US1148720A - Two-cycles engine. - Google Patents

Two-cycles engine. Download PDF

Info

Publication number
US1148720A
US1148720A US83774814A US1914837748A US1148720A US 1148720 A US1148720 A US 1148720A US 83774814 A US83774814 A US 83774814A US 1914837748 A US1914837748 A US 1914837748A US 1148720 A US1148720 A US 1148720A
Authority
US
United States
Prior art keywords
piston
ports
cylinder
intake
engine
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
US83774814A
Inventor
Frederick W Schultz
Franklin B Lawson
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 US83774814A priority Critical patent/US1148720A/en
Application granted granted Critical
Publication of US1148720A publication Critical patent/US1148720A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B75/00Other engines
    • F02B75/02Engines characterised by their cycles, e.g. six-stroke
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B75/00Other engines
    • F02B75/02Engines characterised by their cycles, e.g. six-stroke
    • F02B2075/022Engines characterised by their cycles, e.g. six-stroke having less than six strokes per cycle
    • F02B2075/025Engines characterised by their cycles, e.g. six-stroke having less than six strokes per cycle two

Definitions

  • LAWSON citizens of the United States, residing at San Fran.-
  • the object of the present invention is to provide an improved form of two-cycle in-.
  • ternal combustion engine which will have high eflicincy, and no complications due to valve trouble, and be light in proportion to its power.
  • Figure 1 is a vertical section of the cylinder of our improved engine
  • Fig. 2 is a horizontal section thereof on the line 22 of Fig. 1.
  • 1 indicates a pipe, leading from a carbureter or any other 4 device for producing a gas mixture, to the inlet of a turbine-blower 2 of a sufiicicnt number of Stages to obtain the necessary pressurefor any rotary blower. or other device of sufficient capacityv and pressure, a
  • a deflector 11 which extends opposite, or in proximity to, the intake ports, and rises above the edge of the hollow piston as well-as extends'below said edge, the portion within the piston being spaced therefrom-substantially the same distance as the outer poitionis spaced from the cylinder, so-tha't gases injected through the intake ports are deflected substantially equally both inward and out- Ward;
  • the cylinder head 12 is formed to receive-the piston and the deflector.
  • any suitable means 'of preventing back firing in the case of imperfect mixture may be placed in the chamber 4, which also serves as a. reservoir for a charge of gas when the ⁇ Torts 5 are covered by the piston 7 "In operation, when the intake and exhaust ports are opened by the downward movement of the piston, the waste gases in the center-of thecylinder, which are opposite said exhaust ports, are the first to flow out therefrom. The other waste gases, in the ends of the cylinder, flow toward the center, and their place is taken at both endsof the cylinder by the incoming fuel mixture.
  • Thls principle of construction is adaptable to either single or double acting internal combustion engines using gas or any low face being concave, and a deflectorcarried" thereby the' edge of which nearer to the piston is spaced from the piston to permit the fuel mixture to pass into said concavity.
  • a cylinder hav.-' ing intake and exhaust ports, apiston ar ranged to close said ports, and a. deflector carried thereby the edgeof whichnearer to curved away from the intake may thepiston is spaced from the-piston andiis.

