US1680017A - Two-stroke engine of the opposed-piston type - Google Patents

Two-stroke engine of the opposed-piston type Download PDF

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Publication number
US1680017A
US1680017A US147516A US14751626A US1680017A US 1680017 A US1680017 A US 1680017A US 147516 A US147516 A US 147516A US 14751626 A US14751626 A US 14751626A US 1680017 A US1680017 A US 1680017A
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Prior art keywords
opposed
crank
piston type
stroke engine
engine
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Expired - Lifetime
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US147516A
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Fornaca Guido
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Individual
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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01BMACHINES OR ENGINES, IN GENERAL OR OF POSITIVE-DISPLACEMENT TYPE, e.g. STEAM ENGINES
    • F01B7/00Machines or engines with two or more pistons reciprocating within same cylinder or within essentially coaxial cylinders
    • F01B7/02Machines or engines with two or more pistons reciprocating within same cylinder or within essentially coaxial cylinders with oppositely reciprocating pistons
    • F01B7/14Machines or engines with two or more pistons reciprocating within same cylinder or within essentially coaxial cylinders with oppositely reciprocating pistons acting on different main shafts
    • 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
    • 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
    • F02B75/28Engines with two or more pistons reciprocating within same cylinder or within essentially coaxial cylinders

Definitions

  • my invention consists of an engine of this type, characterized in that one end of the engine is provided with a casing in which is journalled the driven or propeller shaft, whereas its other end is pro-' videdwith a superfeed compressor, said casing and said compressor constituting extensions of the cylinder group.
  • the compressor occupies the space between the magneto, oil pump, etc., and the body thereof constitutes a connecting means between the upper and-the lower crank cases of the engine.
  • Fig. 1 is a rear elevation of the engine.
  • Fig. 2 is a side view, partly in section, on the line A-B of Fig. 1.
  • Fig. 3 is a section in the plane represented by the line C-D of Fig. 2.
  • crank case of the engine on which are mounted the cylinders 3 whichare open at their ends and provided with admission openings 4, discharge openings 5 and sockets "6 for the sparking plugs.
  • upper crank case. 1' similar to the crank. case 1.
  • Said crank cases are provided with an extension casing 2. Journalled in bearings in the crank cases, 1, 1' are the two crankshafts'7, 7' to 1 denotes the.
  • crank shafts carry gear wheels 13 in mesh with gear wheels 16 on the vertical shaft 14 of a superfeed compressor 15 of the rotary type, said compressor forming an extension of the cylinder group.
  • the gear wheel 13 of the shaft 7 also operates, through apinion 17 and a reducifig gear 18, the water pump 19 and the oil pump (not shown),
  • the shaft 7 is provided with a pinion 20 I through which it operates the ignition magnetos 21.
  • Pipes 22 convey the compressed air from the compressor casing 15 to the carburettors 23.
  • crank shafts arranged in the crank casings and extending into both chambers so that their,

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Shafts, Cranks, Connecting Bars, And Related Bearings (AREA)

