US624062A - Exhaust-nozzle - Google Patents
Exhaust-nozzle Download PDFInfo
- Publication number
- US624062A US624062A US624062DA US624062A US 624062 A US624062 A US 624062A US 624062D A US624062D A US 624062DA US 624062 A US624062 A US 624062A
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- US
- United States
- Prior art keywords
- cone
- exhaust
- shell
- nozzle
- cones
- 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.)
- Expired - Lifetime
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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
- F01N1/08—Silencing apparatus characterised by method of silencing by reducing exhaust energy by throttling or whirling
Definitions
- Our invention has for its object to prevent noisy exhaust of gas-engines; and it consists in certain peculiarities of construction and combination of parts constituting the exhaust-nozzle hereinafter particularly set forth with reference to the accompanying drawing and subsequently claimed.
- A indicates the exhaust-pipe of an ordinary gasengine
- B a cylindrical shell that is open at both ends, the inner one of the latter being in screw-thread connection with said pipe.
- spacin g-bracl ets Z Rigidly secured to spacin g-bracl ets Z), made fast to the inside of shell B, is a cone 0, having its point opposing outlet end of pipe A close to the latter on the same line of center.
- a hollow truncated cone D Inverse to cone 0, at a predetermined distance therefrom, is a hollow truncated cone D, having its edge of greatest diameter provided with ears 0, made fast to the aforesaid shell.
- a short shell A and single pair of cones in the arrangement specified may serve as an exhaust-nozzle for an engine of small capacity; but for higher-capacity engines we propose to indefinitely increase the length of shell and multiply the cones therein. Therefore we have shown another pair of cones O D, succeeding those aforesaid.
- the cone 0 is rigid with spacing-brackets I), made fast to the inside of shell B in position to have the point of the latter cone oppose the outer end of cone D aforesaid close to the latter on the same line of center.
- the cone D is similar to cone D and in the same arrangement with respect to cone C as the cone D is to primary cone 0 of the series, the ears 0, extending from the edge of greatest diameter pertaining to said cone D, being made fast to said shell.
- An exhaust-nozzle for a gas-engine comprising a cylindrical shell open at both ends, cones having their greatest diameter less than the shell-bore within which they are suspended to have their points toward the shell-inlet, and hollow truncated cones having their greatest diameters equal to that of said shell-bore in which they are supported inverse to the former cones alternate therewith.
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- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Non-Portable Lighting Devices Or Systems Thereof (AREA)
- Fluidized-Bed Combustion And Resonant Combustion (AREA)
- Combustion Methods Of Internal-Combustion Engines (AREA)
Description
No. 624,062. Patented May 2, I899.
I W. MATTEWS &. G. ANDRICHT.
EXHAUST NOZZLE.
(Applicnticn filed Nov. 4, 1898.)
(No Model.)
UNITED STATES PATENT OFFICE.
\VILLIAM MATTEXVS AND GEORGE ANDRIOHT, OF MILWAUKEE, \VISOONSIN.
EXHAUST-NOZZLE.
SPECIFICATION forming part of Letters Patent No. 624,062, dated May 2, 1899.
' Application filed November 4, 1898. Serial No. 695,447. (No model.)
To all whom, it may concern:
Be it known that we, WILLIAM MATrEws and GEORGE ANDRIOHT, citizens of the United States, and residents of Milwaukee, in the county of Milwaukee and State of \Visconsin, have invented certain new and useful I1nprovements in Exhaust-Nozzles; and we do hereby declare that the following is a full,
clear, and. exact description thereof.
Our invention has for its object to prevent noisy exhaust of gas-engines; and it consists in certain peculiarities of construction and combination of parts constituting the exhaust-nozzle hereinafter particularly set forth with reference to the accompanying drawing and subsequently claimed.
The drawing. illustrates a lengthwise view of our exhaust-nozzle partly broken away.
Referring by letter to the drawing, A indicates the exhaust-pipe of an ordinary gasengine, and B a cylindrical shell that is open at both ends, the inner one of the latter being in screw-thread connection with said pipe.
Rigidly secured to spacin g-bracl ets Z), made fast to the inside of shell B, is a cone 0, having its point opposing outlet end of pipe A close to the latter on the same line of center. Inverse to cone 0, at a predetermined distance therefrom, is a hollow truncated cone D, having its edge of greatest diameter provided with ears 0, made fast to the aforesaid shell. A short shell A and single pair of cones in the arrangement specified may serve as an exhaust-nozzle for an engine of small capacity; but for higher-capacity engines we propose to indefinitely increase the length of shell and multiply the cones therein. Therefore we have shown another pair of cones O D, succeeding those aforesaid. The cone 0 is rigid with spacing-brackets I), made fast to the inside of shell B in position to have the point of the latter cone oppose the outer end of cone D aforesaid close to the latter on the same line of center. The cone D is similar to cone D and in the same arrangement with respect to cone C as the cone D is to primary cone 0 of the series, the ears 0, extending from the edge of greatest diameter pertaining to said cone D, being made fast to said shell.
