of a diffusing screen of high mechanical strength at elevated temperatures.
  • Yet another object is to provide a diffusing screen not subject to corrosion from afterburner exhaust.
  • a further object is to provide a diiiusing screen resistant to thermal shock.
  • FIGURE 1 is a longitudinal cross-sectional elevation of an exhaust noise suppressor
  • FIGURE 2 is a view of one of the difiusing rungs of the present invention. 7 V
  • FIGURE 3 is a perspective view, partially broken away, of one of the diffusing rungs
  • FIGURE 4- is a transverse cross-section of another embodiment of the rung.
  • FIGURE 5 is a perspective view of the three-dimensional labyrinthine cribwork diliusing screen.
  • annular resonant chamber ll3surrcunds the upper portion of the stack and cornmunicates with the-interior. thereof through suitable apertures 18a.
  • the expansion chamber and; the stack 7 are both double-walled and, have acoustical packing material .19 1 disposed between the walls; the inner walls 20, arepreferably offstainless steel and are providedrwith apertures, indicated atZila, to allow acoustical access to the packing,
  • the outer walls may be of mild steelorother suitablematerial.
  • a three-dimensional, labyrinthine cribwork diffusing screen 16 (later to be describedindetail) is positioned within the inner diameter of the entrance section 12, in such a manner that the rearrnost extension of-thescreen is at the plane of entrance into expansion chamber 13.
  • the screen is of suchdimensions in the transverse direction that it substantially spans the inner diameter, of portion 12, and itrnay be mounted onthe inner wall thereof by any convenient structural elements, in the present case a.generallyrectangular frame 22.
  • a grid i simple crisscross pattern. and circular outline is adjustably positioned within the expansion section, disposed on the horizontal axis thereof and transverse to said axis.
  • the grid may be supported and maintained in the selected position bya spider 31 as shown, or by othersuitable structural elements.
  • the grid is nominally positioned approximately halfway betweenthe diffuser screen and. thestackfentrance,
  • h means for translating, it along the axis of the expansion chamber so thatrits operating position may; beeither upstream or downstream .from its nominal position, according to theflow conditions encountered.
  • Suitable translating means may be the slotted brackets 32 to which the ends of the spider are bolted, or any other desired means of well hn'own kind.
  • the op'erationlof the exhaust noise suppressor is as follows.
  • the suppressor is placedinapposition to a reactioncngine 21 with the exhaust nozzle intromitted within the entrance portion, substantially, coaxial therewith.
  • the exhaust is discharged into the suppressor entrance section 12 passing through the cribwork diffusing screen in a plurality of labyrinthine paths, whereby its velocity is greatly diminished, and it is diverted from the axialdirection and expands with considerable turbulence into the expansion chamber.
  • the high velocity of the exhaust leaving the nozzle in combination with the internal diameter of the entrance section and the restricted converging throatdefined by the nozzle and the frustoconicalinternal wall 2-5 disposed inside the entrance section, causes'external air to be aspirated into the suppressor.
  • Such aspirated air serves a double purpose. It cools the exhaust somewhat and assists in diffusing it and in creating turbulence and expansion downstream from the screen; also, owing to the high exit speed of the exhaust from the nozzle,'the aspirated air will pass through the converging throat at a speed of Mach 1 or higher. Selfnoise generated by the impingement of the exhaust stream on the diffusing screen cannot be radiated upstream against an inflow of air at Mach 1 or above. n the event that perfect adjustment between the engine and the suppressor has not been achieved and.
  • the aspirated air may not quite reach Mach 1
  • sound baffles 26 are pro vided in the upstream portion of the entrance section, attached to the inner wall thereof and extending radially inward, and so disposed that any self-noise which may be radiated upstream will be absorbed by the baffles.
  • FIGURES 2 and 3 show one of the rungs of the diffusing screen of this invention.
  • a rod 37 which serves as the structural element of the rung and supports the other elements against the thrust of the exhaust stream.
  • the material of which such a rod is formed must be resistant to corrosion, oxidation, and thermal shock, and must retain its strength at elevated temperatures.
  • Various metals such as corrosion-resistant steels and other alloys having these properties are known and are suitable for such use.
  • a particularly satisfactory material is the alloy sold under the name lnconel 700, a registered trademark of the International Nickel Company, having the following composition:
  • Aluminum 30 Cobalt 23.0 Molybdenum 3.0 Iron 0.5 Nickel Balance Inconel 700 has a melting point around 2500 F., and a rupture life at 1800 F. of five hours under stress of 10,000 p.s.i. or ninety hours under stress of 6000 p.s.i. Although the exhaust temperature may be higher than the melting point of the metal, the rung is so formed that the metal is insulated from a large part of the heat, and the material directly exposed to the hot gases is well able to withstand the temperatures reached in afterburning operation.