Description

F. W. SCHULTZ & F. B. LAWSON.-
TWO-CYCLE ENGINE.
APPLICATION FILED MAY II IN VEN TORS Frederak W. Saudi} Franklin 3. Lawson A TTOR NE Y "II" A jaw; 74.. way w.
n a n n I I i. ,f MK, y \F7 In m/ //1 K... 1 I I. 1 II; III. I MWMWMI T. n, a, I \\\\\N\\\\\ WITNESSES FREDERICK W. SCHULTZ AND FRANKLIN B. LAWSON, 0F FRANCISCO} CALIFORNIA.
TWO-CYCLE ENGINE.
masteol Specification of Letters Patent.
Patented Aug. 3, 1915..
Application filed my 11, 1914 Serial No. 837,748.
To all whom it may concern: I
Be it known that We, FREDERICK W.
SCHULTZ and FRANKLIN B. LAWSON, citizens of the United States, residing at San Fran.-
cisco, county of San Francisco, and State of California, have invented new and useful Improvements in Two-Cycle Engines, 0 which the following is a specification. w i,
The object of the present invention is to provide an improved form of two-cycle in-.
ternal combustion engine, which will have high eflicincy, and no complications due to valve trouble, and be light in proportion to its power.
In the accompanying drawing, Figure 1 is a vertical section of the cylinder of our improved engine; Fig. 2 is a horizontal section thereof on the line 22 of Fig. 1.
Referring to the drawing, 1 indicates a pipe, leading from a carbureter or any other 4 device for producing a gas mixture, to the inlet of a turbine-blower 2 of a sufiicicnt number of Stages to obtain the necessary pressurefor any rotary blower. or other device of sufficient capacityv and pressure, a
pipe 3 leading from the outlet ofsaid blower to a chamber 4 around the intake ports 5 of a cylinder 6. In said cylinder can reciprocate apiston 7, whichxinits reciprocation opens and closes both-said ports 5 and exhaust ports 8 leading into an exhaust chamber 9 connected to an exhaust pipe 10. To said piston is secured, preferably by being formed integral therewith, a deflector 11 which extends opposite, or in proximity to, the intake ports, and rises above the edge of the hollow piston as well-as extends'below said edge, the portion within the piston being spaced therefrom-substantially the same distance as the outer poitionis spaced from the cylinder, so-tha't gases injected through the intake ports are deflected substantially equally both inward and out- Ward; Thus the. deflector is of an approxi mately ogee form, asshown. The cylinder head 12 is formed to receive-the piston and the deflector.
' Any suitable means 'of preventing back firing in the case of imperfect mixture may be placed in the chamber 4, which also serves as a. reservoir for a charge of gas when the {Torts 5 are covered by the piston 7 "In operation, when the intake and exhaust ports are opened by the downward movement of the piston, the waste gases in the center-of thecylinder, which are opposite said exhaust ports, are the first to flow out therefrom. The other waste gases, in the ends of the cylinder, flow toward the center, and their place is taken at both endsof the cylinder by the incoming fuel mixture. By this construction then perfect scavenging is effected in both ends of the cylinder; Thls principle of construction is adaptable to either single or double acting internal combustion engines using gas or any low face being concave, and a deflectorcarried" thereby the' edge of which nearer to the piston is spaced from the piston to permit the fuel mixture to pass into said concavity.
2. In a two-cycle engine, a cylinder hav.-' ing intake and exhaust ports, apiston ar ranged to close said ports, and a. deflector carried thereby the edgeof whichnearer to curved away from the intake may thepiston is spaced from the-piston andiis.
ing intake and exhaust'ports, a hollow pis ton arranged to close said ports, and a deg; fiector carried therebyextendingihto the cavity thereof, and spaced from the edgeof the piston both above and :below said edge to provide outer and inner paths between"? the intake and exhaust ports for the fuel] mixture. 4. In a two-cycle engine, a cylinder having; intake and exhaust ports, a hollow pis ton arranged-t0 close said ports, and a de- In testimony whereof We have hereunto set our hands in the presence of two sub- 1( flectozcarried thereby extending both above scribing witnesses. v
and below the edge of the piston, the part of the deflector within the piston being spaced therefrom as the part without is spaced from the cylinder.
substantially the same distance.
FREDERICK \V. SCHULTZ. v FRANKLIN B. LANSOhh Witnesses FRANCIS M. WVRIGIIT, D. B. RICHARDS.
US83774814A 1914-05-11 1914-05-11 Two-cycles engine. Expired - Lifetime US1148720A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US83774814A US1148720A (en) 1914-05-11 1914-05-11 Two-cycles engine.

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US83774814A US1148720A (en) 1914-05-11 1914-05-11 Two-cycles engine.

Publications (1)

Publication Number Publication Date
US1148720A true US1148720A (en) 1915-08-03

Family

ID=3216802

Family Applications (1)

Application Number Title Priority Date Filing Date
US83774814A Expired - Lifetime US1148720A (en) 1914-05-11 1914-05-11 Two-cycles engine.

Country Status (1)

Country Link
US (1) US1148720A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4174685A (en) * 1978-07-05 1979-11-20 Ab Volvo Penta Two stroke cycle internal combustion engine

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4174685A (en) * 1978-07-05 1979-11-20 Ab Volvo Penta Two stroke cycle internal combustion engine

Similar Documents

Publication Publication Date Title
US4307687A (en) Internal combustion engines
US1148720A (en) Two-cycles engine.
US1664782A (en) Internal-combustion engine
US960797A (en) Engine.
US1523341A (en) Two-stroke engine
US1263820A (en) Internal-combustion engine.
US912751A (en) Explosive-engine.
US1562735A (en) Distribution and control arrangement for two-stroke engines
US1555809A (en) Internal-combustion engine
US1193367A (en) Explosive gas engine
SE531337C2 (en) Fuel-driven breaking machine
US1259391A (en) Two-cycle engine.
US1219512A (en) Internal-combustion engine.
US1798967A (en) Internal-combustion engine
US1344263A (en) Internal-combustion engine
US1423578A (en) Two-cycle internal-combustion engine
US954208A (en) Internal-combustion engine.
US1825545A (en) Internal combustion engine
US1871869A (en) Internal combustion motor
US1432320A (en) Two-stroke-cycle opposed-piston internal-combustion engine
US952483A (en) Explosive-engine.
US1693910A (en) Method of and apparatus for generating thermodynamic energy
US347603A (en) hodg-kinson
US1645797A (en) Internal-combustion engine
US864818A (en) Explosive-engine.