US867973A - Muffler for gas-engines. - Google Patents

Muffler for gas-engines. Download PDF

Info

Publication number
US867973A
US867973A US30136206A US1906301362A US867973A US 867973 A US867973 A US 867973A US 30136206 A US30136206 A US 30136206A US 1906301362 A US1906301362 A US 1906301362A US 867973 A US867973 A US 867973A
Authority
US
United States
Prior art keywords
muffler
casing
air
shaft
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
Application number
US30136206A
Inventor
Jacob B Hoover
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.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Priority to US30136206A priority Critical patent/US867973A/en
Application granted granted Critical
Publication of US867973A publication Critical patent/US867973A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • 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
    • F01N1/16Silencing apparatus characterised by method of silencing by using movable parts
    • F01N1/18Silencing apparatus characterised by method of silencing by using movable parts having rotary movement
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10STECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10S55/00Gas separation
    • Y10S55/30Exhaust treatment

Definitions

  • My invention relates to new and useful improvements in mufflers for gas engines.
  • the object of the invention is to provide a muflier more especially designed for air cooled engines, in
  • Another feature resides in rotatable means disposed within the muffler and arranged to be driven by the exhaust from the engine, with the result that a suction is createdrwhich tends to draw the air so that a circulation about the cylinder and the exhaust pipe is had.
  • the object of the invention is to provide a dethe character described that will be-strong, durable and efficient and one in which the several parts will not be liable to get out of working order.
  • Figure 1 is alongitudinal vertical sectional view of my improved mufiier, also showing a portion of th'e'exhaust-pipe, and air conducting tube
  • Fig. 2 is a transverse vertical sectional view taken on the line as x and looking toward the 'exhaust pipe
  • Fig. 3 is a transverse vertical sectional view taken on the line y y of Fig. '1, and looking toward the discharge end of the muffler.
  • the n moral 1 designates the muffler which is preferably cylindrical in shape, being closed at each end by disk plates or heads 2 and 3. -These heads are each formed with circular rows of openings 4 and 5 respectively.
  • the inner head 3 is provided with a screw threaded opening 6 in which'is threaded the end of the exhaust pipe 7 of an explosive engine (not shown).
  • This exhaust p pe is surrounded by a somewhat larger air conducting tube 8; which is secured to the ends of the muffler by any suitable means as screws 9.
  • the openings 5 inthe head 3 are so disposed as to permit the air in the tube 8 to freely pass therethrough to the muffler casing 1.
  • a longitudinal shaft 10 I is disposed.
  • the shaft is provided with a reduced portion 11 and a shoulder 12, which reduced portion passes through an opening 13 in the head 2, while the shoulder 12 abuts the inner side of the same, a suitable bearing known manner.
  • the shaft At its opposite end the shaft is also provided with a shoulder 14 and has suitable bearing in a spider 15 which the shoulder abuts.
  • the spider is secured at its opposite ends to the inner surface of the casing 1 by any suitable means as screws 16 passed through the casing from the outside thereof.
  • any suitable means as screws 16 passed through the casing from the outside thereof By provision of the shoulders end thrust and longitudinal displacement of the shaft is obviated, while at the same time it is permitted to freely revolve.
  • blades or paddles 17 and 18 Secured on the shaft and projecting therefrom within a short distance of the inner surface of the casing are blades or paddles 17 and 18, the said blades being arranged in sets of four each, or any other suitable combination.
  • the blades 18 project from the shaft at points substantially forty-five degrees from the blades 17, the purpose of which will be hereinafter brought out.
  • the reduced end 11 of the shaft is extended a short distance beyond the head 2 and a fly or balance wheel 19 mounted thereon, which assists in the revolution of the paddles by the shaft. It is to be noted that the blades 17 and 18 are disposed at an angle and inclined away from the head 3 through which the exhaust and air are admitted. y
  • the operation of the device is as follows:
  • the exhaust gases from the engine enter the muffler casing 9 and causes the shaft 10 to revolve when said gases strike against the blades 17.
  • Thevrotation of these blades create a suction in the mufller casing which tends to draw the air from the tube 8.
  • This tube is connected to the air-jacket of the engine in the usual and well
  • a circulation of air is accordingly set up in said tube and about the cylinder of the engine.
  • Theair and gases after passing through the casing es- It is obvious that after the shaft is set in motion, the momentum gained by the balance wheel 19, will materially assist in keeping up the revolution of the shaft.

