US1765713A - Internal-combustion engine - Google Patents

Internal-combustion engine Download PDF

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Publication number
US1765713A
US1765713A US404122A US40412229A US1765713A US 1765713 A US1765713 A US 1765713A US 404122 A US404122 A US 404122A US 40412229 A US40412229 A US 40412229A US 1765713 A US1765713 A US 1765713A
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United States
Prior art keywords
cam
rollers
piston
pistons
engine
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Expired - Lifetime
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US404122A
Inventor
Joseph J Boland
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Aeromarine Plane & Motor Co In
Aeromarine Plane & Motor Co Inc
Original Assignee
Aeromarine Plane & Motor Co In
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Application filed by Aeromarine Plane & Motor Co In filed Critical Aeromarine Plane & Motor Co In
Priority to US404122A priority Critical patent/US1765713A/en
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Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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Classifications

    • 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
    • F01B9/00Reciprocating-piston machines or engines characterised by connections between pistons and main shafts, not specific to groups F01B1/00 - F01B7/00
    • F01B9/04Reciprocating-piston machines or engines characterised by connections between pistons and main shafts, not specific to groups F01B1/00 - F01B7/00 with rotary main shaft other than crankshaft
    • F01B9/06Reciprocating-piston machines or engines characterised by connections between pistons and main shafts, not specific to groups F01B1/00 - F01B7/00 with rotary main shaft other than crankshaft the piston motion being transmitted by curved surfaces
    • 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
    • F02B75/16Engines characterised by number of cylinders, e.g. single-cylinder engines
    • F02B75/18Multi-cylinder engines
    • F02B75/22Multi-cylinder engines with cylinders in V, fan, or star arrangement
    • F02B75/222Multi-cylinder engines with cylinders in V, fan, or star arrangement with cylinders in star arrangement
    • 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
    • F01B9/00Reciprocating-piston machines or engines characterised by connections between pistons and main shafts, not specific to groups F01B1/00 - F01B7/00
    • F01B9/04Reciprocating-piston machines or engines characterised by connections between pistons and main shafts, not specific to groups F01B1/00 - F01B7/00 with rotary main shaft other than crankshaft
    • F01B9/06Reciprocating-piston machines or engines characterised by connections between pistons and main shafts, not specific to groups F01B1/00 - F01B7/00 with rotary main shaft other than crankshaft the piston motion being transmitted by curved surfaces
    • F01B2009/061Reciprocating-piston machines or engines characterised by connections between pistons and main shafts, not specific to groups F01B1/00 - F01B7/00 with rotary main shaft other than crankshaft the piston motion being transmitted by curved surfaces by cams
    • F01B2009/068Quadri-lobe cams
    • 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
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T74/00Machine element or mechanism
    • Y10T74/18Mechanical movements
    • Y10T74/18056Rotary to or from reciprocating or oscillating
    • Y10T74/18296Cam and slide

Definitions

  • This invention relates to internal combustion engines having reciprocating pistons and more particularly to that type of engine wherein such reciprocating pistons transmit their thrust to the drive shaft by means of rollers and suitable cams in place of the usual connecting rods and cranks.
  • Figure 1 is a cross section of the resent [invention with portions of the pistons roken away. I t
  • Figure 2 is a longitudinal section taken on the line 22 of Fig. 1.
  • Figure 3 is a diagrammatic view similar to Fig. 1. Y
  • the present preferred embodiment comprises a plurality of conventional air-cooled cylinders 8, 9 3nd 10 arranged radially about a centrally disposed drive shaft 11 said cylinders and drive shaft being suita 1y supported,- respectively on and within the engine cas-.
  • a main driving cam 13 is mounted u on the shaft 11 and secured thereto by a 'ey 14, said cam being provided with a plurality of lobes 15, 16, 17 and 18.
  • each piston 19 is provided with a roller 21 rotatably mounted upon the usual wrist.v in v,
  • rollers 21 being provided with side flanges and adapted to ride-0n the cam 13 ina manner as to rotationally drive the shaft 11 by means of the cam when the timed explosions occur'within the cylinders 8, 9, and 10. It should be noted that one of the rollers 21 is always disposed in a driving position relative to the cam 13.
  • a pair of cam elements 23 and 24 which are identical in peripheral conformation but of a profile somewhat different than the main driving cam 13.
  • a number of double rollers 26, 27, and 28 which straddle the main cam 13 and which are connected to. the rollers 21 by a series of linkages 29 conveniently disposed on either side of the piston rollers but intermediate the ends of the double rollers 26, 27 and 28.
  • rollers 26, 27 and 28 are disposed radially between the cylinders and that they do not at any time tend to operate the drive shaft 11.
  • the function of these rollers is to co-act with the cams 23, 24 in p such a manner as to create a force which when transmitted through the linkages, will constrain the piston rollers to follow the outline of the cam 13 and thus enforce a constant bearing relation therewith during the oper- 0 ation of the engine.
  • a reciprocating piston engine having a drive shaft
  • a reciprocating piston engine having a drive shaft, the com ination of a plurality of cylinders arranged radially about said i drive shaft, pistons adapted to reciprocate in said cylinders, a main driving cam secured to said drive shaft, rollers rotatably mounted in said pistons and drivably engaging said cam, a pair of cam elements mounted on the drive shaft and disposed on either side of the main cam, spaced apart rollers adapted to straddle the main cam, all-of said rollers being disposed circumferentially about said drive shaft; the last said rollers being alternately arranged relative to the piston rollers, and linkages connecting all of said rollers in series.
  • a reciprocatin piston engine havinga drive shaft, the com ination of a plurality of cylinders arranged radially about said drive shaft, pistons in said 0 linders, a main driving cam secured to the rive shaft, rollers rotatably mounted in said istons and drivably engaging said cam,'a urther cam means disposed adjacent the driving cam,
  • rollers disposed intermediate said cylinders and engagin said cam means, and linkages connecting a l of said rollers in series.

