US1718201A - Muffler for rotary gas engines - Google Patents
Muffler for rotary gas engines Download PDFInfo
- Publication number
- US1718201A US1718201A US298742A US29874219A US1718201A US 1718201 A US1718201 A US 1718201A US 298742 A US298742 A US 298742A US 29874219 A US29874219 A US 29874219A US 1718201 A US1718201 A US 1718201A
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- US
- United States
- Prior art keywords
- muffler
- nozzle
- engine
- nozzles
- gas engines
- 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
- F01N13/00—Exhaust or silencing apparatus characterised by constructional features
- F01N13/06—Exhaust or silencing apparatus characterised by constructional features specially adapted for star-arrangement of cylinders, e.g. exhaust manifolds
-
- 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
- F01N1/16—Silencing apparatus characterised by method of silencing by using movable parts
- F01N1/18—Silencing apparatus characterised by method of silencing by using movable parts having rotary movement
Definitions
- This invention relates to improvements in mufflers for internal combustion engines of the rotary cylinder type.
- the principal object of the invention is the provision of means for reducing the noise of the engine exhaust by causing it to discharge into a partial vacuum, formed by the movement of a nozzle or nozzles carried by the rotating portions of the engine, the discharge of the spent gases being from the rear of said nozzle or nozzles.
- Another object of theinvention is the shaping of the nozzles and their arrangement with respect to each other in such. manner that no nozzle shall interfere. with the functioning of any other nozzle.
- a further object is the provision of a muffler so shaped and positioned as to present little resistance to rotation of the engine.
- Figure I is a side elevational view of a double, opposed cylinder, rotary'engine, embodying my invention, parts being broken away and other parts shown in section in order to more clearly illustrate the construction.
- Fig. II is a cross-sectional view, taken on the line II-II, Fig. I.
- Fig. III is a fragmental view partly cross-section on the line IIIIII, Fig. I.
- Fig. IV is a cross-section of one of the exhaust nozzles, the section being taken upon the line IVIV, Fig. I.
- Fig. V is a side elevational view of a rotary engine embodying a different modification of the invention, one of the inufliers being shown in cross-section.
- / Fig. VI is an outside elevation of a fragment of the muffler, the view being taken at right angles to that of Fig. V.
- Fig. VII is a fragmental view partly in cross-section on the line VII-VII, Fig. V.
- Fig. VIII is a fragmental cross-section taken on the line VIIIVIII, Fig. V.
- a yoke-shaped tubular mufiier has its ends bolted to the cylinder so as to bring the extremities of its gas passage 16 into register with the exhaust ports 15.
- the mufiler extends outwardly from the cylinder in the rearward direction, that is, from the side which is behind as the engine rotates. of the muiller chamber is of much larger crossse'ction than the exhaust ports 15, in order .to permit the gases to expand considerably before leaving the mufller.
- That part of the wall of this transverse chamber which is farthest from the engine shaft, or in other words, radially outermost; is thickened and is provided with a series of screw threaded openings to receive the correspondingly threaded shanks of exhaust nozzles 17.
- the nozzles 17 are flattened on their sides in such manner as to produce a stream-line contour, shown in Fig. IV, in which the direction of rotation of the nozzle is indicated by the arrow A.
- an exhaust discharge opening 18, shown in the drawing as a slot extending substantially throughout the entire length of the nozzle.
- the gases are discharged, instead of against a more or less unyielding wall of air as in the case of the usual muflier.
- the discharged gases tend to hold apart the converging walls of air and to push in between them where they have nearly met. Hence there is no impact of the The transverse portion gases against adense wall of air, and therefore l1ttle noise occurs.
- each engine cylinder has two opposed 5 exhaust ports, but they are engaged at right angles to the engine shaft instead of parallel to it, as in the first modification.
- the muffler 20 is roughly crescent-shaped and is attached at its respective ends to both cylinders on the same side of the engine. On its lateral and outer sides are cooling flanges 21 and 22- respectively.
- a baflie plate 23 with a central opening 24 divides the interior of the chamber into'two parts.
- the hollow interiors of the nozzles communicate with'the interior of the muffler, and the nozzles are provided with discharge openings, preferably slots,
- the gas is first given an opportunity to expand in the large interior'of the muflier chamber, after which it is discharged through slots at the rear edges of the nozzles, 40
- a mufiier adapted to be attached to a rotatable engine member, said muflier havlng an elongated portion with walls exposed to the air as-the englne revolves and an ex.-
- haust nozzle mounted in said mufller, said nozzle being adapted to part the air and leave a partial vacuum in its rear, and having a gas exit at the rear whereby the gas enters said partial vacuum.
- a muffler for gases escaping from movable chambers comprising a flattened tube having front and rear edges, the front edge being broader than the rear edge, and the 7 rear edge having a slot formed therein.
