NO751949L - - Google Patents
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- Publication number
- NO751949L NO751949L NO751949A NO751949A NO751949L NO 751949 L NO751949 L NO 751949L NO 751949 A NO751949 A NO 751949A NO 751949 A NO751949 A NO 751949A NO 751949 L NO751949 L NO 751949L
- Authority
- NO
- Norway
- Prior art keywords
- silencer
- sound
- layer
- muffler
- perforated
- Prior art date
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Classifications
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01N—GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR MACHINES OR ENGINES IN GENERAL; GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR INTERNAL-COMBUSTION ENGINES
- F01N13/00—Exhaust or silencing apparatus characterised by constructional features
- F01N13/18—Construction facilitating manufacture, assembly, or disassembly
- F01N13/1838—Construction facilitating manufacture, assembly, or disassembly characterised by the type of connection between parts of exhaust or silencing apparatus, e.g. between housing and tubes, between tubes and baffles
- F01N13/1844—Mechanical joints
- F01N13/1855—Mechanical joints the connection being realised by using bolts, screws, rivets or the like
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01N—GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR MACHINES OR ENGINES IN GENERAL; GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR INTERNAL-COMBUSTION ENGINES
- F01N1/00—Silencing apparatus characterised by method of silencing
- F01N1/08—Silencing apparatus characterised by method of silencing by reducing exhaust energy by throttling or whirling
- F01N1/10—Silencing apparatus characterised by method of silencing by reducing exhaust energy by throttling or whirling in combination with sound-absorbing materials
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01N—GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR MACHINES OR ENGINES IN GENERAL; GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR INTERNAL-COMBUSTION ENGINES
- F01N13/00—Exhaust or silencing apparatus characterised by constructional features
- F01N13/009—Exhaust or silencing apparatus characterised by constructional features having two or more separate purifying devices arranged in series
- F01N13/0097—Exhaust or silencing apparatus characterised by constructional features having two or more separate purifying devices arranged in series the purifying devices are arranged in a single housing
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01N—GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR MACHINES OR ENGINES IN GENERAL; GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR INTERNAL-COMBUSTION ENGINES
- F01N13/00—Exhaust or silencing apparatus characterised by constructional features
- F01N13/18—Construction facilitating manufacture, assembly, or disassembly
- F01N13/1805—Fixing exhaust manifolds, exhaust pipes or pipe sections to each other, to engine or to vehicle body
- F01N13/1811—Fixing exhaust manifolds, exhaust pipes or pipe sections to each other, to engine or to vehicle body with means permitting relative movement, e.g. compensation of thermal expansion or vibration
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01N—GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR MACHINES OR ENGINES IN GENERAL; GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR INTERNAL-COMBUSTION ENGINES
- F01N13/00—Exhaust or silencing apparatus characterised by constructional features
- F01N13/18—Construction facilitating manufacture, assembly, or disassembly
- F01N13/1888—Construction facilitating manufacture, assembly, or disassembly the housing of the assembly consisting of two or more parts, e.g. two half-shells
- F01N13/1894—Construction facilitating manufacture, assembly, or disassembly the housing of the assembly consisting of two or more parts, e.g. two half-shells the parts being assembled in longitudinal direction
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01N—GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR MACHINES OR ENGINES IN GENERAL; GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR INTERNAL-COMBUSTION ENGINES
- F01N2310/00—Selection of sound absorbing or insulating material
- F01N2310/02—Mineral wool, e.g. glass wool, rock wool, asbestos or the like
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01N—GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR MACHINES OR ENGINES IN GENERAL; GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR INTERNAL-COMBUSTION ENGINES
- F01N2450/00—Methods or apparatus for fitting, inserting or repairing different elements
- F01N2450/24—Methods or apparatus for fitting, inserting or repairing different elements by bolts, screws, rivets or the like
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01N—GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR MACHINES OR ENGINES IN GENERAL; GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR INTERNAL-COMBUSTION ENGINES
- F01N2470/00—Structure or shape of exhaust gas passages, pipes or tubes
- F01N2470/02—Tubes being perforated
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01N—GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR MACHINES OR ENGINES IN GENERAL; GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR INTERNAL-COMBUSTION ENGINES
- F01N2490/00—Structure, disposition or shape of gas-chambers
- F01N2490/02—Two or more expansion chambers in series connected by means of tubes
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Exhaust Silencers (AREA)
- Soundproofing, Sound Blocking, And Sound Damping (AREA)
Description
GasstromninqslyddemperGas flow muffler
Støykontrollens historie har vært en utvikling av trinnvis teknologisk forbedring med samtidig progressiv erkjennelse av den fysiologiske, psykologiske og sosiologiske nødvendig-het av å begrense de stoynivå som folk utsettes for. De vi-tenskapelige prinsipper involvert tas og kombineres fra felt som akustikk, pneumatikk og hydraulikk. På samme måte som i mekanikken kombineres kjente fysiske midler på nye måter med dimensjons- bg andre konstruksjonskriteria som oppdages for å gi stadig bedre resultater. The history of noise control has been a development of step-by-step technological improvement with simultaneous progressive recognition of the physiological, psychological and sociological necessity of limiting the noise levels to which people are exposed. The scientific principles involved are taken and combined from fields such as acoustics, pneumatics and hydraulics. In the same way as in mechanics, known physical means are combined in new ways with dimensions and other construction criteria that are discovered to give increasingly better results.