  • Rod 37 is surrounded by a plurality of cylindrical sleeves 38 threaded end-to-end on the rod and formed of a material of high melting point and high resistance to thermal shock.
  • Various ceramics and cermets possess the desired characteristics; a material which has been d found particularly suitable for the sleeves is silicon carbide, especially when sintered with a silicon nitride binder, having a melting point above 4892 F., and being very little affected by thermal shock.
  • the sleeves are of such internal diameter as to leave an appreciable annularspace between the sleeves and the rod when they are positioned coaxially thereon.
  • This annular space is filled with an insulating material 39 of high melting point and a low coeflicient of heat transfer.
  • insulating material 39 of high melting point and a low coeflicient of heat transfer.
  • powdered zirconium oxide has been found particularly satisfactory, with a melting point of about 4892" F.
  • the insulating material is retained within the annular space by a small annulus of cement 41 at each end of each sleeve. Powdered zirconium oxide with a binder of sodium silicate makes a suitable cement.
  • a metal flange 4-2 may be welded, brazed, or otherwise securely fastened around the rod at each end of the assemblage of sleeves, leaving a length of rod protruding therefrom at each end for positioning the rungs in the cribwork.
  • FIGURE 4 is a transverse cross-section of another embodiment 36a of one of the rungs.
  • the elements of the rung are the same as previously described, comprising a rod 37, a plurality of sleeves 33, insulating material 39, and cement 41, but these elements are differently assembled.
  • the sleeves are positioned coaxial with the rod, they are positioned with the sleeves being coaxial with each other, but with the rod disposed off center and in contact with the inner wall of the sleeves, tangent thereto, leaving a space of lune-shaped cross-section between the rod and the sleeves.
  • This space of lune-shaped section is filled with insulating material and stopped with cement at each end of each sleeve as before.
  • Rungs 36a may also be provided with end flanges 42.
  • the advantage of this construction is that rungs 30a may be assembled in the cribwork screen in such a manner that the exhaust blast impinges on them on the side furthest from the metal and having the largest amount of insulating material upstream from the rod.
  • FIGURE 5 shows a three-dimensional labyrinthine cribwork diffusing screen 16, completely assembled and ready for installation in an exhaust noise suppressor.
  • a generally rectangular frame 22 having sides of flat metal plates welded or otherwise joined, and preferably having beveled corners 43 for attachment to the inner diameter of the entrance portion of the suppressor, the diagonal dimensions of the frame being such as to provide a suitable fit therein.
  • the sides of the frame are bored for positioning a plurality of ranks of rungs 36 or 365a, the free ends of the rods 37 projecting outwardly through the bored apertures.
  • the rods or the flanges may be welded or brazed to the frame at the points of contact, if desired.
  • the first rank 46a comprises a plurality of parallel rungs spanning the frame with the rod ends positioned. by the apertures, the rungs being equally spaced apart with the center rung on the vertical centerline, in the same plane, and with the outermost rungs just inside the bevels at the corners.
  • the second rank 46b comprises a plurality of similar rungs, parallel to each other and similarly spaced, but crossing those of the first rank at substantially in a plane behind or downstream from that of the first rank, the center rung being on the horizontal centerline.
  • a third rank 450 is provided having rungs parallel to those of the first rank, but in a plane downstream from the second rank; the center rung is again on the vertical centerline, but the flanking rungs are positioned somewhat closer together than those of the first rank.
  • a fourth rank 46d of similar rungs is provided in a plane behind the third rank, substantially normal thereto but .having the same spacing as the third rank.
  • a fifth rank 46a is provided in a plane behind the fourth, parallel to the third rank and having the center rung on centerline, but spaced more closely together, so that the flanking rungs are positioned more inwardly than those of the third rank.
  • the sixth and last rank 46f occupies a plane behind the fifth rank, the rungs being normal to those of the fifth but similarly spaced.
