US2116751A - Silencer construction - Google Patents

Silencer construction Download PDF

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Publication number
US2116751A
US2116751A US69100A US6910036A US2116751A US 2116751 A US2116751 A US 2116751A US 69100 A US69100 A US 69100A US 6910036 A US6910036 A US 6910036A US 2116751 A US2116751 A US 2116751A
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United States
Prior art keywords
silencer
tube
chambers
header
chamber
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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.)
Expired - Lifetime
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US69100A
Inventor
Floyd E Deremer
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Individual
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Individual
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Priority to US69100A priority Critical patent/US2116751A/en
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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01NGAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR MACHINES OR ENGINES IN GENERAL; GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR INTERNAL COMBUSTION ENGINES
    • F01N1/00Silencing apparatus characterised by method of silencing
    • F01N1/02Silencing apparatus characterised by method of silencing by using resonance
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01NGAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR MACHINES OR ENGINES IN GENERAL; GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR INTERNAL COMBUSTION ENGINES
    • F01N1/00Silencing apparatus characterised by method of silencing
    • F01N1/08Silencing apparatus characterised by method of silencing by reducing exhaust energy by throttling or whirling
    • F01N1/084Silencing apparatus characterised by method of silencing by reducing exhaust energy by throttling or whirling the gases flowing through the silencer two or more times longitudinally in opposite directions, e.g. using parallel or concentric tubes
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01NGAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR MACHINES OR ENGINES IN GENERAL; GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR INTERNAL COMBUSTION ENGINES
    • F01N2490/00Structure, disposition or shape of gas-chambers
    • F01N2490/15Plurality of resonance or dead chambers
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01NGAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR MACHINES OR ENGINES IN GENERAL; GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR INTERNAL COMBUSTION ENGINES
    • F01N2490/00Structure, disposition or shape of gas-chambers
    • F01N2490/15Plurality of resonance or dead chambers
    • F01N2490/155Plurality of resonance or dead chambers being disposed one after the other in flow direction

Definitions

  • a tube 22 which functions as a tuning tube.
  • first pass tube Il being telescoped within an in- A silencer having a shell, end headers, and a termediate tube I6 which passes through an intransverse header dividing it into two chambers, termediate header I1 dividing the silencer into a tube positioned in said header and communi- 25 chambers I8 and I9, and the rst and third pass cating the chambers through the header, an in- 25 tubes I4 and I5 serving to communicate chamlet tube passing through one of the chambers and bers I9 and I8 respectively with the outside of the header and inletting into the other of the the silencer at the forward and rear ends of the Chambers and 9J!
  • tube serving as a tuning means for low frequency 35
  • a tube 22 which between the chambers, and means providing side communicates the interior of the chamber I9 with chambers for the inlet tube for tuning high frethe interior of the chamber I8. 'Ihe tube 22 not quency waves.