På det spesielle felt som vedrorer behandling og kontroll av gasstrommer, spesielt pulserende eller trykk- og/eller has-tighetsforstyrret stromning, er det nodvendig å takle kompli-serte problemer vedrorende eliminasjon eller i det minste hoy dempning av lydfrekvenssystemer såvel som utjevning og end-ring på andre måter av stromningen for å unngå generering av stoy direkte på utstromning til atmosfæren eller indirekte ved forårsaking av stoy som skaper vibrasjoner i mekanisk ut-styr. Samtidig må dannelse av sekundær stoy i selve lyddemperen eller andre behandlingsinnretninger unngås. In the special field relating to the treatment and control of gas drums, especially pulsating or pressure- and/or velocity-disturbed flow, it is necessary to tackle complicated problems relating to the elimination or at least high attenuation of sound frequency systems as well as equalization and end- ring off the flow in other ways to avoid the generation of noise directly on discharge into the atmosphere or indirectly by causing noise that creates vibrations in mechanical equipment. At the same time, the formation of secondary noise in the silencer itself or other treatment devices must be avoided.
Det er et formål ved foreliggende oppfinnelse å tilveiebringe en lyddemper for kontroll av den eksisterende eller potensielle stoy i en gasstrom og som er i stand til å absorbere stoy oppstroms og jevne ut uregelmessig stromning for å unngå dannelse av stoy nedstroms, mens det samtidig unngås at sekundær stoy dannes i selve lyddemperen. Anordningen er i stand til å behandle stromninger med svært varierende trykk og hastighets-egenskaper, inklusive stotbolger. It is an object of the present invention to provide a silencer for controlling the existing or potential noise in a gas stream and which is able to absorb noise upstream and smooth out irregular flow to avoid the formation of noise downstream, while at the same time avoiding that secondary noise is formed in the silencer itself. The device is able to process flows with highly varying pressure and velocity characteristics, including shock waves.
Et ytterligere formål med oppfinnelsen er å tilveiebringe en slik lyddemper som har lang og pålitelig levetid. Et annet A further object of the invention is to provide such a silencer which has a long and reliable lifetime. Another
formål er å tilveiebringe en slik fleretrinns lyddemper, til [ hvilken kan tilfoyes ett eller flere trinn for å gi mer full-stendig lyddempning etter hvert som stoyforurensningsstandar-dene blir strengere. Et annet formål er å tilveiebringe en slik lyddemper som har meget hbyt forhold mellom ytelse og storr el se. — Fig. 1 viser et sideriss av en typisk lyddemper ifolge oppfinnelsen. Fig. 2 er et langsgående snitt av lyddemperen på fig. 1. Fig. 3 viser i forstorret målestokk oppbygningen og virkningen av den sjokkabsorberende seksjon av enheten. Fig. 3Å og 3B viser detaljer av henholdsvis perforasjonsmons-tre for de indre mantler og av diffusorene i full storrelse. Fig. 4 og 5 viser detaljerte snitt av alternative former for vibrasjonsisolerende forbindelser mellom tilstotende seksjoner av lyddemperen, idet konstruksjonen på fig. 1 og 2 er den som er vist på fig. 4. purpose is to provide such a multi-stage silencer, to which one or more stages can be added to provide more complete sound attenuation as the noise pollution standards become stricter. Another purpose is to provide such a silencer which has a very high ratio between performance and size. - Fig. 1 shows a side view of a typical silencer according to the invention. Fig. 2 is a longitudinal section of the silencer in fig. 1. Fig. 3 shows on an enlarged scale the construction and the effect of the shock-absorbing section of the unit. Fig. 3A and 3B show details of the perforation patterns for the inner mantles and of the diffusers in full size, respectively. Figs. 4 and 5 show detailed sections of alternative forms of vibration-isolating connections between adjacent sections of the silencer, the construction in fig. 1 and 2 is the one shown in fig. 4.
Fig. 6 er en adskilt fremstilling av en "tilleggsenhet".Fig. 6 is a disassembled representation of an "additional unit".
Fig. 7 er et sideriss av en modifisert lyddemper.Fig. 7 is a side view of a modified silencer.