  • the foregoing construction provides a three-dimensional'lattice or cribwork, with none of the rungs except the center ones occluding anyparallel rung in the axial directioinand so arranged that the exhaust stream in passing therethrough is broken up and takes a plurality of labyrinthine paths, with a plurality of minor shocks,
  • the diffusing screen may be made with more or less ranks of rungs, with more or less rungs, in each rank, and with rungs of the form of either 36 or 36a. Spacing may also be diiierent, and the rungs may be arranged .so that none of them occlude each other. It'is immaterial which rungs may be vertical in the operating position of the screen, or whether any are. The rungs may, if desired,
  • a three-dimensional labyrinthine cribwork diffusing screen for an exhaust noise suppressor comprising in combination a plurality of ranks of rungs; each of said ranks comprising a plurality of parallel rungs spaced apart from each other in a plane; said ranks beingstacked in laminar fashion; each of saidrungs comprising a straight metal rod, a plurality of cylindrical ceramic sleeves having a fusing temperature above 3200" F. disposed in end-to-end relationship and surrounding said rod and defining with said rod a space between said rod and said sleeves, and a powdered ceramic heat-insulating material having a fusing temperature above 3200 F. disposed in said space 6.
  • a three-dimensionai labyrinthine cribwork diffusing screen for an exhaust noise suppressor comprising in combination a plurality of ranks of rungs; each of said ranks comprising a plurality of parallel rungs spaced rather than a single one is that under the enormous pressure of an exhaust stream some flexibility of the rungs is desirable, which would not be provided by a single sleeve.
  • rungs having single continuous sleeves may be employed.
  • the exterior surface of thesleeves may also be given an oxidationresistant coating of flame-sprayed refractory material,

Description

Dec. 1, 1964 w. B. SHEARER 3,159,238
DIFFUSER SCREEN WITH HEAT-INSULATING RUNGS FOR EXHAUST NOISE SUPPRESSOR FOR REACTION ENGINES Filed Dec. 1. 1960 s Sheets-Sheet 1 F I G. 1
INVENTOR.
WAYNE B. SHEARER BY W'Z AGENT INVENTOR.
WAYNE B. SHEARER AGENT 1, 1964 w. a. SHEARER DIFFUSER SCREEN WITH HEAT-INSULATING RUNGS FOR EXHAUST NOISE SUPPRESSOR FOR REACTION ENGINES Filed Decl, 1960 3 Sheets-Sheet 2 1964 w. B. SHEARER 3,159,238
DIFFUSER SCREEN WITH HEAT-INSULATING RUNGS FOR EXHAUST NOISE SUPPRESSOR FOR REACTION ENGINES Filed Dec. 1, 1960 I5 Sheets-Sheet 3 F I G. 5
INVENTOR. WAYNE B. SHEARER AGENT United States Patent M I 3,159,238 DHEFUSER SEREEN WlTH ,lHiEAT-KNSULATlNG .RUNGS EOREXHAUS'E NGESE SUEERESSE'R E'JR REAQ'HUN ENGENES Wayne Bafih'earer, dtaie College, Pa, assigns-r to 'Curtiss- Wright Corporation, a cor-'poration oi Deiaware Filed Dec. l, 196%), Set. No. 72,3?131 '7 Claims (El. Edi-33) Thisinvention relates to a three-dimensional labyrinthine cribworlc diffusing screen, and more particularly to an improvement ,on such a screen as described in the copending application of Maron L. Morris and lohn A. Sobel Ill, Exhaust Noist Suppressor for Reaction En ines, Serial'No. 65, 389, filed October 27, 1960, now Patent No. 3,120,877, patented February 11, 1964, and assigned to the same assignee.
As disclosed in the forementioned application, such an exhaust noise suppressor comprises in part a large chan berin which the exhaust from a reaction engine can expand, after first passing througha diffusing screen comprising a labyrinthine cribworlc of rungs disposed -transversely to the axis of discharge of the exhaust stream, the cribwork having considerable extension in. the. axial direction, whereby staged diffusion. is provided in a plurality of planes at various distances from the engine nozzle, as the exhaust stream strikes the rungs of the cribwork and iabroken up thereby. Such a diffusing screen, when formed .of corrosionresistant carbon steel rungs, will satisfactorily withstand the exhaust temperature of the usual jet engine, of the order of ll50 F. 'With a rocket engine, however, the temperature of the exhaust gases is much higher, and a jet engine with an atterburner in operation discharges gas at a temperature of the order 053150? F. To use the previous "diffusing screen at such high temperatures it is necessary th'at it be formed of tubular rungs with a coolant flowing theretln'ough, to prevent it from being destroyed by the heat.
However, the use of a coolant, usually water, necessitate's many connections, a circulating system, and a source of supply, and in addition limits the movability of the sound suppressor. There are many occasions for the use of noise suppressor where such cumbersomeness is .undesirable, or where a supply of coolant is not readily available.
It is therefore a principal object of this invention to provide a difiusing screen for an exhaust noise suppressor which may be used at elevated temperatures without cooling. I i
It is a further object to provide an uncooled diffusing screen suitable for use with afterburner operation.