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- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Exhaust Silencers (AREA)
Description
June 18, 1929. c. P. BROCKWAY MUFFLER FOR ROTARY GAS ENGINES Filed May 21. 1919 3 Sheets-Sheet l l INVENTOR. v t I Car-lRBrockWay ATTORNEY June 18, 1929. c. P. BROCKWAY 1,71 01 MUFFLER FOR ROTARY GAS ENGINES Filed May 21. 1919 5 sheets-sheet 2 [II Ilm 16 I 17 1a 15 I INVENTOR. Carl PBroclrm ay ATTORNEY June 18, 1929.
c. P. BROCKWAY MUFFLER FOR ROTARY GAS ENGINES 'Filed y 21. 1919 3 Sheets-Sheet ,lllll lll llllllll fi INVENTOR. far! 1? Brockwa BY I m I I I I fllvllllll/l ATTORNEY Patented June 18, 1929.
UNITED: STATES 3,718,201 PATENT: OFFICE.
CARL P. BROCKWAY, OF TOLEDO, OHIO, ASSIGNOR TO INDUSTRIAL RESEARCH COR- PORATION, 0F TOLEDO, OHIO, A CORPORATION OF DELAWARE.
MUFFLER FOR ROTARY GAS ENGINES.
Application filed May 21,
This invention relates to improvements in mufflers for internal combustion engines of the rotary cylinder type.
The principal object of the invention is the provision of means for reducing the noise of the engine exhaust by causing it to discharge into a partial vacuum, formed by the movement of a nozzle or nozzles carried by the rotating portions of the engine, the discharge of the spent gases being from the rear of said nozzle or nozzles.
Another object of theinvention is the shaping of the nozzles and their arrangement with respect to each other in such. manner that no nozzle shall interfere. with the functioning of any other nozzle.
A further object is the provision of a muffler so shaped and positioned as to present little resistance to rotation of the engine.
Other objects, and objects relating to details of construction and economies of manufacture, will appear as I proceed with the description of that embodiment of the inven tion, which for the purposes of the present application, I have illustrated in the accompanying drawings, in which, I
Figure I is a side elevational view of a double, opposed cylinder, rotary'engine, embodying my invention, parts being broken away and other parts shown in section in order to more clearly illustrate the construction. r
Fig. II is a cross-sectional view, taken on the line II-II, Fig. I.
Fig. III is a fragmental view partly cross-section on the line IIIIII, Fig. I.
Fig. IV is a cross-section of one of the exhaust nozzles, the section being taken upon the line IVIV, Fig. I.
Fig. V is a side elevational view of a rotary engine embodying a different modification of the invention, one of the inufliers being shown in cross-section.
/ Fig. VI is an outside elevation of a fragment of the muffler, the view being taken at right angles to that of Fig. V.
Fig. VII is a fragmental view partly in cross-section on the line VII-VII, Fig. V.
Fig. VIII is a fragmental cross-section taken on the line VIIIVIII, Fig. V.
Similar reference characters refer to like parts throughout the views.
In the drawings, the invention is shown applied to a rotary engine having double, op-
posed cylinders 10, identical in construction,
1919. Serial No. 298,742.
vided with a pair of opposed exhaust ports 15,
extending through the cylinder walls in a direction parallel to the engine shaft 12. A yoke-shaped tubular mufiier has its ends bolted to the cylinder so as to bring the extremities of its gas passage 16 into register with the exhaust ports 15. The mufiler extends outwardly from the cylinder in the rearward direction, that is, from the side which is behind as the engine rotates. of the muiller chamber is of much larger crossse'ction than the exhaust ports 15, in order .to permit the gases to expand considerably before leaving the mufller. That part of the wall of this transverse chamber which is farthest from the engine shaft, or in other words, radially outermost; is thickened and is provided with a series of screw threaded openings to receive the correspondingly threaded shanks of exhaust nozzles 17.
The nozzles 17 are flattened on their sides in such manner as to produce a stream-line contour, shown in Fig. IV, in which the direction of rotation of the nozzle is indicated by the arrow A. In the rear side of each nozzle is an exhaust discharge opening 18, shown in the drawing as a slot, extending substantially throughout the entire length of the nozzle. In revolving rapidly the nozzle 17 parts the. air. Due to the rapidity of the motion the separated walls of air do not come together again directly behind the nozzle, and consequently there is always a small space just behind the slot 18 in which a partial vacuum exists. It is into this vacuum that the gases are discharged, instead of against a more or less unyielding wall of air as in the case of the usual muflier. The discharged gases tend to hold apart the converging walls of air and to push in between them where they have nearly met. Hence there is no impact of the The transverse portion gases against adense wall of air, and therefore l1ttle noise occurs.