Description

PATENTED OUT. 15, 1907.
J. B. HOOVER.
MUFFLER FOB. GAS ENGINES.
APPLICATION II LED FEB-16, 1906.
INVENTOR WITNESSES ATTORNEYS I vice of UNITED STATES PATENT OFFICE.
JACOB B. HOOVER, OF COLUMBUS, OHIO.
MUFFLER FOR GAS-ENGINES.
Application filed February 16,
Specification of Letters Patent.
Patented Oct. 15, 1907.
1906. Serial No. 301,362.
To all whom it may concern.-
Be it known that I, JACOB B. HoovER, a citizen of the United States, residing at Columbus, in the county of Franklin and State of Ohio, have invented certain new and useful Improvements in Muffiers for Gas-Engines, of which'the following is a specification.
My invention relates to new and useful improvements in mufflers for gas engines.
The object of the invention is to provide a muflier more especially designed for air cooled engines, in
which air is conveyed along the exhaust pipe.
Another feature resides in rotatable means disposed within the muffler and arranged to be driven by the exhaust from the engine, with the result that a suction is createdrwhich tends to draw the air so that a circulation about the cylinder and the exhaust pipe is had.
Finally the object of the invention is to provide a dethe character described that will be-strong, durable and efficient and one in which the several parts will not be liable to get out of working order.
With the above and other objects in view, the invenconstruction and operation, a preferable embodiment of which is described in the specification and illustrated in the accompanying drawings, wherein:
Figure 1 is alongitudinal vertical sectional view of my improved mufiier, also showing a portion of th'e'exhaust-pipe, and air conducting tube, Fig. 2 is a transverse vertical sectional view taken on the line as x and looking toward the 'exhaust pipe, and, Fig. 3 is a transverse vertical sectional view taken on the line y y of Fig. '1, and looking toward the discharge end of the muffler. I v
In the drawings the n moral 1 designates the muffler which is preferably cylindrical in shape, being closed at each end by disk plates or heads 2 and 3. -These heads are each formed with circular rows of openings 4 and 5 respectively. The inner head 3 is provided with a screw threaded opening 6 in which'is threaded the end of the exhaust pipe 7 of an explosive engine (not shown). This exhaust p pe is surrounded by a somewhat larger air conducting tube 8; which is secured to the ends of the muffler by any suitable means as screws 9. The openings 5 inthe head 3 are so disposed as to permit the air in the tube 8 to freely pass therethrough to the muffler casing 1.
Centrally within the casing 1 a longitudinal shaft 10 I is disposed. The shaft is provided with a reduced portion 11 and a shoulder 12, which reduced portion passes through an opening 13 in the head 2, while the shoulder 12 abuts the inner side of the same, a suitable bearing known manner.
cape through the openings 4 in the head 2.
being thus provided. At its opposite end the shaft is also provided with a shoulder 14 and has suitable bearing in a spider 15 which the shoulder abuts. The spider is secured at its opposite ends to the inner surface of the casing 1 by any suitable means as screws 16 passed through the casing from the outside thereof. By provision of the shoulders end thrust and longitudinal displacement of the shaft is obviated, while at the same time it is permitted to freely revolve. Secured on the shaft and projecting therefrom within a short distance of the inner surface of the casing are blades or paddles 17 and 18, the said blades being arranged in sets of four each, or any other suitable combination. However, in the present instance, the blades 18 project from the shaft at points substantially forty-five degrees from the blades 17, the purpose of which will be hereinafter brought out. The reduced end 11 of the shaft is extended a short distance beyond the head 2 and a fly or balance wheel 19 mounted thereon, which assists in the revolution of the paddles by the shaft. It is to be noted that the blades 17 and 18 are disposed at an angle and inclined away from the head 3 through which the exhaust and air are admitted. y
The operation of the device is as follows: The exhaust gases from the engine enter the muffler casing 9 and causes the shaft 10 to revolve when said gases strike against the blades 17. Thevrotation of these blades create a suction in the mufller casing which tends to draw the air from the tube 8. This tube is connected to the air-jacket of the engine in the usual and well A circulation of air is accordingly set up in said tube and about the cylinder of the engine. Theair and gases after passing through the casing es- It is obvious that after the shaft is set in motion, the momentum gained by the balance wheel 19, will materially assist in keeping up the revolution of the shaft. I wish it clearly understood that I use no manual or mechanical power in revolving the shaft 10, but depend solely upon the force of the exhaust gtses as they strike up with an exhaust pipe of an explosive engine ot a mufller casing-into which said exhaust pipe discharges, a an mounted in said casing and adapted tohave movement imparted thereto by the force of said exhaust, an air conduit which is also in communication with said casing,
said cas- I cuiation of air in the air conduit.
10 the exterior of the leasing, an air conduit which surrounds Y the exhaust pipe and which is also in communication with the interior of the casing, and said casing having openings formed in the end thereof opposite the end at which, the
exhaust pipe is connected.
In testimony whereof I afliiz my signature in presenceof 15 two witnesses. JACOB B. HOOVER. Witnesses:
A. L. PHELPS, M. B. SCHLEY.
US30136206A 1906-02-16 1906-02-16 Muffler for gas-engines. Expired - Lifetime US867973A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US30136206A US867973A (en) 1906-02-16 1906-02-16 Muffler for gas-engines.