It will be seen that the greatest area of cone 0 or O is less than that of the shell-bore in transverse section, but that the greatest area of the truncated cone D or D is equal to said area of the shell-bore.
In practice products of combustion generated in a gas-engine have forcible emission through pipe A into shell B and are diffused by cone C, the air ahead of said products being-gradu ally compressed by convergence of the latter in truncated cone D on the way to exit. The immediate diffusion and succeeding convergence of the forcible products of combustion prevent sudden shock that would otherwise come upon the air to produce the noisy sound commonly experienced in the use of gas-engines, and in order to prevent back pressure of air the diffusion and convergence of said products may be indefinitely multiplied on their way to exit by a succession of cones arranged as herein specified, the force of the aforesaid products being gradually diminished as the exit is approached.
Having thus described our invention, what we claim as new, and desire to secure by Letters Patent, is
An exhaust-nozzle for a gas-engine,the same comprising a cylindrical shell open at both ends, cones having their greatest diameter less than the shell-bore within which they are suspended to have their points toward the shell-inlet, and hollow truncated cones having their greatest diameters equal to that of said shell-bore in which they are supported inverse to the former cones alternate therewith.
In testimony that we claim the foregoing we have hereunto set our hands, at Milwaukee,
in the county of Milwaukee and State of YVisconsin, in the presence of two witnesses.
XVM. MATTEWS. GEORGE ANDRICHT.
\Vitnesses:
N. E. OLIPHANT, H. H. MEIXsEA.
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US624062A true US624062A (en) | 1899-05-02 |
Family
ID=2692666
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US624062D Expired - Lifetime US624062A (en) | Exhaust-nozzle |
Country Status (1)
| Country | Link |
|---|---|
| US (1) | US624062A (en) |
Cited By (21)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2485555A (en) * | 1944-12-15 | 1949-10-25 | Leonard R Bester | Baffle type muffler with plural expansion chambers |
| US2557687A (en) * | 1948-04-27 | 1951-06-19 | Omer J Rainville | Baffle type exhaust silencer |
| US2609886A (en) * | 1948-07-03 | 1952-09-09 | Waterloo Foundry Company | Muffler with concave baffles |
| US2936788A (en) * | 1955-04-26 | 1960-05-17 | Dole Valve Co | Flow control system |
| US4574914A (en) * | 1983-11-03 | 1986-03-11 | Flowmaster, Inc. | Compact, sound-attenuating muffler for high-performance, internal combustion engine |
| US4809812A (en) * | 1983-11-03 | 1989-03-07 | Flowmaster, Inc. | Converging, corridor-based, sound-attenuating muffler and method |
| US5123502A (en) * | 1990-08-30 | 1992-06-23 | Flowmaster, Inc. | Muffler assembly with perforated partition for ignition of accumulated fuel and method |
| US5351481A (en) * | 1992-06-26 | 1994-10-04 | Flowmaster, Inc. | Muffler assembly with balanced chamber and method |
| US5444197A (en) * | 1993-08-09 | 1995-08-22 | Flugger; Ray T. | Muffler with intermediate sound-attenuating partition and method |
| US5936210A (en) * | 1998-01-15 | 1999-08-10 | Maremont Exhaust Products, Inc. | High performance muffler |
| US5962822A (en) * | 1998-06-23 | 1999-10-05 | May; Daniel A. | Muffler/exhaust extractor and method |
| US6050363A (en) * | 1999-03-04 | 2000-04-18 | Tu; Hui-Li | Muffler |
| US6286623B1 (en) * | 2000-07-27 | 2001-09-11 | Silent Exhaust Systems Ltd. | Sound-attenuating muffler for internal combustion engine |
| US6364054B1 (en) | 2000-01-27 | 2002-04-02 | Midas International Corporation | High performance muffler |
| US20030173147A1 (en) * | 2002-03-12 | 2003-09-18 | Leon Mazurets | Tikho |
| US6776257B1 (en) | 2003-05-13 | 2004-08-17 | Silent Exhaust Systems Ltd. | Sound-attenuating muffler having reduced back pressure |