I, Stillanother object is the provision of a diffusing screen of high mechanical strength at elevated temperatures.
Yet another object is to provide a diffusing screen not subject to corrosion from afterburner exhaust.
A further object is to provide a diiiusing screen resistant to thermal shock.
The foregoing objectsand advantages and others ancillary thereto will be better understood on reading the following specification in connection with the accompanying drawings, in which FIGURE 1 is a longitudinal cross-sectional elevation of an exhaust noise suppressor;
FIGURE 2 is a view of one of the difiusing rungs of the present invention; 7 V
FIGURE 3 is a perspective view, partially broken away, of one of the diffusing rungs;
FIGURE 4- is a transverse cross-section of another embodiment of the rung; and
FIGURE 5 is a perspective view of the three-dimensional labyrinthine cribwork diliusing screen.
axially therewith, anda. stack ldqangulariy disposedflto the expansion chamber and communicating therewith.
.An annular resonant chamber ll3surrcunds the upper portion of the stack and cornmunicates with the-interior. thereof through suitable apertures 18a. The expansion chamber and; the stack 7 are both double-walled and, have acoustical packing material .19 1 disposed between the walls; the inner walls 20, arepreferably offstainless steel and are providedrwith apertures, indicated atZila, to allow acoustical access to the packing, The outer walls may be of mild steelorother suitablematerial.
A three-dimensional, labyrinthine cribwork diffusing screen 16 (later to be describedindetail) is positioned within the inner diameter of the entrance section 12, in such a manner that the rearrnost extension of-thescreen is at the plane of entrance into expansion chamber 13. The screen is of suchdimensions in the transverse direction that it substantially spans the inner diameter, of portion 12, and itrnay be mounted onthe inner wall thereof by any convenient structural elements, in the present case a.generallyrectangular frame 22. A grid i simple crisscross pattern. and circular outline is adjustably positioned within the expansion section, disposed on the horizontal axis thereof and transverse to said axis. The grid may be supported and maintained in the selected position bya spider 31 as shown, or by othersuitable structural elements.
The grid is nominally positioned approximately halfway betweenthe diffuser screen and. thestackfentrance,
but is provided wit h means for translating, it along the axis of the expansion chamber so thatrits operating position may; beeither upstream or downstream .from its nominal position, according to theflow conditions encountered. Suitable translating means may be the slotted brackets 32 to which the ends of the spider are bolted, or any other desired means of well hn'own kind.
The op'erationlof the exhaust noise suppressor is as follows. The suppressor is placedinapposition to a reactioncngine 21 with the exhaust nozzle intromitted within the entrance portion, substantially, coaxial therewith. When the engine is operated the exhaust is discharged into the suppressor entrance section 12 passing through the cribwork diffusing screen in a plurality of labyrinthine paths, whereby its velocity is greatly diminished, and it is diverted from the axialdirection and expands with considerable turbulence into the expansion chamber. At the same time, the high velocity of the exhaust leaving the nozzle, in combination with the internal diameter of the entrance section and the restricted converging throatdefined by the nozzle and the frustoconicalinternal wall 2-5 disposed inside the entrance section, causes'external air to be aspirated into the suppressor.
Such aspirated air serves a double purpose. It cools the exhaust somewhat and assists in diffusing it and in creating turbulence and expansion downstream from the screen; also, owing to the high exit speed of the exhaust from the nozzle,'the aspirated air will pass through the converging throat at a speed of Mach 1 or higher. Selfnoise generated by the impingement of the exhaust stream on the diffusing screen cannot be radiated upstream against an inflow of air at Mach 1 or above. n the event that perfect adjustment between the engine and the suppressor has not been achieved and. the aspirated air may not quite reach Mach 1, sound baffles 26 are pro vided in the upstream portion of the entrance section, attached to the inner wall thereof and extending radially inward, and so disposed that any self-noise which may be radiated upstream will be absorbed by the baffles.
After the initial expansion of the exhaust in the expansion chamber just downstream from the diffusing screen, there is some tendency for the central portion of it to re-form into a jet stream, although at lower velocity. This central portion now passes through the resistance grid 17, which is of considerably smaller diameter than the expansion chamber, in order not to impede the flow of peripheral, expanded, and diffused exhaust. The central stream of exhaust gas undergoes a second immediate diffusion and expansion, with further diminution of velocity, as a result of passing through the grid. The fully diffused exhaust now passes through the remainder of the expansion chamber and the stack, with further expansion and reduction of velocity, and with absorption of noise in the range of 300600 c.p.s. by the resonant chamber. Upon exit from the stack the overall sound pressure level has been reduced, with present jet engines, by as much as 22 to 30 decibels, and in certain octave bands, particularly the third and fourth, the reduction may be as much as 40 decibels.