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US30136206A US867973A (en) 1906-02-16 1906-02-16 Muffler for gas-engines.

Publications (1)

Publication Number Publication Date
US867973A true US867973A (en) 1907-10-15

Family

ID=2936421

Family Applications (1)

Application Number Title Priority Date Filing Date
US30136206A Expired - Lifetime US867973A (en) 1906-02-16 1906-02-16 Muffler for gas-engines.

Country Status (1)

Country Link
US (1) US867973A (en)

Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2710165A (en) * 1947-09-23 1955-06-07 Percy H Thomas Rotary gas or vapor device having series arranged rows of buckets
US2837169A (en) * 1955-02-07 1958-06-03 Howard C Sawyer Combined engine muffler and combustion chamber
US4236598A (en) * 1978-06-06 1980-12-02 Lockheed Corporation Rotating self-cleaning sound absorber for ducts
US4706454A (en) * 1986-01-31 1987-11-17 Johnny M. Smith, Jr. Vehicle anti-pollution exhaust device
US5884666A (en) * 1998-04-14 1999-03-23 Johnson; Nikia Deshawn Exhaust pipe extension
US6810992B1 (en) * 2002-09-19 2004-11-02 Mario Lombardo Sound producing vehicle exhaust system
US20050011697A1 (en) * 2003-07-17 2005-01-20 Arlasky David F. Muffler
US20070012510A1 (en) * 2005-07-18 2007-01-18 Roland Kess Muffler outlet part for a motorcycle muffler
US20220298940A1 (en) * 2019-09-25 2022-09-22 Paolo Fresi Noise abatement system for internal combustion engines

Cited By (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2710165A (en) * 1947-09-23 1955-06-07 Percy H Thomas Rotary gas or vapor device having series arranged rows of buckets
US2837169A (en) * 1955-02-07 1958-06-03 Howard C Sawyer Combined engine muffler and combustion chamber
US4236598A (en) * 1978-06-06 1980-12-02 Lockheed Corporation Rotating self-cleaning sound absorber for ducts
US4706454A (en) * 1986-01-31 1987-11-17 Johnny M. Smith, Jr. Vehicle anti-pollution exhaust device
US5884666A (en) * 1998-04-14 1999-03-23 Johnson; Nikia Deshawn Exhaust pipe extension
US6810992B1 (en) * 2002-09-19 2004-11-02 Mario Lombardo Sound producing vehicle exhaust system
US20050011697A1 (en) * 2003-07-17 2005-01-20 Arlasky David F. Muffler
US7383919B2 (en) * 2003-07-17 2008-06-10 Arlasky Performance Inc. Rotatable propeller driven engine exhaust system
US20070012510A1 (en) * 2005-07-18 2007-01-18 Roland Kess Muffler outlet part for a motorcycle muffler
US7484591B2 (en) * 2005-07-18 2009-02-03 Roland Kess Muffler outlet part for a motorcycle muffler
US20220298940A1 (en) * 2019-09-25 2022-09-22 Paolo Fresi Noise abatement system for internal combustion engines
US11603780B2 (en) * 2019-09-25 2023-03-14 Paolo Fresi Noise abatement system for internal combustion engines

Similar Documents

Publication Publication Date Title
US867973A (en) Muffler for gas-engines.
US999776A (en) Reaction-engine.
US2043788A (en) Rotary steam friction motor
US1144921A (en) Gas-engine.
US1085203A (en) Muffler for internal-combustion motors.
US1286365A (en) Exhaust device for internal-combustion engines.
US2172713A (en) Aeromuffler
US925127A (en) Rotary engine.
US788972A (en) Combined muffler and fly-wheel for engines.
US1109547A (en) Engine-muffler.
US1272485A (en) Muffler.
US1045732A (en) Turbo-displacement engine.
US981770A (en) Muffler for internal-combustion engines.
US734878A (en) Muffler.
US832124A (en) Muffler.
US799062A (en) Compound steam-turbine.
US1318996A (en) Aibplane-engrbte muffler
US1125426A (en) Muffler.
US905371A (en) Rotary engine.
US657590A (en) Rotary engine.
US953778A (en) Muffler.
US2639697A (en) Air-cooled internal-combustion engine with exhaust jet
US771070A (en) Muffler.
US807975A (en) Rotary engine.
US1261993A (en) Combined engine and turbine.