Lyddemperen vist på fig. 1 til 4 er en toseksjons enhet som omfatter sylindriske mantler 1 og 2 med innlopsenden lukket av et deksel 3. Et forstetrinns diffusorror 4 er sveiset til dekslet, og en standard forbindelsesflens 5 er sveiset til den utragende ende av diffusorroret. De sylindriske veggene av roret er perforert, og monsteret er vist i full storrelse på fig. 3B. En blende 6 med en åpning 7, hvis funksjon skal beskrives i det folgende, er vist liggende mot overflaten av flensen 5. The silencer shown in fig. 1 to 4 is a two-section unit comprising cylindrical shells 1 and 2 with the inlet end closed by a cover 3. A first stage diffuser tube 4 is welded to the cover, and a standard connecting flange 5 is welded to the projecting end of the diffuser tube. The cylindrical walls of the rudder are perforated, and the monster is shown in full size in fig. 3B. An aperture 6 with an opening 7, whose function will be described in the following, is shown lying against the surface of the flange 5.
De sammenstøtende ender av mantlene 1 og 2 er utstyrt med flenser 8 og 9. En skillevegg 10 med en sentral åpning 11 og I en perifer flens 12 er montert ved overgangen mellom lyddem- The abutting ends of the casings 1 and 2 are equipped with flanges 8 and 9. A partition wall 10 with a central opening 11 and a peripheral flange 12 is mounted at the transition between the sound dem-
perens forste og andre trinn ved hjelp av den perifere flensen, j Elastomere avstandsholdere 13 er innskutt mellom flensen 12 og' flensene 8 og 9 for forbindelsen strammes til ved hjelp av bolter 14. Hensikten med de elastomere avstandsholderne er å forhindre overforing av vibrasjon mellom mantlene bundet sammen av forbindelsen. the first and second stages of the pair by means of the peripheral flange, j Elastomeric spacers 13 are inserted between flange 12 and' flanges 8 and 9 for the connection is tightened by means of bolts 14. The purpose of the elastomeric spacers is to prevent the transmission of vibration between the jackets bound together by the compound.
Indre sylindriske mantler 15 og 16 er montert ved hjelp av ringer 17 i avstand fra mantlene 1 og 2. De indre mantlene er som vist perforert for å gi adgang fra det indre av lyddemperen til det materiale som er pakket inn i rammene mellom de indre mantler og lyddempermantlene. Disse materialers egenskaper og funksjon skal beskrives nærmere i det folgende. De indre mantlers perforasjonsmonster er vist i full skala på fig. 3A. Inner cylindrical casings 15 and 16 are mounted by means of rings 17 at a distance from the casings 1 and 2. The inner casings are, as shown, perforated to allow access from the interior of the silencer to the material packed in the frames between the inner casings and the muffler shrouds. The properties and function of these materials shall be described in more detail below. The inner mantle perforation sample is shown in full scale in fig. 3A.
Et andre trinns diffusorror 18 er montert i skilleveggens 10 åpning 11. Dette ror er som vist perforert på samme måte som det forste trinns diffusorror. A second stage diffuser rudder 18 is mounted in the opening 11 of the partition 10. This rudder is, as shown, perforated in the same way as the first stage diffuser rudder.
Et perforert indre deksel 19 er fortrinnsvis montert i avstand fra dekslet 3 og det rom som derved er fylt med lydabsorberende materiale, såsom en matte av kobber- eller stålfibre. Dessuten er mantelen 1 av lyddemperens forste seksjon omgitt . med to lag mantelvibrasjonsdempende materiale, såsom bly- eller asbestplate 21. Det er også anordnet en kappe av tynnplate. A perforated inner cover 19 is preferably mounted at a distance from the cover 3 and the space which is thereby filled with sound-absorbing material, such as a mat of copper or steel fibres. In addition, the casing 1 is surrounded by the silencer's first section. with two layers of casing vibration-damping material, such as lead or asbestos sheet 21. A cover made of thin sheet is also provided.
Selv om gasstromningslyddemperen ifolge oppfinnelsen kan for-bindes i en ledning, dvs. at dens innlop er forbundet med en tilforselskanal for gass og at dens utlop også er forbundet med en kanal, er anordningen vist på tegningen konstruert for å danne enden av gasstromningskanalen. Den indre og ytre mantel ved utlopsenden 22 av lyddemperen er åpen til atmosfæren. Although the gas flow silencer according to the invention can be connected in a line, i.e. that its inlet is connected to a supply channel for gas and that its outlet is also connected to a channel, the device shown in the drawing is constructed to form the end of the gas flow channel. The inner and outer casing at the outlet end 22 of the muffler is open to the atmosphere.
Gasstrommen, hvis egenskaper kan variere fra relativt jevn stromning til voldsomt pulserende stromning, fores inn i forste trinns diffusorroret 4. Siden nedstromsenden av roret er lukket, tvinges gassene til å stromme radialt utover gjennom The gas drum, whose properties can vary from relatively steady flow to violently pulsating flow, is fed into the first stage diffuser tube 4. Since the downstream end of the tube is closed, the gases are forced to flow radially outward through
rorets perforasjoner. I lopet av hver puls rettes gassene i et stort antall individuelle stråler mot den indre kappen 15. rudder perforations. In the course of each pulse, the gases are directed in a large number of individual jets towards the inner casing 15.