When such a noise suppressor is employed with the usual jet engine without afterburning, a diffusing screen having solid rungs of corrosion-resistant steel is satisfactory, and with afterburning, tubular rungs having an internal coolant fiowing therethrough, both such screens having been described and claimed in the aforementioned copending application Serial No. 65,389. However, it is sometimes desired to use a noise suppressor without cooling in conjunction with a rocket engine or an afterburning engine, where the temperature of exhaust gases may be over 3000 F., and for this use the three-dimensional labyrinthine cribwork dilfusing screen must be able to withstand the high temperature. Such a screen will now be described.
FIGURES 2 and 3 show one of the rungs of the diffusing screen of this invention. There is provided a rod 37 which serves as the structural element of the rung and supports the other elements against the thrust of the exhaust stream. The material of which such a rod is formed must be resistant to corrosion, oxidation, and thermal shock, and must retain its strength at elevated temperatures. Various metals such as corrosion-resistant steels and other alloys having these properties are known and are suitable for such use. A particularly satisfactory material is the alloy sold under the name lnconel 700, a registered trademark of the International Nickel Company, having the following composition:
Percent Carbon 0.10
Manganese 0.05 Silicon 0.2 Chromium 15.0 Titanium 2.0
Aluminum 30 Cobalt 23.0 Molybdenum 3.0 Iron 0.5 Nickel Balance Inconel 700 has a melting point around 2500 F., and a rupture life at 1800 F. of five hours under stress of 10,000 p.s.i. or ninety hours under stress of 6000 p.s.i. Although the exhaust temperature may be higher than the melting point of the metal, the rung is so formed that the metal is insulated from a large part of the heat, and the material directly exposed to the hot gases is well able to withstand the temperatures reached in afterburning operation.
Rod 37 is surrounded by a plurality of cylindrical sleeves 38 threaded end-to-end on the rod and formed of a material of high melting point and high resistance to thermal shock. Various ceramics and cermets possess the desired characteristics; a material which has been d found particularly suitable for the sleeves is silicon carbide, especially when sintered with a silicon nitride binder, having a melting point above 4892 F., and being very little affected by thermal shock.
The sleeves are of such internal diameter as to leave an appreciable annularspace between the sleeves and the rod when they are positioned coaxially thereon. This annular space is filled with an insulating material 39 of high melting point and a low coeflicient of heat transfer. Although various ceramic and cermet materials are suitable for this purpose, powdered zirconium oxide has been found particularly satisfactory, with a melting point of about 4892" F. The insulating material is retained within the annular space by a small annulus of cement 41 at each end of each sleeve. Powdered zirconium oxide with a binder of sodium silicate makes a suitable cement.
If the entire cribwork diffusing screen is to be assembled at once, no further structure for the individual rungs is required. However, it is often desirable to manufacture a quantity of rungs which may be handled as units, and even though the sleeves are cemented at each end they may not be very firmly attached to the central rod. For this reason, a metal flange 4-2 may be welded, brazed, or otherwise securely fastened around the rod at each end of the assemblage of sleeves, leaving a length of rod protruding therefrom at each end for positioning the rungs in the cribwork.
FIGURE 4 is a transverse cross-section of another embodiment 36a of one of the rungs. In this embodiment the elements of the rung are the same as previously described, comprising a rod 37, a plurality of sleeves 33, insulating material 39, and cement 41, but these elements are differently assembled. Instead of the sleeves being positioned coaxial with the rod, they are positioned with the sleeves being coaxial with each other, but with the rod disposed off center and in contact with the inner wall of the sleeves, tangent thereto, leaving a space of lune-shaped cross-section between the rod and the sleeves. This space of lune-shaped section is filled with insulating material and stopped with cement at each end of each sleeve as before. Rungs 36a may also be provided with end flanges 42. The advantage of this construction is that rungs 30a may be assembled in the cribwork screen in such a manner that the exhaust blast impinges on them on the side furthest from the metal and having the largest amount of insulating material upstream from the rod.
FIGURE 5 shows a three-dimensional labyrinthine cribwork diffusing screen 16, completely assembled and ready for installation in an exhaust noise suppressor. There is provided a generally rectangular frame 22 having sides of flat metal plates welded or otherwise joined, and preferably having beveled corners 43 for attachment to the inner diameter of the entrance portion of the suppressor, the diagonal dimensions of the frame being such as to provide a suitable fit therein.