Description

Aug. 7, 1928.
1 380,01 7 G. FORNACA TWO-STROKE ENGINEOF THE OPPOSED PIS-TON TYPE II M Filed NOV. 10, 1926 i Fig.2
Patented Aug. 7, 1928.
' 'GUIIDO nonnaca, or 'rUnr'N, I'rALY.
FFPCE.
TWO-STROKE ENGTNE OF THE OPPOSED-IISTON TYPE.
a lication filed November 10, 1926, Serial No. 147,516, and in Italy November 17, 1925.
This invention relates to that type of two stroke internal combustion engine in which two pistons work in each cylinder, said pis-v tons moving in opposite directions and being connected, by means of connecting rods, to two separate crank shafts; its object is to provide an improved engine of this type,
more especially for aircraft, having its parts compactly arranged.
Accordingly, my invention consists of an engine of this type, characterized in that one end of the engine is provided with a casing in which is journalled the driven or propeller shaft, whereas its other end is pro-' videdwith a superfeed compressor, said casing and said compressor constituting extensions of the cylinder group.
Preferably, the driven .shaft has fixed thereon a toothed wheel in mesh with two pinions secured one on each of the crank shafts.
The compressor occupies the space between the magneto, oil pump, etc., and the body thereof constitutes a connecting means between the upper and-the lower crank cases of the engine. a
One. constructional form of my improved engine is illustrated on the accompanying drawing, V
Fig. 1 is a rear elevation of the engine. Fig. 2 is a side view, partly in section, on the line A-B of Fig. 1.
Fig. 3 is a section in the plane represented by the line C-D of Fig. 2.
Referring to the drawings, lower crank case of the engine on which are mounted the cylinders 3 whichare open at their ends and provided with admission openings 4, discharge openings 5 and sockets "6 for the sparking plugs. Upon the cylinders 3 is secured the upper crank case. 1' similar to the crank. case 1. Said crank cases are provided with an extension casing 2. Journalled in bearings in the crank cases, 1, 1' are the two crankshafts'7, 7' to 1 denotes the.
Y which the opposed pistons 9 in each cylinder 3 are connected through connecting rods 8.
Each crank shaft is provided, at one of its ends, with a pinion 10 in mesh with a reducing gear wheel 11 secured on the driven or propeller shaft 12 that is journalled-in the casing formed by "the extension 2'.
The other ends of the crank shafts carry gear wheels 13 in mesh with gear wheels 16 on the vertical shaft 14 of a superfeed compressor 15 of the rotary type, said compressor forming an extension of the cylinder group. The gear wheel 13 of the shaft 7 also operates, through apinion 17 and a reducifig gear 18, the water pump 19 and the oil pump (not shown),
The shaft 7 is provided with a pinion 20 I through which it operates the ignition magnetos 21.
Pipes 22 convey the compressed air from the compressor casing 15 to the carburettors 23. A
What I claim is:
In aninternal combustion engine with op positely arranged pistons, the combination of two end casings forming chambers, a series of cylinders containing the pistons arranged parallel to and interposed between the end casings, crank casings at both ends of the cylinders extending over and clos;
ing both chambers, crank shafts arranged in the crank casings and extending into both chambers so that their,
chambers, compressor rotors for generating axes lie parallel to those of the cylinders,
bevel gears operatively connecting .both crank shafts with-one of said rotors, adriven shaft journaled in the other chamber parallel to the crank shafts, and reducing gears in the last named chamber operatively con-' necting the driven and crank shaftsy In testimony that I claim the foregoing as my invention I have signed my name.
GUIDO FORNACA.
US147516A 1925-11-17 1926-11-10 Two-stroke engine of the opposed-piston type Expired - Lifetime US1680017A (en)

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IT1680017X 1925-11-17

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Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2501053A (en) * 1948-03-12 1950-03-21 United Aircraft Corp Accessory drive for free-piston units
US2507946A (en) * 1942-02-14 1950-05-16 Sulzer Ag Internal-combustion power plant combining two-shaft opposed-piston engine, air supply compressor, and exhaust-gas turbine
US2527424A (en) * 1944-02-04 1950-10-24 Goetaverken Ab Multiple internal-combustion engines of the opposed piston type with clutches and crankshaft synchronizing devices
US3023743A (en) * 1957-11-12 1962-03-06 Jr George A Schauer Engine construction
US3129700A (en) * 1959-01-19 1964-04-21 David G Peterson Engine accessory case
US20140238360A1 (en) * 2013-02-25 2014-08-28 Achates Power, Inc. Rocking Journal Bearings for Two-Stroke Cycle Engines
US9470136B2 (en) 2014-03-06 2016-10-18 Achates Power, Inc. Piston cooling configurations utilizing lubricating oil from a bearing reservoir in an opposed-piston engine
WO2017062509A1 (en) * 2015-10-05 2017-04-13 Pinnacle Engines, Inc. Inverted piston configurations for internal combustion engines

Cited By (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2507946A (en) * 1942-02-14 1950-05-16 Sulzer Ag Internal-combustion power plant combining two-shaft opposed-piston engine, air supply compressor, and exhaust-gas turbine
US2527424A (en) * 1944-02-04 1950-10-24 Goetaverken Ab Multiple internal-combustion engines of the opposed piston type with clutches and crankshaft synchronizing devices
US2501053A (en) * 1948-03-12 1950-03-21 United Aircraft Corp Accessory drive for free-piston units
US3023743A (en) * 1957-11-12 1962-03-06 Jr George A Schauer Engine construction
US3129700A (en) * 1959-01-19 1964-04-21 David G Peterson Engine accessory case
US20140238360A1 (en) * 2013-02-25 2014-08-28 Achates Power, Inc. Rocking Journal Bearings for Two-Stroke Cycle Engines
US9175725B2 (en) * 2013-02-25 2015-11-03 Achates Power, Inc. Rocking journal bearings for two-stroke cycle engines
US9470136B2 (en) 2014-03-06 2016-10-18 Achates Power, Inc. Piston cooling configurations utilizing lubricating oil from a bearing reservoir in an opposed-piston engine
US10208704B2 (en) 2014-03-06 2019-02-19 Achates Power, Inc. Piston cooling configurations utilizing lubricating oil from a bearing reservoir in an opposed-piston engine
WO2017062509A1 (en) * 2015-10-05 2017-04-13 Pinnacle Engines, Inc. Inverted piston configurations for internal combustion engines

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