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Transmission Devices (AREA)

Description

June 24, 1930. J. J. BOLAND l,765,713
INTElENAL COMBUSTION ENGINE Filed Nov. 1, 1929 s Sheets-Sheet 1 IN VEN TOR.
Jase w J a/a/r W ATTORNEY June 24, 1930. J. J. BOLAND INTERNAL COMBUSTION ENGINE Filed Nov. 1, 1929 5 Sheets-Sheet 2 dos June 24, 1930. J BQLAND 1,765,713 t INTERNAL COMBUSTION ENGINE Filed Nov. 1. 1929 3 Sheets-Sheet 3 INVENTOR.
L/asgafi 4190/4/20 "7 B ATTORNEY Patented June 24, 1930 UNITED STATES-PATENT? OFFICE JOSEPH .J'. ROLAND, OF KEYPOBT, NEW JERSEY, ASSIGN'OR '10 AEROHABIN E PLANE &
MOTOR 00., INC., A CORPORATION OF NEW YORK nvrmman-comnusrron ENGINE Application filed November 1, 1929. Serial No. 404,122.
This invention relates to internal combustion engines having reciprocating pistons and more particularly to that type of engine wherein such reciprocating pistons transmit their thrust to the drive shaft by means of rollers and suitable cams in place of the usual connecting rods and cranks.
It is a requisite with an engine of such construction that these rollers constantly engage the peripheral ortion of the cam under all movements of the pistons audit will be readily understood that any lost motion between the operating parts will not only greatly reduce the efiiciency of the engine as a whole but will also result in a rapid deterioration of the parts with the resultant ifncrease in various noises resulting thererom.
In the'past it has been found extremely diflicult to maintain these piston rollers in constant engagement with the cam particu 'larly at high speeds, and it will be readily appreciated that the condition resulting from such lack of contact is much the same as that resulting from loose connecting rod bearings in the conventional crank-shaft enine.
Another more serious problem that has confronted the designers of this type of engine in the past, was the elimination or reduction of the extremely high side pressures of the pistons against the cylinder walls which are induced by the action of the piston rollers against the cam, particularly during each power stroke.
Accordingly it is an object of the present invention to .provide an improved mechanism having new and novel features in which the construction is such as not to be subject to the usual objections hereinbefore set forth.
In the present disclosure I have illustrated a means whereby side pressuresof the pistons can be substantially eliminated in a multi-cylinder engine by interconnecting the piston rollers together in series with a set of intermediate rollers. which operate in conjunction with a cam means in a manner as to equalize the side pressuresbetween the pistons and to restrain them against any tendency towards lateralmotion.
As 'shown in the drawings, I have provided a pair of cam members mounted on the drive shaft and disposed on either side of the main driving cam. These cams are K formed with a different contour than that of the main cam and are engaged by separate sets of rollers which are linked to the piston rollers. With the additional improvements hereinafter more particularly described it will be seen that two of the objects are attained by the same mechanism, namely that the piston rollers are not only effectively constrained to remain in contact with the co-acting cam periphery, but also that the pistons themselves cannot be subjected to the usual. side pressures so common toa cam enne. Various other objects and advantages of the invention will be in part obvious from an inspection of the accompanying drawings and a c reful consideration of the following particu ar description and claims of one form of the invention as herein disclosed.
In the drawings:
Figure 1 is a cross section of the resent [invention with portions of the pistons roken away. I t
' Figure 2 is a longitudinal section taken on the line 22 of Fig. 1. Figure 3 is a diagrammatic view similar to Fig. 1. Y
With reference to the drawings, the present preferred embodiment comprises a plurality of conventional air-cooled cylinders 8, 9 3nd 10 arranged radially about a centrally disposed drive shaft 11 said cylinders and drive shaft being suita 1y supported,- respectively on and within the engine cas-.
big-12.
A main driving cam 13 is mounted u on the shaft 11 and secured thereto by a 'ey 14, said cam being provided with a plurality of lobes 15, 16, 17 and 18.
'Each piston 19 is provided with a roller 21 rotatably mounted upon the usual wrist.v in v,
22, said rollers being provided with side flanges and adapted to ride-0n the cam 13 ina manner as to rotationally drive the shaft 11 by means of the cam when the timed explosions occur'within the cylinders 8, 9, and 10. It should be noted that one of the rollers 21 is always disposed in a driving position relative to the cam 13.
On either side of the cam 13 there are mounted, also in driving relation with the shaft 11, a pair of cam elements 23 and 24 which are identical in peripheral conformation but of a profile somewhat different than the main driving cam 13. In rolling cont-act with the cams 23, 24 there are mounted a number of double rollers 26, 27, and 28 which straddle the main cam 13 and which are connected to. the rollers 21 by a series of linkages 29 conveniently disposed on either side of the piston rollers but intermediate the ends of the double rollers 26, 27 and 28.
