US1889946A - Gas engine - Google Patents

Gas engine Download PDF

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Publication number
US1889946A
US1889946A US421041A US42104130A US1889946A US 1889946 A US1889946 A US 1889946A US 421041 A US421041 A US 421041A US 42104130 A US42104130 A US 42104130A US 1889946 A US1889946 A US 1889946A
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Prior art keywords
shafts
shaft
cylinders
gas engine
crank
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Expired - Lifetime
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US421041A
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Leslie E Cadwell
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HEADLESS MULTIPLE MOTOR Corp
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HEADLESS MULTIPLE MOTOR CORP
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Priority to US421041A priority Critical patent/US1889946A/en
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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
    • F02B75/28Engines with two or more pistons reciprocating within same cylinder or within essentially coaxial cylinders

Definitions

  • This invention relates to the art of internal combustion engines and has for its primary objects the provision of means whereby an expansion of gases may take pace between two' oppositely traveling pistons; in the elimination of a cylinder head with its accompanying gasket; the provision for a plurality of power take-off shafts and in the provision of means permitting a drive shaft speed differing from that of the motor crank shaft s eed.
  • FIG. 1 is a front elevation of a motor embodying my invention
  • Fig. 2 a vertical longitudinal section through the motor on the line 22 in Fig. 1;
  • Fig. 3 a vertical transverse section through a cylinder of the motor on the line 3-3 in Fig. 2.
  • a crank shaft 23 is rotatably carried across the undersides of the four cylinders and has rockably attached thereto the connecting rods 24, 25, 26 and 27 which in turn are rockably secured to the respective pistons 16, 18, 20. and 22 all in the usual and well known manner.
  • crank shaft 28 in the same plane with the shaft 23 is rotatably mounted a second crank shaft 28 surrounded by the removable crank case 29.
  • the crank shaft 28 is of the four throw interconnecting it with the respective pistons 15, 17, 19 and 21"
  • the gears 34 j and 35 are fixed on similar ends of the crank shafts 23 and 28.
  • the gears 34 j and 35 are fixed on similar ends of the crank shafts 23 and 28.
  • the gears 34 j and 35 are fixed on similar ends of the crank shafts 23 and 28.
  • the gears 34 j and 35 are fixed on similar ends of the crank shafts 23 and 28, each having the same number of teeth thereon.
  • a stub shaft 36 Midway between the two gears 34 and 35 is rotatably carried a stub shaft 36 on which is fixed a gear 37 in mesh with the gears 34 and 35.
  • the two gears 34 and 35 are meshed with the gear 37 to have the corresponding throws of the shafts 23 and 28 opposing one another as indicated in Figs. 2 and 3 whereby the pis tons in each cylinder will be traveling in opposite directions one in respect to the other upon rotation of the shafts.
  • crank shaft 23 Gear driven from the crank shaft 23 is the usual cam shaft 38 runing at one-half crank shaft speed as is customary in four cycle gas engine practice.
  • the length of each of the respective cylinders is such that when the two pistons within that cylinder have reached their limit of travel toward each other, Fig. 3,
  • a space therebetween serving as a compression and combustion space in communication with a pocket 39. Entrance into this pocket 39 is to behad' from the upper side by removing the plug 40 to permit the insertion of the necessary intake and exhaust valves 41 fitting'over ports in the bottom of the pocket and slidingly pass on down to carry the compression spring 42 therearound as a means of seating the valves after being lifted by the cams on the shaft 38 in the usual manner.
  • a spark plug 43 is screw-threadedly carried by the plug 40 as a means of igniting combustible mixtures within the pocket 39 and communicating space between the vpistons.
  • a water jacket 44 is centrally located about the cylinders as a means of conducting away excessive heat.
  • gears 34 and 35 may be of different diameters as indicated by the dash lines 34 and 35 to permit the use of a smallergear 37 as indicated by the line 37 whereby the stub shaft 36 may be given adifi'erent rate of speed. Power may be taken off from the engine. at either ends ofboth I shafts 23 and 28 or from the shaft 36, makin five points in all available. Since the cran shafts 23 and 28 are interconnected by the livered to the shafts 23 and 28 may be utilized at any one of the five oints.
  • a motor ,block having aplurality of vertically disposed cylinders in pairs each comprising an upperand lower cylinder, :1 iston in each cylinder, transverse crank aha ts common to adjoining cylinders, at the ends of the en and operated by said patent, the len each cylinder being.