Rommet 23 som omslutter diffusorroret, er fylt med et holdbart I materiale, såsom metallspon eller kobberskrap, som gir mange små rom i forbindelse med hverandre. Selv om det bidrar til absorpsjon av lydvibrasjoner i gassene fra oppstroms kilder, er dette roms hovedfunksjon å motta og dempe stotet av strå-lene fra diffusorroret 4. Med andre ord, selv om lydabsorpsjon er en onskelig egenskap ved materiale som inneholdes i rommet 23, er denne egenskap delvis ofret for å oppnå motstand mot odeleggelse av gassene som med hoy hastighet strommer gjennom perforasjonene av den indre mantelen 15 og inn i rommets små tomrom. Rommet 24, som befinner seg nedstroms for diffusoren, men som likevel er en del av lyddemperens forste sjokkseksjon, er fortrinnsvis fylt med et lydabsorberende materiale av hold-bar type. Lydenergi absorberes av materialet i rommene 23 og 24 og også av det lydabsorberende materiale 20 som også står i forbindelse med rommet i lyddemperens forste trinn. The space 23 which encloses the diffuser tube is filled with a durable material, such as metal shavings or copper scrap, which provides many small spaces in connection with each other. Although it contributes to the absorption of sound vibrations in the gases from upstream sources, this space's main function is to receive and dampen the shock of the rays from the diffuser tube 4. In other words, although sound absorption is a desirable property of material contained in the space 23, this property is partly sacrificed in order to achieve resistance to destruction by the gases which flow at high speed through the perforations of the inner mantle 15 and into the small voids of the room. The space 24, which is located downstream of the diffuser, but which is nevertheless part of the silencer's front shock section, is preferably filled with a sound-absorbing material of the hold-bar type. Sound energy is absorbed by the material in the spaces 23 and 24 and also by the sound-absorbing material 20 which is also connected to the space in the silencer's first stage.
Behandlingen av stromningen i lyddemperens forste seksjon gir en delvis, men betydelig utjevning av gasstrommen etter plas-sering av de sjokk- og lydabsorberende partier. The treatment of the flow in the silencer's first section provides a partial but significant equalization of the gas volume after placement of the shock and sound absorbing parts.
Lyddemperens andre trinn er konstruert for ytterligere å dempe pulseringer og absorbere lydenergi som fremdeles eksisterer i gasstrommen idet den strommer fra det forste trinn inn i det andre trinns diffusorror 18. Selv om behandlingen i det andre trinn virker på samme måte som behandlingen i lyddemperens forste trinn, er vekten her endret fra sjokkdempning til lydabsorpsjon med fortsatt utjevning av stromningen for forberedelse av utstromning i atmosfæren med minimalt stoy-skapende stot. Lydenergien absorberes av et materiale som er bedre lydabsorberende enn materialet inneholdt i forste seksjon, såsom perforert filt eller glassfiber inneholdt i rommet 25. Stoy, hvis kilder befinner seg oppstroms for lyddemperen og stoy som kan dannes i gassystemet inne i lyddemperen, absorberes til et akseptabelt nivå for den når lyddemperens utlop. The muffler's second stage is designed to further dampen pulsations and absorb sound energy still present in the gas drum as it flows from the first stage into the second stage diffuser vane 18. Although the treatment in the second stage works in the same way as the treatment in the first stage of the muffler , the emphasis here is changed from shock absorption to sound absorption with continued smoothing of the flow in preparation for outflow into the atmosphere with minimal noise-creating noise. The sound energy is absorbed by a material that is better sound absorbing than the material contained in the first section, such as perforated felt or glass fiber contained in the space 25. Noise, whose sources are located upstream of the silencer and noise that can form in the gas system inside the silencer, is absorbed to an acceptable level before it reaches the muffler outlet.