It will be seen from Figs. 1 and 3 that the above mentioned rollers 26, 27 and 28 are disposed radially between the cylinders and that they do not at any time tend to operate the drive shaft 11. The function of these rollers is to co-act with the cams 23, 24 in p such a manner as to create a force which when transmitted through the linkages, will constrain the piston rollers to follow the outline of the cam 13 and thus enforce a constant bearing relation therewith during the oper- 0 ation of the engine.
'Another and equally important function of the mechanism just described, which was hereinbefore referred to, is the one which eliminates the usual side pressure of the pistons such as are common to this type of engine. With reference to the diagram shown in Fig. 3 of the drawings and assuming the engine to be of the two cycle variety, it will be seen that the piston 19 of cylinder 9 is on 40 the firing stroke (rotation of the shaft as indicated by the arrow) while cylinder 10 is in the act of firing and the piston of cylinder 8 being on the compression stroke. It should be noted that with the roller of cylinder 9 transmitting the piston thrust to the cam lobe 17, there is a component force generated due to the position of the roller on the cam, said force tending towards lateral displacement of the piston in the direction indicated 5:0 by the arrow which would ordinarilycause side pressures. With cylinder 8, which is on thecompression stroke, the cam lobe'15 is also imposing two forces upon the piston, namely, an initial side thrust which is transformed into an axial thrust by the resistance of the cylinder walls, but it should again be noted that the side thrust of this piston is in a direction opposed to that of the one of cylinder 9. Also with the arrangement of the intermediate rollers 26 27 and 28 as shown in the drawings, it will be seen that the cam'23 is tending to move the intermediate roller 28 in ,the direction indicated by the arrow thereon which is in a direction op osed to that of the o5 roller 21, and said rollers eing connected by the linkages 29, the forces are acting largely in opposite directions which has a tendency to equalize them. 7 In view of the fact that all of the rollers are connected in series by the linkages, it will be understood that the tendency of any one piston towards side pressures is also resisted by all the other pistons within their cylinders and that the combined restraint is more than sufficient to overcome the tendency of any one piston towards side pressures.
I have cited herein just a few of the forces and counter forces in describing theoperation of the present invention, but it should be understood that there are also present additional forces that have not been touched on. Those not mentioned will however be apparent to those skilled in the art.
There was no intention of depicting any particular type of engine cylinder in the drawings inasmuch as the improved construction herein disclosed is adapted for either two cycle or four cycle operation.
Variations may be resorted to within the scope of the invention and portions of the improvements may be used without the others, whilst not departing from the spirit of the invention.
Having thus described my invention, I
claim 1. In a reciprocating piston engine having a drive shaft, the combination of a plurality of cylinders arranged radially about the drive shaft, pistons ladapted to reciprocate in said cylinders, a main driving cam secured .to the drive shaft and rotationally actuated by the thrust of the pistons, a further'cam means having a peripheral contour dissimilar to that of the main cam, a plurality of elements havin a rolling contact with said cam means, an a series of linkages articulated both to said rollin elements and to said pistons; said linkages a aptedto restrain the dissimilar to that of the main cam, a plurality of elements having rolling contact with said cam means, and a series of linkages articulated both to said rollin elements and to said piston rollers; said lin ages adapted to restrain the pistons against lateral displacement and to maintain all the rolling means respectively in contact with said cam and sald cam means. 1 7
3. In a reciprocating piston engine having a drive shaft, the com ination of a plurality of cylinders arranged radially about said i drive shaft, pistons adapted to reciprocate in said cylinders, a main driving cam secured to said drive shaft, rollers rotatably mounted in said pistons and drivably engaging said cam, a pair of cam elements mounted on the drive shaft and disposed on either side of the main cam, spaced apart rollers adapted to straddle the main cam, all-of said rollers being disposed circumferentially about said drive shaft; the last said rollers being alternately arranged relative to the piston rollers, and linkages connecting all of said rollers in series.
4. In a reciprocatin piston engine havinga drive shaft, the com ination of a plurality of cylinders arranged radially about said drive shaft, pistons in said 0 linders, a main driving cam secured to the rive shaft, rollers rotatably mounted in said istons and drivably engaging said cam,'a urther cam means disposed adjacent the driving cam,
rollers disposed intermediate said cylinders and engagin said cam means, and linkages connecting a l of said rollers in series.
5. An engine according to claim 4 in which the said further cam means has a different peripheral conformation than the .first said main drivin cam.
6. An engine according to claim 4 in which the said further cam means comprises two cam elements disposed on either side of the main driving cam.
Signed at Keyport, in the county of Mon- I mouth, and State of New Jersey, this 31st day of October, 1929.
' JOSEPH J. BOLAND.
US404122A 1929-11-01 1929-11-01 Internal-combustion engine Expired - Lifetime US1765713A (en)