The sides of the frame are bored for positioning a plurality of ranks of rungs 36 or 365a, the free ends of the rods 37 projecting outwardly through the bored apertures. The rods or the flanges may be welded or brazed to the frame at the points of contact, if desired. In the embodiment shown there are six such ranks. The first rank 46a comprises a plurality of parallel rungs spanning the frame with the rod ends positioned. by the apertures, the rungs being equally spaced apart with the center rung on the vertical centerline, in the same plane, and with the outermost rungs just inside the bevels at the corners.
The second rank 46b comprises a plurality of similar rungs, parallel to each other and similarly spaced, but crossing those of the first rank at substantially in a plane behind or downstream from that of the first rank, the center rung being on the horizontal centerline. A third rank 450 is provided having rungs parallel to those of the first rank, but in a plane downstream from the second rank; the center rung is again on the vertical centerline, but the flanking rungs are positioned somewhat closer together than those of the first rank. A fourth rank 46d of similar rungs is provided in a plane behind the third rank, substantially normal thereto but .having the same spacing as the third rank. A fifth rank 46a is provided in a plane behind the fourth, parallel to the third rank and having the center rung on centerline, but spaced more closely together, so that the flanking rungs are positioned more inwardly than those of the third rank. The sixth and last rank 46f occupies a plane behind the fifth rank, the rungs being normal to those of the fifth but similarly spaced.
The foregoing construction provides a three-dimensional'lattice or cribwork, with none of the rungs except the center ones occluding anyparallel rung in the axial directioinand so arranged that the exhaust stream in passing therethrough is broken up and takes a plurality of labyrinthine paths, with a plurality of minor shocks,
arising in different planes of depth, at afplurality of transverse locations.
It is to be understood that this particular design of six ranks of rungs has been adopted for convenience, and that the diffusing screen may be made with more or less ranks of rungs, with more or less rungs, in each rank, and with rungs of the form of either 36 or 36a. Spacing may also be diiierent, and the rungs may be arranged .so that none of them occlude each other. It'is immaterial which rungs may be vertical in the operating position of the screen, or whether any are. The rungs may, if desired,
be made of varying lengths as shown, so that they more or less completely span that portion of the entrance section in'which they are positioned.
The reason for using a plurality ofceramic sleeves 2. The combination recited in claim 1, wherein the inner diameter of said sleeves is tangent to the surface of said rod at one side, said sleeves and said rod defining opposite to the-tangency a space of lune-shaped crosssection, said powdered ceramic heat-insulating material being disposed in said space.
3. The combination recited in claim 1, wherein said sleeves are formed of silicon carbide and said insulating material is zirconium oxide. i
4. The combination recited in claim 2,-wherein said sleeves are formed of silicon carbide and said insulating material is zirconium oxide.
5. A three-dimensional labyrinthine cribwork diffusing screen for an exhaust noise suppressor, comprising in combination a plurality of ranks of rungs; each of said ranks comprising a plurality of parallel rungs spaced apart from each other in a plane; said ranks beingstacked in laminar fashion; each of saidrungs comprising a straight metal rod, a plurality of cylindrical ceramic sleeves having a fusing temperature above 3200" F. disposed in end-to-end relationship and surrounding said rod and defining with said rod a space between said rod and said sleeves, and a powdered ceramic heat-insulating material having a fusing temperature above 3200 F. disposed in said space 6. Thecombination recited in claim 5,;wherein said sleeves are formed of silicon carbide and said insulating material is Zirconiumoxide. I i
7. A three-dimensionai labyrinthine cribwork diffusing screen for an exhaust noise suppressor, comprising in combination a plurality of ranks of rungs; each of said ranks comprising a plurality of parallel rungs spaced rather than a single one is that under the enormous pressure of an exhaust stream some flexibility of the rungs is desirable, which would not be provided by a single sleeve. However, if it is desired to use the screen with a reaction engine of relatively low thrust, rungs having single continuous sleeves may be employed. The exterior surface of thesleeves may also be given an oxidationresistant coating of flame-sprayed refractory material,
such as aluminum oxide, zirconium oxide, molybdenum disilicide, or molybdenum diboride.
Although the improved three-dimensional labyrinthine cribwork diffusing screen has been described above in a preferred embodiment, it will be understood that various changes and modifications may be made by those skilled in the art Without departing from the scope of the invention. It is intended to cover all such modifications by the appended claims.