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Valve-Gear Or Valve Arrangements (AREA)

Description

Dec. 6, 1932. CADWELL 1,889,946
GAS ENGINE Filed Jan 15. 1930 5 Sheets-Sheet 1 Dec. 6, 1932. D L 1,889,946
GAS ENGINE Filed Jan. 15, 1930 3 Sheets-Sheet 2 flfforne d.
Dec. 6, 1932.
L. E. CADWELL 1,889,946
GAS ENGINE Filed Jan. 15, 1930 3 Sheets-Sheet 5 Patented Dec. 6, 1932 UNITED STATES PATENT OFFICE I LESLIE E. CADWELL, OF INDIANAPOLIS, INDIANA, ASSIGNOR 'lO HEADLESSMULTEPLE MOTOR CORPORATION, OF INDIANAPOLIS, INDIANA, A CORPORATION GAS ENGINE Application filed January 15, 1980. Serial No. 421,041.
This invention relates to the art of internal combustion engines and has for its primary objects the provision of means whereby an expansion of gases may take pace between two' oppositely traveling pistons; in the elimination of a cylinder head with its accompanying gasket; the provision for a plurality of power take-off shafts and in the provision of means permitting a drive shaft speed differing from that of the motor crank shaft s eed.
These and other objects will become apparent in the following description of my invention as illustrated in the accompanying drawings, in which Fig. 1 is a front elevation of a motor embodying my invention;
Fig. 2, a vertical longitudinal section through the motor on the line 22 in Fig. 1; and
Fig. 3, a vertical transverse section through a cylinder of the motor on the line 3-3 in Fig. 2.
Like characters of reference indicate like parts throughout the several views in the drawings.
Referring principally'to Figs. 2 and 3, I form a motor block 10 here shown as having four vertically disposed cylinders 11, 12, 13, and 14 therein. Within each of these cylinders I place a pair of opposing pistons 15, 16, 17, 18, 19, 20, 21 and 22 respectively, all of the usual type carrying expansion packing rings. A crank shaft 23 is rotatably carried across the undersides of the four cylinders and has rockably attached thereto the connecting rods 24, 25, 26 and 27 which in turn are rockably secured to the respective pistons 16, 18, 20. and 22 all in the usual and well known manner.
Above the cylinders, in the same plane with the shaft 23 is rotatably mounted a second crank shaft 28 surrounded by the removable crank case 29.
The crank shaft 28 is of the four throw interconnecting it with the respective pistons 15, 17, 19 and 21" On similar ends of the crank shafts 23 and 28 are fixed the gears 34 j and 35, each having the same number of teeth thereon. Midway between the two gears 34 and 35 is rotatably carried a stub shaft 36 on which is fixed a gear 37 in mesh with the gears 34 and 35.
The two gears 34 and 35 are meshed with the gear 37 to have the corresponding throws of the shafts 23 and 28 opposing one another as indicated in Figs. 2 and 3 whereby the pis tons in each cylinder will be traveling in opposite directions one in respect to the other upon rotation of the shafts.
Gear driven from the crank shaft 23 is the usual cam shaft 38 runing at one-half crank shaft speed as is customary in four cycle gas engine practice. The length of each of the respective cylinders is such that when the two pistons within that cylinder have reached their limit of travel toward each other, Fig. 3,
there is a space therebetween serving as a compression and combustion space in communication with a pocket 39. Entrance into this pocket 39 is to behad' from the upper side by removing the plug 40 to permit the insertion of the necessary intake and exhaust valves 41 fitting'over ports in the bottom of the pocket and slidingly pass on down to carry the compression spring 42 therearound as a means of seating the valves after being lifted by the cams on the shaft 38 in the usual manner. A spark plug 43 is screw-threadedly carried by the plug 40 as a means of igniting combustible mixtures within the pocket 39 and communicating space between the vpistons. A water jacket 44 is centrally located about the cylinders as a means of conducting away excessive heat.
I employ the four cycle principle whereby, upon suitable rotation of the shafts 23 and 28, the pistons 15 and 16 in cylinder 11,
for example, are advancedone toward the e other to compress a charge therebetween following which that charge is ignited .and the pistons forced apart one from-the other to D. revolve the respective crank shafts in the same direction of rotation, the pistons traveling to their extreme outer limits to positions aswould be indicated bypistons 17 and 18 in i le cylinder 12. i 4 1 The remaining third and fourth cyclesof travel of the respective pistons exhaust the products of combustion and draw in a new charge and compress it ready for thenext power stroke. It is to be noted that the construction of the motor block .10 is very simple in that the cylinders 11. 12, 13, 14 are bored directly therethrough and that no-seat is required to be fixed to receive a cylinder head from the valves terminating within their respective extensions, sprin s to normally seat t e valves, a .cam shaft rivingly connected with the adjacent crank shaft, cams on the cam shaft lifting the valves at each revolu- 70 tion of the cam shaft, a water jacket coolin the cylinders, a stub shaft between the cr shafts, gears drivingly connecting the crank shafts and stub shaft, means for taking powerfrom the stub shaft and means for taking 76 power from each end of the crank shafts.
In testimony whereof I aifix my si ature.
LESLIE E. CAD ELL.
with a gasket therebetween. It is also to be 3 noted, Fig. 1, that the gears 34 and 35 may be of different diameters as indicated by the dash lines 34 and 35 to permit the use of a smallergear 37 as indicated by the line 37 whereby the stub shaft 36 may be given adifi'erent rate of speed. Power may be taken off from the engine. at either ends ofboth I shafts 23 and 28 or from the shaft 36, makin five points in all available. Since the cran shafts 23 and 28 are interconnected by the livered to the shafts 23 and 28 may be utilized at any one of the five oints. While I'have here s own and described my invention in the one form as now best known to me, it is obvious that structural deviations may bemade from that form withoutdepant ing from the spirit of the invention, and I therefore, donot desire to be limited to that precise form nor anymore than may be required by the following claim. y I claim:
In. an internal combustion'engine, a motor ,block having aplurality of vertically disposed cylinders in pairs each comprising an upperand lower cylinder, :1 iston in each cylinder, transverse crank aha ts common to adjoining cylinders, at the ends of the en and operated by said patent, the len each cylinder being. such that when t e two pistons within a pair of cylinders reach their I limit of travel toward each other there is a space between the istons, a hqusing laterally of each pair of cy inders defining a ocket in communication with said space, 1n ake and exhaust ports in the bottom of the pocket, valves closing and opening the ports, opentings through the top. of the pocket for the introduction of the valves, plugs screwed 1nto and closingtheo emngs,s ark plugs through 7 the last named p ugs, cran cases in two parts containing the crank shafts and cranks, one
gears 34, 37 and 35, the combined power deto v part being integral with the cylinder walls and the other art removably secured to the fir'stpart, the ower inte al art having an' i 6 extension under the va ve ousing, stems
US421041A 1930-01-15 1930-01-15 Gas engine Expired - Lifetime US1889946A (en)