In the modification of Figs. V to VIII inclusive, each engine cylinder has two opposed 5 exhaust ports, but they are engaged at right angles to the engine shaft instead of parallel to it, as in the first modification. The muffler 20 is roughly crescent-shaped and is attached at its respective ends to both cylinders on the same side of the engine. On its lateral and outer sides are cooling flanges 21 and 22- respectively. A baflie plate 23 with a central opening 24 divides the interior of the chamber into'two parts. Along the outer side of the mufiler, I arrange a series of nozzles 25, which are preferably shaped like saw teeth. The hollow interiors of the nozzles communicate with'the interior of the muffler, and the nozzles are provided with discharge openings, preferably slots,
along their rear edges. Space must be left behind each nozzle for the vacuum which is formed as the nozzle rotates, and in order to accomplish this result I prefer to make 25 the forward edges of the nozzles inclined as shown in the drawing; Although in the drawing the mufiler is shown connected with two exhaust ports, one in each cylinder, and because of its crescent shape it is peculiarly adapted for this purpose, obviously it could be employed, if desired, to receive the exhaust from a single cylinder only, the attachment of the other cylinder being merely for the purpose of stabilizing the structure.
The two modifications'of my invention above described operate in the same manner.
' The gas is first given an opportunity to expand in the large interior'of the muflier chamber, after which it is discharged through slots at the rear edges of the nozzles, 40
move through it, each nozzle leaving a partial vacuum for a space in its rear, behind which the walls of air gradually converge. Into this space the gas discharges and wedges in between the two walls of air, being gradually absorbed by the air on each side as it moves along. In this way, heavy impact of the gas against a'dense wall of air is avoided and a more or less gradual admixture of thetwo is brought about. Consequently the noise of the exhaust is greatly reduced.
Iclaim as my invention:
1. A mufiier adapted to be attached to a rotatable engine member, said muflier havlng an elongated portion with walls exposed to the air as-the englne revolves and an ex.-
haust nozzle mounted in said mufller, said nozzle being adapted to part the air and leave a partial vacuum in its rear, and having a gas exit at the rear whereby the gas enters said partial vacuum.
2. A muffler for gases escaping from movable chambers comprising a flattened tube having front and rear edges, the front edge being broader than the rear edge, and the 7 rear edge having a slot formed therein.
In testimony whereof I afiix my signature.
CARL P. BROCKWAY.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US298742A US1718201A (en) | 1919-05-21 | 1919-05-21 | Muffler for rotary gas engines |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US298742A US1718201A (en) | 1919-05-21 | 1919-05-21 | Muffler for rotary gas engines |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US1718201A true US1718201A (en) | 1929-06-18 |
Family
ID=23151847
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US298742A Expired - Lifetime US1718201A (en) | 1919-05-21 | 1919-05-21 | Muffler for rotary gas engines |
Country Status (1)
| Country | Link |
|---|---|
| US (1) | US1718201A (en) |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2755928A (en) * | 1953-10-09 | 1956-07-24 | Lutes Donald | Coin control mechanism |
| US10344660B1 (en) * | 2016-05-02 | 2019-07-09 | Northwest Uld, Inc. | Aerodynamically conformal muffler |
| WO2020257883A1 (en) * | 2019-06-28 | 2020-12-30 | Orbital Australia Pty Ltd | An improved muffler for small engines |
| US20220055765A1 (en) * | 2020-08-24 | 2022-02-24 | Sonin Hybrid, LLC | Exhaust System For Aerial Vehicle |
| US12441491B2 (en) | 2020-04-17 | 2025-10-14 | Sonin Hybrid, LLC | Powertrain for aerial vehicle |
-
1919
- 1919-05-21 US US298742A patent/US1718201A/en not_active Expired - Lifetime
Cited By (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2755928A (en) * | 1953-10-09 | 1956-07-24 | Lutes Donald | Coin control mechanism |
| US10344660B1 (en) * | 2016-05-02 | 2019-07-09 | Northwest Uld, Inc. | Aerodynamically conformal muffler |
| WO2020257883A1 (en) * | 2019-06-28 | 2020-12-30 | Orbital Australia Pty Ltd | An improved muffler for small engines |
| CN114072572A (en) * | 2019-06-28 | 2022-02-18 | 奥比托澳大利亚有限公司 | Improved muffler for small engine |
| US20220243638A1 (en) * | 2019-06-28 | 2022-08-04 | Orbital Australia Pty Ltd | Improved muffler for small engines |
| US12006855B2 (en) * | 2019-06-28 | 2024-06-11 | Orbital Australia Pty Ltd | Muffler for small engines |
| US12441491B2 (en) | 2020-04-17 | 2025-10-14 | Sonin Hybrid, LLC | Powertrain for aerial vehicle |
| US20220055765A1 (en) * | 2020-08-24 | 2022-02-24 | Sonin Hybrid, LLC | Exhaust System For Aerial Vehicle |
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