. apart from each other in a plane; said ranks being stacked ture above 3200 F. disposed in said space. Y
References Cited in the file of this patent UNITED STATES PATENTS 2,445,231 McDermott July 13, 1948 2,864,455 Hirschorn Dec. 16, 1958 2,956,399 Beighleyns Oct. 18, 1960 2,956,637 Lemmerman Oct. 18, 1960 2,977,265 Forsberg et al Mar. 28, 1961 3,011,584 Lemmerman et al Dec. 5, 1961 OTHER REFERENCES Technical Note 4033, Natl. Advisory Committee for Aeronautics, July 1947.

Claims (1)

  1. 5. A THREE-DIMENSIONAL LABYRINTHINE CRIBWORK DIFFUSING SCREEN FOR AN EXHAUST NOISE SUPPRESSOR, COMPRISING IN COMBINATION A PLURALITY OF RANKS OF RUNGS; EACH OF SAID RANKS COMPRISING A PLURALITY OF PARALLEL RUNGS SPACED APART FROM EACH OTHER IN A PLANE; SAID RANKS BEING STACKED IN LAMINAR FASHION; EACH OF SAID RUNGS COMPRISING A STRAIGHT METAL ROD, A PLURALITY FO CYLINDRICAL CERAMIC SLEEVES HAVING A FUSING TEMPERATURE ABOVE 3200*F. DISPOSED IN END-TO-END RELATIONSHIP AND SURROUNDING SAID ROD AND DEFINING WITH SAID ROD A SPACE BETWEEN SAID ROD AND
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Cited By (21)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1271466B (en) * 1965-01-11 1968-06-27 Koppers Co Inc Diffuser that can be used in particular for use in silencer devices behind recoil engines between an inlet part and a vent part
US3708036A (en) * 1970-05-11 1973-01-02 Bertin & Cie Apparatus for attenuating the noise made by fluid jets ejected from a conduit
US3830335A (en) * 1973-05-14 1974-08-20 Nasa Noise suppressor
US4064963A (en) * 1975-05-30 1977-12-27 Vereinigte Metallwerke Ranshofen-Berndorf Aktiengesellschaft Exhaust for internal-combustion engine
US4733751A (en) * 1985-12-27 1988-03-29 General Dynamics, Pomona Division Rocket exhaust disrupter
US4747467A (en) * 1986-04-01 1988-05-31 Allied-Signal Inc. Turbine engine noise suppression apparatus and methods
US4753319A (en) * 1985-10-16 1988-06-28 Nuovopignone S.P.A. Exhaust silencer for high-power gas turbines
US5715672A (en) * 1996-04-01 1998-02-10 Braden Manufacturing Exhaust silencer panel for gas turbine
US5837890A (en) * 1994-12-12 1998-11-17 Aero Systems Engineering, Inc. Jet engine test cell structure
US6530221B1 (en) * 2000-09-21 2003-03-11 Siemens Westinghouse Power Corporation Modular resonators for suppressing combustion instabilities in gas turbine power plants
US20080202848A1 (en) * 2005-08-08 2008-08-28 Alstom Technology Ltd Sound absorber for gas turbine installations
US7482705B2 (en) * 2003-05-12 2009-01-27 Piercey Iii Gerald S Generator support plenum
US20090277714A1 (en) * 2008-05-09 2009-11-12 Siemens Power Generations, Inc. Gas turbine exhaust sound suppressor and associated methods
US20110048847A1 (en) * 2009-09-02 2011-03-03 United States Of America As Represented By The Secretary Of The Navy Noise attenuation device for reducing noise attenuation in a jet engine test cell
US8307943B2 (en) * 2010-07-29 2012-11-13 General Electric Company High pressure drop muffling system
US8430202B1 (en) 2011-12-28 2013-04-30 General Electric Company Compact high-pressure exhaust muffling devices
US8511096B1 (en) 2012-04-17 2013-08-20 General Electric Company High bleed flow muffling system
US8550208B1 (en) 2012-04-23 2013-10-08 General Electric Company High pressure muffling devices
US8939253B1 (en) * 2012-04-27 2015-01-27 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration System and method for suppression of unwanted noise in ground test facilities
US20150377139A1 (en) * 2012-03-14 2015-12-31 Mitsubishi Heavy Industries, Ltd. Exhaust flue
US9399951B2 (en) 2012-04-17 2016-07-26 General Electric Company Modular louver system

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US2445231A (en) * 1944-09-09 1948-07-13 Johns Manville Method of and apparatus for making tubular coverings
US2864455A (en) * 1955-04-13 1958-12-16 Hirschorn Martin Exhaust noise abatement apparatus
US2956399A (en) * 1956-11-16 1960-10-18 Clair M Beighley Fluid cooled homogeneous ceramic rocket motor wall structure
US2956637A (en) * 1959-04-23 1960-10-18 Koppers Co Inc Sound attenuating device