| US20060054384A1 (en) * | 2004-09-16 | 2006-03-16 | Terrance Chen | Automobile muffler with high flow rate |
| US20070045044A1 (en) * | 2005-08-26 | 2007-03-01 | Sullivan John T | Flow-through mufflers with optional thermo-electric, sound cancellation, and tuning capabilities |
| US20070205046A1 (en) * | 2006-02-21 | 2007-09-06 | Elroy Newberry | Muffler for internal combustion engine |
| US20080083582A1 (en) * | 2006-10-06 | 2008-04-10 | Towne Lloyd I | Exhaust system |
| US20090127025A1 (en) * | 2007-11-19 | 2009-05-21 | Grant Robert Rimback | Triangular cross section exhaust muffler |
-
0
- US US624062D patent/US624062A/en not_active Expired - Lifetime
Cited By (26)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2485555A (en) * | 1944-12-15 | 1949-10-25 | Leonard R Bester | Baffle type muffler with plural expansion chambers |
| US2557687A (en) * | 1948-04-27 | 1951-06-19 | Omer J Rainville | Baffle type exhaust silencer |
| US2609886A (en) * | 1948-07-03 | 1952-09-09 | Waterloo Foundry Company | Muffler with concave baffles |
| US2936788A (en) * | 1955-04-26 | 1960-05-17 | Dole Valve Co | Flow control system |
| US4574914A (en) * | 1983-11-03 | 1986-03-11 | Flowmaster, Inc. | Compact, sound-attenuating muffler for high-performance, internal combustion engine |
| US4809812A (en) * | 1983-11-03 | 1989-03-07 | Flowmaster, Inc. | Converging, corridor-based, sound-attenuating muffler and method |
| US5123502A (en) * | 1990-08-30 | 1992-06-23 | Flowmaster, Inc. | Muffler assembly with perforated partition for ignition of accumulated fuel and method |
| US5351481A (en) * | 1992-06-26 | 1994-10-04 | Flowmaster, Inc. | Muffler assembly with balanced chamber and method |
| US5444197A (en) * | 1993-08-09 | 1995-08-22 | Flugger; Ray T. | Muffler with intermediate sound-attenuating partition and method |
| US5936210A (en) * | 1998-01-15 | 1999-08-10 | Maremont Exhaust Products, Inc. | High performance muffler |
| US5962822A (en) * | 1998-06-23 | 1999-10-05 | May; Daniel A. | Muffler/exhaust extractor and method |
| US6050363A (en) * | 1999-03-04 | 2000-04-18 | Tu; Hui-Li | Muffler |
| US6364054B1 (en) | 2000-01-27 | 2002-04-02 | Midas International Corporation | High performance muffler |
| US6286623B1 (en) * | 2000-07-27 | 2001-09-11 | Silent Exhaust Systems Ltd. | Sound-attenuating muffler for internal combustion engine |
| US20030173147A1 (en) * | 2002-03-12 | 2003-09-18 | Leon Mazurets | Tikho |
| US6776257B1 (en) | 2003-05-13 | 2004-08-17 | Silent Exhaust Systems Ltd. | Sound-attenuating muffler having reduced back pressure |
| WO2004101960A2 (en) | 2003-05-13 | 2004-11-25 | Silent Exhaust Systems Ltd. | Sound-attenuating muffler having reduced back pressure |
| US20060054384A1 (en) * | 2004-09-16 | 2006-03-16 | Terrance Chen | Automobile muffler with high flow rate |
| US20070045044A1 (en) * | 2005-08-26 | 2007-03-01 | Sullivan John T | Flow-through mufflers with optional thermo-electric, sound cancellation, and tuning capabilities |
| US7610993B2 (en) | 2005-08-26 | 2009-11-03 | John Timothy Sullivan | Flow-through mufflers with optional thermo-electric, sound cancellation, and tuning capabilities |
| US20070205046A1 (en) * | 2006-02-21 | 2007-09-06 | Elroy Newberry | Muffler for internal combustion engine |
| US7549512B2 (en) * | 2006-02-21 | 2009-06-23 | Elroy Newberry | Muffler for internal combustion engine |
| US20080083582A1 (en) * | 2006-10-06 | 2008-04-10 | Towne Lloyd I | Exhaust system |
| US7631725B2 (en) | 2006-10-06 | 2009-12-15 | Ingersoll Rand Company | Exhaust system |
| US20090127025A1 (en) * | 2007-11-19 | 2009-05-21 | Grant Robert Rimback | Triangular cross section exhaust muffler |
| US7793758B2 (en) * | 2007-11-19 | 2010-09-14 | Grant Robert Rimback | Triangular cross section exhaust muffler |
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