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US1701439A - Engine - Google Patents

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Publication number
US1701439A
US1701439A US33533A US3353325A US1701439A US 1701439 A US1701439 A US 1701439A US 33533 A US33533 A US 33533A US 3353325 A US3353325 A US 3353325A US 1701439 A US1701439 A US 1701439A
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United States
Prior art keywords
engine
crank
shafts
cylinder
piston
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Expired - Lifetime
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US33533A
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Charles G Canfield
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Priority to US33533A priority Critical patent/US1701439A/en
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    • 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
    • F02B75/06Engines with means for equalising torque
    • F02B75/065Engines with means for equalising torque with double connecting rods or crankshafts
    • 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
    • Y10T74/18208Crank, pitman, and slide

Definitions

  • This invention relates to engines either of the internal combustion or the fluid pressure type and has for its object the provision of a novel engine embodying plural shafts having drive connection with each other and so arranged and connected with the piston as to give the engine increased power, as compared with ordinary types, on account of the power stroke being of longer duration than the idle or return stroke.
  • An important object is the provision of an engine of this character having a pair of shafts located atopposite sides of the longitudinal axis of the cylinder or cylinders, both shafts being operatively connected with-each piston, the connections being opposed or reversed so that eachshaft will have power applied thereto during the major portion of 1ts revolution the application of power tothe two shafts being alternate so there will be no idleness at any time.
  • Yet another and more specific object is the provision of an engine having a peculiar mode of connection between the pistons and the twopower shaft so that upon two successive power strokes applied to each shaft the shaft thr'oughsuccessively operating pistons will move through substantially two-thirds of a revolution. 7 Y
  • An additional object is the provision of a..-
  • Figure 1 is a vertical cross section taken through an engine constructed in accordance with my invention, and showing the power shaft in one position.
  • Figure 2 is a similar view showing the moving parts in a differentposition
  • Figure 3 is a bottom lan view or section 5 taken on the line 3-3 0 Figure 1.
  • crank case 10 upon which are mounted any desired number of cylinders 11 of any ordi- 56 nary or preferred construction preferably water-jacketed as indicated at 12.
  • Operating sired means may be provided for permitting the exhaust ofsteam or other fluid pressure, in case of thesteam engine, or the outlet of burnt gases in the case of .an'internal combustion engine.
  • crank case 10 Extending longitudinally of the crank case 10 and journaled in suitable bearings 16 are spaced parallel shafts 17 which project beyond both ends of the crank case. At one end these shaftscarry intermeshing gears 18 and suitable fly wheels 19 while at the other end of either one maybe provided any suitable power take-off device, not shown.
  • the shafts 17 are formed with crank portions 20 upon which areengaged connecting rods 21 arranged inpairs as shown and having their other ends pivoted as at 22 within the yokes or U-shaped members 15 carried by the piston rods 14.
  • crank shafts are geared together and both provided with the fly wheels; Obviously it will be clear that power may be applied successively to the intergeared crank shafts through successive power strokes of the pistons providing a substantially two-thirds revolution of eachcrank shaft.
  • a crankcase a cylinder mounted thereon, a piston reciprocating in the cylinder and carrying a piston rod, a pair of parallel crank shafts journalled through the crank case lying in a plane at right angles to the longitudinal axis of the cylinder and disposed at equal distances from the longitudinal median line of the cylinder greater than the cylinder radius, intermeshing gears and fly wheels on said spaced crank shafts, cranks on each of said shafts in line with the cylinder and oppositely disposed, a pair of pitmen pivotally connected in common to the piston rod and having their other ends pivotally connected to said cranks, the points of pivotal connection of the pitmen with the piston rod and cranks being in substantial alinement at the beginning of the power stroke of the piston.
  • crank case a crank case, a plurality of cylinders mounted thereon, a piston recipro-. eating in each cylinder and carrying a piston rod, a pair of parallel crank shafts jour-' 40 nalled through the crank case with their axes lying in a plane at right angles to the longi-' tudinal axis of the cylinder and disposed at equal distances from the longitudinal axis of the cylinder greater than the piston radius, intermeshing gears on the crank shafts for reverse rotation thereof and a fly wheel on each shaft, a pair of cranks on each of said crank shafts in line with each cylinder, the cranks so alined being oppositely disposed.