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Cited By (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2462092A (en) * 1945-01-26 1949-02-22 Gustav R Gehrandt Opposed piston engine
US6039011A (en) * 1997-03-05 2000-03-21 The American University Of Baku Internal combustion engine with opposed pistons
DE19905057A1 (en) * 1999-02-08 2000-08-17 Peter Pelz Internal combustion engine with at least two piston-cylinder units, in which each unit has its own crank drive with output crankshaft
US20080047530A1 (en) * 2006-04-18 2008-02-28 Cleeves James M Internal combustion engine
US20100147269A1 (en) * 2008-11-23 2010-06-17 Cleeves Engines Inc. Internal Combustion Engine With Optimal Bore-To-Stroke Ratio
US20110041799A1 (en) * 2009-08-20 2011-02-24 Cleeves James M High Swirl Engine
RU2529290C2 (en) * 2013-01-10 2014-09-27 Федеральное Государственное Автономное Образовательное Учреждение Высшего Профессионального Образования "Сибирский Федеральный Университет" (Сфу) Internal combustion engine (versions)
US9175609B2 (en) 2010-10-08 2015-11-03 Pinnacle Engines, Inc. Control of combustion mixtures and variability thereof with engine load
US9206749B2 (en) 2009-06-04 2015-12-08 Pinnacle Engines, Inc. Variable compression ratio systems for opposed-piston and other internal combustion engines, and related methods of manufacture and use
US9316150B2 (en) 2012-07-02 2016-04-19 Pinnacle Engines, Inc. Variable compression ratio diesel engine
US9650951B2 (en) 2010-10-08 2017-05-16 Pinnacle Engines, Inc. Single piston sleeve valve with optional variable compression ratio capability
US11085297B1 (en) * 2016-02-24 2021-08-10 Enginuity Power Systems, Inc Opposed piston engine and elements thereof