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Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3279261A (en) * 1951-04-10 1966-10-18 Paul A Crafton Random motion generator
US3948230A (en) * 1974-05-17 1976-04-06 Ruapehu Pty. Ltd. Rotary engine provided with first and secondary rotatably mounted rotors
DE3117707A1 (en) * 1980-05-05 1982-01-28 Alfred J. 43623 Toledo Ohio Crocker INTERNAL COMBUSTION ENGINE
US4387672A (en) * 1981-10-08 1983-06-14 Crocker Alfred J Energy transfer apparatus
EP0658688A1 (en) * 1993-12-14 1995-06-21 Karl Urban Machine
WO1995018915A1 (en) * 1994-01-01 1995-07-13 Chen Fei Chang An engine with reciprocating coupling pistons and with one cam for each cylinder group
WO2016124431A1 (en) * 2015-02-04 2016-08-11 Ludger Hellkuhl Engine with a piston guided on a double-cam cam disk

Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3279261A (en) * 1951-04-10 1966-10-18 Paul A Crafton Random motion generator
US3948230A (en) * 1974-05-17 1976-04-06 Ruapehu Pty. Ltd. Rotary engine provided with first and secondary rotatably mounted rotors
DE3117707A1 (en) * 1980-05-05 1982-01-28 Alfred J. 43623 Toledo Ohio Crocker INTERNAL COMBUSTION ENGINE
US4381740A (en) * 1980-05-05 1983-05-03 Crocker Alfred J Reciprocating engine
US4387672A (en) * 1981-10-08 1983-06-14 Crocker Alfred J Energy transfer apparatus
EP0658688A1 (en) * 1993-12-14 1995-06-21 Karl Urban Machine
WO1995018915A1 (en) * 1994-01-01 1995-07-13 Chen Fei Chang An engine with reciprocating coupling pistons and with one cam for each cylinder group
US5836234A (en) * 1994-01-01 1998-11-17 Chen; Feichang Single CAM reciprocating linked piston type engine
WO2016124431A1 (en) * 2015-02-04 2016-08-11 Ludger Hellkuhl Engine with a piston guided on a double-cam cam disk

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