Gasstromningslyddemperen må konstrueres slik at den ikke bare absorberer i så stor grad som mulig stoyenergi som når den fra I oppstroms kilder og jevner ut stromningen for å unngå dannelse j The gas flow silencer must be designed so that it not only absorbs as much as possible noise energy that reaches it from upstream sources and smooths the flow to avoid the formation of j
av stoy ved eller etter lyddemperens utlop, men også for å I unngå dannelse av stoy inne i selve lyddemperen. Dannelse av lavfrekvent stromningsstoy som har en tendens til å oppstå of noise at or after the muffler exits, but also to avoid the formation of noise inside the muffler itself. Formation of low-frequency current noise that tends to occur
når en strom med relativt hoy hastighet strommer inn i et stort volum, som f.eks. når en strom fra en innlopskanal strommer inn i et relativt stort lyddemperkammer, unngås i den her be-skrevne lyddemper. Innlopsstrommen deles i et stort antall stråler 26 (fig. 3), og det sjokkabsorberende materiale er anordnet noe forbi strålenes kjerner, såsom vist ved 27 i forstorret målestokk på fig. 3. Den foretrukne avstanden mellom innlopsroret 4 og den perforerte indre mantel 15 er fra fire til tyve ganger diameteren av perforasjonene i diffusorroret. Med denne utforming unngås skade på det sjokkabsorberende materiale på grunn av strålenes store kjernehastighet, og gassene mottas og behandles uten at det oppstår lavfrekvent stoy. Denne avstand kan være noe mindre eller noe storre med med-følgende tap av levetid for det sjokkabsorberende materiale eller akustisk ytelse av lyddemperen, men de angitte dimensjoner gir optimal virkning. when a stream with a relatively high speed flows into a large volume, such as e.g. when a current from an inlet channel flows into a relatively large silencer chamber, is avoided in the silencer described here. The inlet current is divided into a large number of jets 26 (fig. 3), and the shock-absorbing material is arranged somewhat beyond the cores of the jets, as shown at 27 on an enlarged scale in fig. 3. The preferred distance between the inlet pipe 4 and the perforated inner jacket 15 is from four to twenty times the diameter of the perforations in the diffuser pipe. With this design, damage to the shock-absorbing material is avoided due to the high core speed of the jets, and the gases are received and processed without causing low-frequency noise. This distance can be somewhat smaller or somewhat larger, with a consequent loss of life for the shock-absorbing material or acoustic performance of the silencer, but the stated dimensions give optimal effect.
Etter behandling av gasstrommen i det forste sjokktrinn av lyddemperen strommer gassene inn i det andre trinns diffusorror 18 og radialt derfra gjennom perforasjonene i dette. Perforasjonene i det andre trinns diffusorror er fortrinnsvis noe mindre, og roret er noe lengre sammenlignet med de til-svarende dimensjoner for det forste trinns diffusor. Dette resulterer i flere og mindre stråler. Selv om det andre trinns diffusorror gir ytterligere utjevning av strommen, er behandlingen i det andre trinn forst og fremst akustisk, After treatment of the gas drum in the first shock stage of the silencer, the gases flow into the second stage diffuser tube 18 and radially from there through the perforations therein. The perforations in the second stage diffuser rudder are preferably somewhat smaller, and the rudder is somewhat longer compared to the corresponding dimensions for the first stage diffuser. This results in more and smaller rays. Although the second stage diffuser rudder provides further smoothing of the flow, the treatment in the second stage is primarily acoustic,
dvs. absorpsjon av lydbolger som forplanter seg i gasstrommen. Rommet 25 er pakket med et effektivt lydabsorberende materiale, såsom hårfilt eller glassfiber. Som vist på fig. 1 er den blottlagte flate av det lydabsorberende materiale forlenget godt forbi den lukkede nedstroms ende av diffusorroret for å gi fortsatt absorbsjon av lydenergi etter som strommen sam-les for utlop i atmosfæren med relativt lav og jevn hastighet gjennom den åpne nedstroms ende av lyddemperen. Lyddemperen må nodvendigvis være konstruert for. å kunne behandle et for-utbestemt maksimum av strommende gasser. Selv om det kan I anordnes en ventil i den oppstroms kanal som forer til lyd- i.e. absorption of sound waves propagating in the gas chamber. Room 25 is packed with an effective sound-absorbing material, such as hair felt or fiberglass. As shown in fig. 1, the exposed surface of the sound-absorbing material is extended well past the closed downstream end of the diffuser pipe to provide continued absorption of sound energy as the stream is collected for discharge into the atmosphere at a relatively low and steady velocity through the open downstream end of the muffler. The silencer must necessarily be designed for. to be able to process a predetermined maximum of flowing gases. Although a valve can be arranged in the upstream channel that leads to the sound
demperen for å begrense stromningen, er det sannsynlig at se-kun dæ r stoy dannes nedstroms for ventilen. Dette kan unngås ved å benytte en blende 6 ved. innlopet til det forste trinns diffusorror. Den totale åpne flate som dannes av perforasjonene i diffusorroret står i forhold til storrelsen av blen-deåpningen 7. Dersom perforasjonene i det andre trinns diffusorror er noe mindre enn de i det forste diffusorroret, hvilket er å foretrekke, vil det totale åpne areal for stromning gjennom perforasjonene i det andre roret være tilnærmet det samme som for det forste roret for å gi optimalt resultat fordi strommen inn i det andre diffusorroret er adskiltig jevnere. the damper to limit the flow, it is likely that only then noise will form downstream of the valve. This can be avoided by using a shutter 6 wood. the inlet to the first stage diffuser vane. The total open surface formed by the perforations in the diffuser tube is proportional to the size of the aperture opening 7. If the perforations in the second stage diffuser tube are somewhat smaller than those in the first diffuser tube, which is preferable, the total open area for flow will through the perforations in the second rudder be approximately the same as for the first rudder to give optimal results because the flow into the second diffuser rudder is distinctly smoother.