US2977265A (en) * 1957-06-19 1961-03-28 Hexcel Products Inc Ceramic structure and method of making same
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US2445231A (en) * 1944-09-09 1948-07-13 Johns Manville Method of and apparatus for making tubular coverings
US2864455A (en) * 1955-04-13 1958-12-16 Hirschorn Martin Exhaust noise abatement apparatus
US2956399A (en) * 1956-11-16 1960-10-18 Clair M Beighley Fluid cooled homogeneous ceramic rocket motor wall structure
US2977265A (en) * 1957-06-19 1961-03-28 Hexcel Products Inc Ceramic structure and method of making same
US3011584A (en) * 1957-12-16 1961-12-05 Koppers Co Inc Sound attenuating device
US2956637A (en) * 1959-04-23 1960-10-18 Koppers Co Inc Sound attenuating device

Cited By (28)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1271466B (en) * 1965-01-11 1968-06-27 Koppers Co Inc Diffuser that can be used in particular for use in silencer devices behind recoil engines between an inlet part and a vent part
US3708036A (en) * 1970-05-11 1973-01-02 Bertin & Cie Apparatus for attenuating the noise made by fluid jets ejected from a conduit
US3830335A (en) * 1973-05-14 1974-08-20 Nasa Noise suppressor
US4064963A (en) * 1975-05-30 1977-12-27 Vereinigte Metallwerke Ranshofen-Berndorf Aktiengesellschaft Exhaust for internal-combustion engine
US4753319A (en) * 1985-10-16 1988-06-28 Nuovopignone S.P.A. Exhaust silencer for high-power gas turbines
US4733751A (en) * 1985-12-27 1988-03-29 General Dynamics, Pomona Division Rocket exhaust disrupter
US4747467A (en) * 1986-04-01 1988-05-31 Allied-Signal Inc. Turbine engine noise suppression apparatus and methods
US5837890A (en) * 1994-12-12 1998-11-17 Aero Systems Engineering, Inc. Jet engine test cell structure
US5715672A (en) * 1996-04-01 1998-02-10 Braden Manufacturing Exhaust silencer panel for gas turbine
US6530221B1 (en) * 2000-09-21 2003-03-11 Siemens Westinghouse Power Corporation Modular resonators for suppressing combustion instabilities in gas turbine power plants
US20050166596A1 (en) * 2000-09-21 2005-08-04 Sattinger Stanley S. Resonator adopting counter-bored holes and method of suppressing combustion instabilities
US7194862B2 (en) 2000-09-21 2007-03-27 Siemens Power Generation, Inc. Resonator adopting counter-bored holes and method of suppressing combustion instabilities
US20070125089A1 (en) * 2000-09-21 2007-06-07 Siemens Power Generation, Inc. Method of suppressing combustion instabilities using a resonator adopting counter-bored holes
US7549506B2 (en) 2000-09-21 2009-06-23 Siemens Energy, Inc. Method of suppressing combustion instabilities using a resonator adopting counter-bored holes
US7482705B2 (en) * 2003-05-12 2009-01-27 Piercey Iii Gerald S Generator support plenum
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
US20090277714A1 (en) * 2008-05-09 2009-11-12 Siemens Power Generations, Inc. Gas turbine exhaust sound suppressor and associated methods
US7717229B2 (en) * 2008-05-09 2010-05-18 Siemens Energy, Inc. Gas turbine exhaust sound suppressor and associated methods
US20110048847A1 (en) * 2009-09-02 2011-03-03 United States Of America As Represented By The Secretary Of The Navy Noise attenuation device for reducing noise attenuation in a jet engine test cell
US8307943B2 (en) * 2010-07-29 2012-11-13 General Electric Company High pressure drop muffling system
US8430202B1 (en) 2011-12-28 2013-04-30 General Electric Company Compact high-pressure exhaust muffling devices
US20150377139A1 (en) * 2012-03-14 2015-12-31 Mitsubishi Heavy Industries, Ltd. Exhaust flue
US9970358B2 (en) * 2012-03-14 2018-05-15 Mitsubishi Heavy Industries, Ltd. Exhaust flue
US8511096B1 (en) 2012-04-17 2013-08-20 General Electric Company High bleed flow muffling system
US9399951B2 (en) 2012-04-17 2016-07-26 General Electric Company Modular louver system
US8550208B1 (en) 2012-04-23 2013-10-08 General Electric Company High pressure muffling devices
US8939253B1 (en) * 2012-04-27 2015-01-27 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration System and method for suppression of unwanted noise in ground test facilities

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