EP0316640A1 - Silencieux à basse fréquence - Google Patents

Silencieux à basse fréquence Download PDF

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Publication number
EP0316640A1
EP0316640A1 EP88117971A EP88117971A EP0316640A1 EP 0316640 A1 EP0316640 A1 EP 0316640A1 EP 88117971 A EP88117971 A EP 88117971A EP 88117971 A EP88117971 A EP 88117971A EP 0316640 A1 EP0316640 A1 EP 0316640A1
Authority
EP
European Patent Office
Prior art keywords
feed pipe
damping
inlet tube
sectional area
medium
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Granted
Application number
EP88117971A
Other languages
German (de)
English (en)
Other versions
EP0316640B1 (fr
Inventor
Jacob Dr. Keller
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
BBC Brown Boveri AG Switzerland
Original Assignee
BBC Brown Boveri AG Switzerland
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by BBC Brown Boveri AG Switzerland filed Critical BBC Brown Boveri AG Switzerland
Publication of EP0316640A1 publication Critical patent/EP0316640A1/fr
Application granted granted Critical
Publication of EP0316640B1 publication Critical patent/EP0316640B1/fr
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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Classifications

    • 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

Definitions

  • the present invention relates to a silencer for damping low-frequency sound waves.
  • the impedance properties of flow feeders play an important role with regard to their acoustic stability properties, particularly with regard to low-frequency acoustic natural vibrations of such components.
  • Sound waves that are emitted into feed divisions should, if possible, not be reflected, or at most only to a small extent. Otherwise, the reflected waves can help to ignite strong resonant vibrations.
  • Effective damping of high-frequency sound waves can usually be achieved with simple technical precautions (e.g. use of a classic silencer: perforated plate over a small closed cavity). The attenuation of low-frequency sound waves, however, is much more difficult.
  • the invention seeks to remedy this.
  • the invention as characterized in the claims, is based on the object of achieving the attenuation of a wide frequency band in the smallest space in a silencer of the type mentioned.
  • the main advantage of the invention can be seen in the fact that waves of this type can also be strongly damped, the wavelength of which is substantially greater than four times the length of the feed pipe between the pipe inlet and the row of holes.
  • the absorption in the object according to the invention is proportional to the amplitude , in the vibration-free case, the damping holes are flowed through.
  • the subject matter according to the invention acts as an absorber for the frequency designed in each case, within an attenuation bandwidth of approximately 1 octave.
  • silencer can be integrated into all possible turbomachines at any time with only minor modifications due to its simple and space-saving shape, also as a retrofit measure.
  • the muffler consists of a supply pipe 1 through which a medium flows 3 and around which it flows 4. After a length L from the pipe inlet, this has a row of damper bores 2 distributed over the circumference, through which part 4 of the supplied pipe Medium flows into the interior of the feed pipe 1 and collides there with the medium 3 flowing through the feed pipe.
  • the medium 5 then leaves the feed pipe 1 and enters a turbomachine, not shown.
  • the medium in question is intended to be a gas, in many cases it will be air.
  • the wall 6 is intended to symbolize that the feed pipe 1 forming the muffler can communicate directly with the combustion chamber 7 of the turbomachine, not shown. Of course, the feed pipe 1 can be placed on a premixing element.
  • the type of combustion chamber determines whether a change in cross-section, for example due to a jump in the borehole, is required at the transition between feed pipe 1 and the premixing element (not shown) together.
  • the feed pipe 1 can be followed directly by a burner, which in turn is connected upstream of the combustion chamber. It is physically noticeable that the feed pipe 1 is only characterized by three geometrical sizes, namely by the cross-sectional area A of the feed pipe 1, by the effective length L of the feed pipe, which extends in the direction of flow from the pipe inlet to the center of the damper bores 2, and by the overall cross section B of all damping holes 2 on the bolt circle.
  • the total cross-sectional area B of all the damping bores 2 remains for the optimal design of the muffler.
  • the number of damping bores 2 distributed over the circumference and their diameter depend on the size of the feed pipe 1. The optimization must take into account that the flow velocity V in the damping bores 2 and the sound velocity c of the medium still play a role as further parameters.
  • the sound power of the sound wave of frequency f scattered back by the damper is expressed as a percentage of the radiated power:
  • FIG. 2 shows a further embodiment variant of the muffler, in which the guidance of the air portion 4 to the damping bores 2 is guided through an annular opening 9, which extends over the entire length of the feed pipe 1.
  • a second pipe 8 is provided concentrically with the feed pipe 1. The distance between the second tube 8 and the feed tube 1 depends on the determined amount of the air portion 4 and also on the desired speed of the flow V through the damping bores 2.
  • Fig. 3 shows a graphical representation, from the ⁇ OPTIMAL and the associated percentage performance of the silencer reflected wave are readable.
  • the abscissa 10 with the term represents the phase, ie the length of the muffler, which represents the ideal length for the value 1 on the abscissa 10.
  • one ordinate 11 plots the power of the wave reflected by the muffler in%, based on the incident wave, ie on the wave which is fanned in the combustion chamber and radiated into the muffler.
  • the other ordinate 12 represents ⁇ OPTIMAL . As already explained above, this value contains the total cross-sectional area B of the damping bores 2 as a weight.
  • Curve 13 describes the falling power in% of the wave reflected by the muffler as a function of an increasing phase ( ).
  • the other curve 14 describes the increasing value of ⁇ OPTIMAL with decreasing phase ( ).
  • the graph clearly shows how the ideal value 1 (ideal length) of the muffler means that the power in% of the wave reflected by the muffler is zero, ie complete absorption would have been achieved in such a case.