For en totrinns lyddemper er det vanligvis kun nodvendig å anordne midler for forhindring av utstråling av stoy til atmosfæren fra mantelen for det forste trinn.eller sjokktrinn. Dette gjores ved å omgi mantelen 1 med vibrasjonsdempende For a two-stage silencer, it is usually only necessary to provide means for preventing the emission of noise into the atmosphere from the casing for the first stage or shock stage. This is done by surrounding the mantle 1 with vibration dampening
lag som beskrevet ovenfor. Overforing av vibrasjoner i det forste trinns mantel 1 til det andre trinns mantel 2 unngås i storre grad ved innskyting av elastomert materiale i forbindelsen mellom disse som beskrevet ovenfor, og den relativt jevnere strom av gass inn i og gjennom det andre trinn forår-saker vanligvis ikke problematiske vibrasjoner i mantelen. layer as described above. Transfer of vibrations in the first stage casing 1 to the second stage casing 2 is largely avoided by inserting elastomeric material in the connection between them as described above, and the relatively smoother flow of gas into and through the second stage usually causes no problematic vibrations in the casing.
En alternativ form for vibrasjonsisolerende forbindelse er vist på fig. 5. I dette arrangement overlapper endene av mantlene la og 2a og er festet til hverandre med en elastomer avstandshoIder 13a imellom som vibrasjonsbarriere. An alternative form of vibration isolating connection is shown in fig. 5. In this arrangement, the ends of the sheaths 1a and 2a overlap and are attached to each other with an elastomer spacer 13a in between as a vibration barrier.
Selv om det generelt sett er mer onskelig både fra omkost-nings- og ytelsesstandpunkt å konstruere lyddemperen med sylindriske mantler, kan disse alternativt være koniske som vist på fig. 7. De konstruksjonsbetraktninger som er beskrevet i forbindelse med lyddemperen vist på fig. 1 til 4 gjelder også for enheten vist på fig. 7 som adskiller seg stort sett bare ved at mantlene er koniske istedenfor sylindriske. Although it is generally more desirable, both from a cost and performance point of view, to construct the silencer with cylindrical casings, these can alternatively be conical as shown in fig. 7. The construction considerations described in connection with the silencer shown in fig. 1 to 4 also apply to the unit shown in fig. 7, which differ largely only in that the mantles are conical instead of cylindrical.
Utviklingen i de senere år har krevet stadig bedre lyddempning for å redusere stoyforurensning. Hva som kan aksepteres j og tolereres i dag er ikke tilstrekkelig til å mote morgen- Developments in recent years have required increasingly better sound attenuation to reduce noise pollution. What can be accepted j and tolerated today is not sufficient to fashion tomorrow-
I -I I - I
dagens mer strenge standarder. Med denne utvikling for bye, og sannsynligheten for at den vil fortsette i fremtiden, tar oppfinnelsen sikte på mulige fremtidige utvidelser ved til-foyélse av ett eller flere behandlingstrinn til den opprinne-lig installerte lyddemper som kan omfatte kun to trinn. Dette konsept er vist på fig. 6 hvor den opprinnelige totrinns enhet er utstyrt med en forbindelsesflens 28. Et tilleggstrinn 29 som omfatter en mantel 30 med en foring av lydabsorberende materiale 31, diffusorror 32 og forbindelseselementer, er vist i stilling for tilknytning til utlopsenden av den opprinnelige totrinns enhet. Dersom det er. onskelig på et senere tidspunkt, kan ett eller flere ytterligere trinn settes inn mellom den opprinnelige enhet og endetrinn 29. today's more stringent standards. With this development for the city, and the likelihood that it will continue in the future, the invention aims at possible future extensions by adding one or more processing steps to the originally installed silencer which may comprise only two steps. This concept is shown in fig. 6 where the original two-stage unit is equipped with a connecting flange 28. An additional stage 29 comprising a jacket 30 with a lining of sound-absorbing material 31, diffuser pipes 32 and connecting elements is shown in position for connection to the outlet end of the original two-stage unit. If it is. If desired at a later stage, one or more further stages may be inserted between the original unit and the end stage 29.
Lyddemperen vist på fig. 6 illustrerer et ytterligere alternativt konstruksjonstrekk. For ytterligere å lyddempe gasstrommen er et lydabsorberende element 33, som er inneholdt mellom et indre massivt ror 34 og et ytre perforert ror 35, anordnet som en forlengelse av diffusorroret 32. Utvidet lydabsorpsjon oppnås ved å la strommen passere gjennom den ringformede passasje som dannes av overflaten av det lydabsorberende element . The silencer shown in fig. 6 illustrates a further alternative design feature. To further dampen the sound of the gas drum, a sound absorbing element 33, which is contained between an inner solid tube 34 and an outer perforated tube 35, is arranged as an extension of the diffuser tube 32. Extended sound absorption is achieved by allowing the stream to pass through the annular passage formed by the surface of the sound-absorbing element.