Cited By (23)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2462092A (en) * 1945-01-26 1949-02-22 Gustav R Gehrandt Opposed piston engine
US6039011A (en) * 1997-03-05 2000-03-21 The American University Of Baku Internal combustion engine with opposed pistons
DE19905057A1 (en) * 1999-02-08 2000-08-17 Peter Pelz Internal combustion engine with at least two piston-cylinder units, in which each unit has its own crank drive with output crankshaft
DE19905057B4 (en) * 1999-02-08 2006-02-09 Peter Pelz Internal combustion engine
US7921817B2 (en) 2006-04-18 2011-04-12 Cleeves Engines Inc. Internal combustion engine
US20090266329A1 (en) * 2006-04-18 2009-10-29 Cleeves Engines Inc. Internal combustion engine
US20090266339A1 (en) * 2006-04-18 2009-10-29 Cleeves Engines Inc. Internal combustion engine
US7559298B2 (en) 2006-04-18 2009-07-14 Cleeves Engines Inc. Internal combustion engine
US20080047530A1 (en) * 2006-04-18 2008-02-28 Cleeves James M Internal combustion engine
US9745915B2 (en) 2006-04-18 2017-08-29 Pinnacle Engines, Inc Internal combustion engine
US8365697B2 (en) 2006-04-18 2013-02-05 Pinnacle Engines, Inc. Internal combustion engine
US8651086B2 (en) 2006-04-18 2014-02-18 Pinnacle Engines, Inc. Internal combustion engine
US20100147269A1 (en) * 2008-11-23 2010-06-17 Cleeves Engines Inc. Internal Combustion Engine With Optimal Bore-To-Stroke Ratio
US9206749B2 (en) 2009-06-04 2015-12-08 Pinnacle Engines, Inc. Variable compression ratio systems for opposed-piston and other internal combustion engines, and related methods of manufacture and use
US20110041799A1 (en) * 2009-08-20 2011-02-24 Cleeves James M High Swirl Engine
EP2467586A4 (en) * 2009-08-20 2014-10-08 Pinnacle Engines Inc High swirl engine
US9194288B2 (en) 2009-08-20 2015-11-24 Pinnacle Engines, Inc. High swirl engine
EP2467586A2 (en) * 2009-08-20 2012-06-27 Pinnacle Engines, Inc. High swirl engine
US9175609B2 (en) 2010-10-08 2015-11-03 Pinnacle Engines, Inc. Control of combustion mixtures and variability thereof with engine load
US9650951B2 (en) 2010-10-08 2017-05-16 Pinnacle Engines, Inc. Single piston sleeve valve with optional variable compression ratio capability
US9316150B2 (en) 2012-07-02 2016-04-19 Pinnacle Engines, Inc. Variable compression ratio diesel engine
RU2529290C2 (en) * 2013-01-10 2014-09-27 Федеральное Государственное Автономное Образовательное Учреждение Высшего Профессионального Образования "Сибирский Федеральный Университет" (Сфу) Internal combustion engine (versions)
US11085297B1 (en) * 2016-02-24 2021-08-10 Enginuity Power Systems, Inc Opposed piston engine and elements thereof

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