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Exhaust Silencers (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
EP88117971A 1987-11-18 1988-10-28 Silencieux à basse fréquence Expired - Lifetime EP0316640B1 (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
CH449487 1987-11-18
CH4494/87 1987-11-18

Publications (2)

Publication Number Publication Date
EP0316640A1 true EP0316640A1 (fr) 1989-05-24
EP0316640B1 EP0316640B1 (fr) 1993-02-10

Family

ID=4277151

Family Applications (1)

Application Number Title Priority Date Filing Date
EP88117971A Expired - Lifetime EP0316640B1 (fr) 1987-11-18 1988-10-28 Silencieux à basse fréquence

Country Status (3)

Country Link
US (1) US4923035A (fr)
EP (1) EP0316640B1 (fr)
DE (1) DE3878408D1 (fr)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE10336738B4 (de) * 2002-08-28 2007-08-23 General Motors Corp., Detroit Schalldämpfer für die Öffnung einer Kurbelgehäuseentlüftung

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP3863588B2 (ja) * 1995-04-29 2006-12-27 株式会社大宇エレクトロニクス 洗濯機用気泡発生器
US20040163886A1 (en) * 2002-02-15 2004-08-26 Sutera Anthony J. Air turbine for combustion engine
US7650965B2 (en) * 2006-06-09 2010-01-26 Emcon Technologies Llc Exhaust system
US9422843B2 (en) * 2013-09-08 2016-08-23 Michael Wayne Barrett Resonance generating muffler
DE102014226266A1 (de) 2014-12-17 2016-06-23 Fraunhofer-Gesellschaft zur Förderung der angewandten Forschung e.V. Dämm- und Filterstoff und seine Verwendung als inertes schallabsorbierendes Material

Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1338520A (en) * 1919-07-03 1920-04-27 George W Moores Muffler
US2838128A (en) * 1955-08-30 1958-06-10 Sr Edward A Kliewer Engine exhaust muffler
GB888853A (en) * 1958-12-30 1962-02-07 Edward Henry Phillips Exhaust silencer
US3361227A (en) * 1963-10-24 1968-01-02 Mekes Oy Mufflers and exhaust systems
DE1264864B (de) * 1960-06-27 1968-03-28 Leistritz Hans Karl Schalldaempfer fuer stroemende Gase
US3888331A (en) * 1974-05-03 1975-06-10 Gen Motors Corp Power tuned wave interference silencer
FR2363696A1 (fr) * 1976-08-31 1978-03-31 Nihon Radiator Co Perfectionnements a un pot d'echappement

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US944646A (en) * 1909-02-18 1909-12-28 Joseph A Xardell Exhaust-muffler.
US1966620A (en) * 1932-11-26 1934-07-17 Fluor Corp Muffler

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1338520A (en) * 1919-07-03 1920-04-27 George W Moores Muffler
US2838128A (en) * 1955-08-30 1958-06-10 Sr Edward A Kliewer Engine exhaust muffler
GB888853A (en) * 1958-12-30 1962-02-07 Edward Henry Phillips Exhaust silencer
DE1264864B (de) * 1960-06-27 1968-03-28 Leistritz Hans Karl Schalldaempfer fuer stroemende Gase
US3361227A (en) * 1963-10-24 1968-01-02 Mekes Oy Mufflers and exhaust systems
US3888331A (en) * 1974-05-03 1975-06-10 Gen Motors Corp Power tuned wave interference silencer
FR2363696A1 (fr) * 1976-08-31 1978-03-31 Nihon Radiator Co Perfectionnements a un pot d'echappement

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE10336738B4 (de) * 2002-08-28 2007-08-23 General Motors Corp., Detroit Schalldämpfer für die Öffnung einer Kurbelgehäuseentlüftung

Also Published As

Publication number Publication date
US4923035A (en) 1990-05-08
EP0316640B1 (fr) 1993-02-10
DE3878408D1 (de) 1993-03-25

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