Lyddemperen ifolge oppfinnelsen er meget fleksibel i bruk. Mens demping av relativt voldsom stromning er dens forse, er den også effektiv ved trykkreduksjon, såsom lyddemping av damp som under trykk strommer ut i atmosfæren. The muffler according to the invention is very flexible in use. While attenuation of relatively violent flow is its forte, it is also effective at pressure reduction, such as sound attenuation of pressurized steam escaping into the atmosphere.
Claims (10)
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US498984A US3894610A (en) | 1974-08-20 | 1974-08-20 | Gas stream silencer |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| NO751949L true NO751949L (en) | 1976-02-23 |
Family
ID=23983309
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| NO751949A NO751949L (en) | 1974-08-20 | 1975-06-03 |
Country Status (10)
| Country | Link |
|---|---|
| US (1) | US3894610A (en) |
| JP (1) | JPS51128501A (en) |
| CA (1) | CA1026239A (en) |
| DE (1) | DE2534556B2 (en) |
| DK (1) | DK140181B (en) |
| ES (1) | ES435717A1 (en) |
| FR (1) | FR2282533A1 (en) |
| GB (1) | GB1466512A (en) |
| NO (1) | NO751949L (en) |
| SE (1) | SE7507131L (en) |
Families Citing this family (32)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4180141A (en) * | 1975-11-24 | 1979-12-25 | Judd Frederick V H | Distributor for gas turbine silencers |
| US4105089A (en) * | 1975-11-24 | 1978-08-08 | Judd Frederick V H | Flow distributor for gas turbine silencers |
| US4045057A (en) * | 1976-02-02 | 1977-08-30 | Burgess Industries Incorporated | Vibration barrier/structural connector for conduits and the like |
| DE3144193A1 (en) * | 1981-11-06 | 1983-05-19 | Grünzweig + Hartmann und Glasfaser AG, 6700 Ludwigshafen | Sound-absorbing body, in particular for installation in silencers |
| IT1182270B (en) * | 1984-09-18 | 1987-10-05 | Luigi Carboni | SILENCER SYSTEM FOR EXHAUST GAS OF TERNA COMBUSTION ENGINES |
| CA1277604C (en) * | 1988-09-30 | 1990-12-11 | Heinz H. Rieger | Fireplace flue ambient noise reducing device |
| FR2642470A1 (en) * | 1989-01-27 | 1990-08-03 | Glaenzer Spicer Sa | SILENCER FOR EXHAUST GASES AND EXHAUST LINE PART COMPRISING SUCH SILENCER |
| KR0136305Y1 (en) * | 1996-09-10 | 1999-02-01 | 최진호 | Suction nozzle of a vacuum cleaner |
| FR2785360A1 (en) * | 1998-11-03 | 2000-05-05 | Decibel France Sa | Method of silencing fluid flows in pipes involves using diffuser with perforated and non-perforated sections along its length |
| US6799657B2 (en) * | 2002-10-02 | 2004-10-05 | Carrier Corporation | Absorptive/reactive muffler for variable speed compressors |
| FR2857431A1 (en) * | 2003-07-09 | 2005-01-14 | Dbvib Insonorisation | Sound suppressor for use in pressurized gas outlet, has diffuser that is provided with longitudinal tubular wall situated remotely from annular layer to form annular space in which orifices are arranged |
| GB2405666A (en) * | 2003-09-05 | 2005-03-09 | Dunlop Aerospace Ltd | Noise attenuator, eg for turbofan engine air bleed system |
| US20060124385A1 (en) * | 2004-12-10 | 2006-06-15 | Ingersoll-Rand Company | Modular pressure pulsation dampener |
| RU2280172C1 (en) * | 2005-02-28 | 2006-07-20 | Олег Савельевич Кочетов | Multisection exhaust silencer |
| RU2313673C1 (en) * | 2006-09-15 | 2007-12-27 | Олег Савельевич Кочетов | Multisection noise silencer |
| US8240427B2 (en) * | 2008-10-01 | 2012-08-14 | General Electric Company | Sound attenuation systems and methods |
| RU2394162C1 (en) * | 2009-01-16 | 2010-07-10 | Олег Савельевич Кочетов | Single sound-absorber for noise suppressor |
| RU2392501C1 (en) * | 2009-01-16 | 2010-06-20 | Олег Савельевич Кочетов | Single sound absorber by kochetov |
| DE102009029875A1 (en) * | 2009-06-22 | 2010-12-30 | Airbus Operations Gmbh | Flow restrictor and use of a flow restrictor in an air distribution system of an air conditioning system of an aircraft |