Description

May 10, 1938.
F. E. DEREME SILENCER CONSTRUCTION Filed March 16, 1936 c? INVENTOR. BY MMW Il I ATTORNEY.
Patented May 10, 1938 UNITED STATES PATENT OFFICE SILENCER CONSTRUCTION Floyd E. Deremer, Detroit, Mich.
Application March 16, 1936, Serial No. 69,100
1 Claim. (Cl. 181-54) 'I'his application relates to silencer construcbut also serves to provide the second pass of the tions, silencer and is in the nature of a return tube.
'Ihe principal object of the present invention It will readily be understood that for tuning is to provide a silencer construction which is sat- Purposes the length of the return tube 22, its ex- 5 isfactory of operation and economical of man-` tension to either side of header I1, and the posiufacture. The silencer of this application may tion of the inner head I1 may be varied as desired. be characterized by the fact that it provides a 'Ihe silencer hereof is characterized by the fact retroverted through-passage for the gas, with the that the passage through the tuning tube is part through-passage including a resonator chamber of the main and only passage for the gas and -operatng to tune out low frequency sound waves, sound waves and that neither of the chambers 10 by its having no closed or blind or branch pas- I8 and I9 is a branch chamber or ablind chamber. sages for the gas or for low frequency sound Gases entering the silencer course therethrough waves, and by other novel details of construction continuously, with retroversion or otherwise, with which will better be understood upon reference no branches or dead ends, and the passage from to the appended drawing, whose single figure is one chamber to another is accomplished through 15 an elevational section of the silencer. a tube 22 which functions as a tuning tube.
Referring to the drawing, it will be seen that Now having described a silencer construction, the same shows a silencer comprising an outer reference will be had to the claim which follows casing I0 closed by end headers II and I 2 for a determination of the monopoly sought to be 2o through which pass respectively the first and covered herein. 20
third pass tubes I4 and I5 of the silencer, the I claim:
first pass tube Il being telescoped within an in- A silencer having a shell, end headers, and a termediate tube I6 which passes through an intransverse header dividing it into two chambers, termediate header I1 dividing the silencer into a tube positioned in said header and communi- 25 chambers I8 and I9, and the rst and third pass cating the chambers through the header, an in- 25 tubes I4 and I5 serving to communicate chamlet tube passing through one of the chambers and bers I9 and I8 respectively with the outside of the header and inletting into the other of the the silencer at the forward and rear ends of the Chambers and 9J! Outlet tube passing thrOllgh same, respectivelysuch other chamber and the header and outlet- For high frequency tuning, there are provided ting out of the first mentioned chamber, the two 30 between the perforated iirst pass tube I4 and the chambers and the communicating JSube CODStitutintermediate tube I6, and between header I1 and ing the main and only passage for the gases and the rear end of tube I4, a plurality of diaphragms sound waves of the silencer between the ends of 20 which divide the annular space between tubes the inlet and outlet tubes, the COmmllniCating I4 and I6 into a plurality of side chambers 2 I. tube serving as a tuning means for low frequency 35 For low frequency tuning there is disposed in sound waves as well as a communicating means and passing through header I1 a tube 22 which between the chambers, and means providing side communicates the interior of the chamber I9 with chambers for the inlet tube for tuning high frethe interior of the chamber I8. 'Ihe tube 22 not quency waves.
40 only serves as a means for low frequency tuning, FLOYD E. DEREMER. 40
US69100A 1936-03-16 1936-03-16 Silencer construction Expired - Lifetime US2116751A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US69100A US2116751A (en) 1936-03-16 1936-03-16 Silencer construction

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Application Number Priority Date Filing Date Title
US69100A US2116751A (en) 1936-03-16 1936-03-16 Silencer construction

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US2116751A true US2116751A (en) 1938-05-10

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Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2445045A (en) * 1944-06-26 1948-07-13 Strachan Christopher Sound-trapping muffler construction
US2881337A (en) * 1957-07-01 1959-04-07 Gen Electric Acoustically treated motor
US2949165A (en) * 1954-11-26 1960-08-16 Gen Motors Corp Muffler
US2993559A (en) * 1958-05-19 1961-07-25 Wilhelm S Everett Fluid surge alleviator
US3103256A (en) * 1959-11-09 1963-09-10 Oldberg Mfg Company Silencer or muffler
US3286787A (en) * 1963-08-26 1966-11-22 Garrett Corp Turbine exhaust silencer
US3315761A (en) * 1962-06-13 1967-04-25 Oldberg Mfg Company Muffler with spaced concentric tubular members
US3741336A (en) * 1971-06-10 1973-06-26 Tenneco Inc Expansion type silencer
US5388408A (en) * 1993-10-01 1995-02-14 Lawrence-Keech Inc. Exhaust system for internal combustion engines

Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2445045A (en) * 1944-06-26 1948-07-13 Strachan Christopher Sound-trapping muffler construction
US2949165A (en) * 1954-11-26 1960-08-16 Gen Motors Corp Muffler
US2881337A (en) * 1957-07-01 1959-04-07 Gen Electric Acoustically treated motor
US2993559A (en) * 1958-05-19 1961-07-25 Wilhelm S Everett Fluid surge alleviator
US3103256A (en) * 1959-11-09 1963-09-10 Oldberg Mfg Company Silencer or muffler
US3315761A (en) * 1962-06-13 1967-04-25 Oldberg Mfg Company Muffler with spaced concentric tubular members
US3286787A (en) * 1963-08-26 1966-11-22 Garrett Corp Turbine exhaust silencer
US3741336A (en) * 1971-06-10 1973-06-26 Tenneco Inc Expansion type silencer
US5388408A (en) * 1993-10-01 1995-02-14 Lawrence-Keech Inc. Exhaust system for internal combustion engines

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