| US8708779B2 (en) * | 2011-02-04 | 2014-04-29 | Phuong Taylor Nguyen | Air blast blowdown silencer system for blast pot |
| JP6071664B2 (en) * | 2012-03-14 | 2017-02-01 | 三菱重工業株式会社 | Exhaust flue |
| US8550208B1 (en) * | 2012-04-23 | 2013-10-08 | General Electric Company | High pressure muffling devices |
| RU2661423C2 (en) * | 2014-02-12 | 2018-07-16 | Олег Савельевич Кочетов | Single piece sound absorber for the compressor stations noise silencers |
| RU2646995C2 (en) * | 2015-07-27 | 2018-03-13 | Олег Савельевич Кочетов | Kochetov's single sound absorber |
| RU2632562C1 (en) * | 2017-01-13 | 2017-10-05 | Олег Савельевич Кочетов | Sound absorber |
| CN107476864A (en) * | 2017-09-28 | 2017-12-15 | 徐州瑞田工程机械有限公司 | A kind of silencer of replaceable air inlet |
| RU2662021C1 (en) * | 2017-10-03 | 2018-07-23 | Олег Савельевич Кочетов | Noise suppressor |
| RU2654772C1 (en) * | 2017-10-03 | 2018-05-22 | Олег Савельевич Кочетов | Sound absorber |
| RU201874U1 (en) * | 2020-04-13 | 2021-01-19 | Федеральное государственное бюджетное образовательное учреждение высшего образования "Дальневосточный государственный университет путей сообщения" (ДВГУПС) | NOISE SUPPRESSOR |
| CN112196672A (en) * | 2020-10-28 | 2021-01-08 | 南昌航空大学 | A kind of micro-miniature turbojet engine muffler and its design method |
| CN112761816A (en) * | 2021-01-25 | 2021-05-07 | 南昌航空大学 | Miniature aero-engine silencer |
| CN114592944B (en) * | 2021-12-29 | 2023-04-11 | 江苏徐海环境监测有限公司 | Noise treatment equipment and use method thereof |
Family Cites Families (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US759964A (en) * | 1903-09-19 | 1904-05-17 | James Bonar | Steam exhaust-head or muffler. |
| US992839A (en) * | 1910-11-19 | 1911-05-23 | Hartley C Wolle | Blast-stove apparatus. |
| FR499519A (en) * | 1918-07-24 | 1920-02-13 | Cesare Parolini | New mufflers for aircraft engines, automobiles, etc. |
| FR514944A (en) * | 1920-05-05 | 1921-03-22 | Cesare Parolini | Silencers for explosion engines |
| US2640557A (en) * | 1950-12-13 | 1953-06-02 | Fuller Co | Retroverted passage type muffler with outer conduit formed of sound absorbing material |
| US2764250A (en) * | 1953-01-23 | 1956-09-25 | Jeffords Joseph | Silencer for pneumatic devices |
| US3196977A (en) * | 1960-04-27 | 1965-07-27 | Industrial Acoustics Co | Sound attenuation control means including diffuser for high velocity streams |
| CH391384A (en) * | 1961-04-14 | 1965-04-30 | Vaucher Roger | Use of heat curable resin |
-
1974
- 1974-08-20 US US498984A patent/US3894610A/en not_active Expired - Lifetime
-
1975
- 1975-03-18 ES ES435717A patent/ES435717A1/en not_active Expired
- 1975-03-18 GB GB1126675A patent/GB1466512A/en not_active Expired
- 1975-03-18 CA CA222,353A patent/CA1026239A/en not_active Expired
- 1975-04-17 FR FR7512033A patent/FR2282533A1/en active Granted
- 1975-06-03 NO NO751949A patent/NO751949L/no unknown
- 1975-06-03 DK DK247275AA patent/DK140181B/en unknown
- 1975-06-19 SE SE7507131A patent/SE7507131L/en unknown
- 1975-06-24 JP JP50077067A patent/JPS51128501A/en active Pending
- 1975-08-02 DE DE2534556A patent/DE2534556B2/en not_active Withdrawn
Also Published As
| Publication number | Publication date |
|---|---|
| CA1026239A (en) | 1978-02-14 |
| GB1466512A (en) | 1977-03-09 |
| DK140181C (en) | 1979-11-26 |
| FR2282533A1 (en) | 1976-03-19 |
| FR2282533B1 (en) | 1979-07-27 |
| ES435717A1 (en) | 1976-12-16 |
| SE7507131L (en) | 1976-02-23 |
| DK247275A (en) | 1976-02-21 |
| DK140181B (en) | 1979-07-02 |
| DE2534556B2 (en) | 1979-02-01 |
| US3894610A (en) | 1975-07-15 |
| JPS51128501A (en) | 1976-11-09 |
| DE2534556A1 (en) | 1976-03-04 |
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