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  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Shafts, Cranks, Connecting Bars, And Related Bearings (AREA)
  • Transmission Devices (AREA)

Description

Feb. 5, 1929. 1,701,439
C. G. CANFIELD ENGINE Filed May 28, 1925 CfiarlesGfCagfi'ezd/ INVENTOR ATTORN EY Patented: Feb. 1929.
UNITED STATES 1,701,439 PATENT OFFICE.
CHARLES G. CANFIELD, F YALE, OKLAHOMA.
ENGINE.
Application filed May 28, 1925. Serial N0. 33,533.
This invention relates to engines either of the internal combustion or the fluid pressure type and has for its object the provision of a novel engine embodying plural shafts having drive connection with each other and so arranged and connected with the piston as to give the engine increased power, as compared with ordinary types, on account of the power stroke being of longer duration than the idle or return stroke.
An important object is the provision of an engine of this character having a pair of shafts located atopposite sides of the longitudinal axis of the cylinder or cylinders, both shafts being operatively connected with-each piston, the connections being opposed or reversed so that eachshaft will have power applied thereto during the major portion of 1ts revolution the application of power tothe two shafts being alternate so there will be no idleness at any time.
Yet another and more specific object is the provision of an engine having a peculiar mode of connection between the pistons and the twopower shaft so that upon two successive power strokes applied to each shaft the shaft thr'oughsuccessively operating pistons will move through substantially two-thirds of a revolution. 7 Y
An additional object is the provision of a..-
mechanism of this character which will be comparatively simple and inexpensive to manufacture, positive in action, efiicient and durable in service "and a general improvement intheart.
With the above andother objects and advantages in view, the invention consists in the details of construction andthe arrange ment and combination of parts to be herein- Q after more fully described and claimed, and illustrated in the accompanying drawings,
in which: a
Figure 1 is a vertical cross section taken through an engine constructed in accordance with my invention, and showing the power shaft in one position.
Figure 2 -is a similar view showing the moving parts in a differentposition, and Figure 3 is a bottom lan view or section 5 taken on the line 3-3 0 Figure 1. I
Referringmore particularly'to the drawings I have shown the engine as comprising a crank case 10 upon which are mounted any desired number of cylinders 11 of any ordi- 56 nary or preferred construction preferably water-jacketed as indicated at 12. Operating sired means may be provided for permitting the exhaust ofsteam or other fluid pressure, in case of thesteam engine, or the outlet of burnt gases in the case of .an'internal combustion engine. These details are not shown as they'form no part of the present invention and furthermore as they may be varied within such wide limits.
- Extending longitudinally of the crank case 10 and journaled in suitable bearings 16 are spaced parallel shafts 17 which project beyond both ends of the crank case. At one end these shaftscarry intermeshing gears 18 and suitable fly wheels 19 while at the other end of either one maybe provided any suitable power take-off device, not shown. The shafts 17 are formed with crank portions 20 upon which areengaged connecting rods 21 arranged inpairs as shown and having their other ends pivoted as at 22 within the yokes or U-shaped members 15 carried by the piston rods 14.
In the operation, it will be apparent that the pistons are intendd to have only one power stroke, namely the downward stroke, and assuming that the parts are in the positionshown in Figure 1, it'will be seen that b the time successive pistons successively reac 1 their lowermost positions, as shown in 'Figure 2, each crank shaft will have been turned through successive arcs of substantially one hundred and twenty degrees. Since the pis-. tons are arranged to move in alternation and connected with the crank shaft in the manner specified there will be no unevenness in the movement owing to the fact that the crank shafts are geared together and both provided with the fly wheels; Obviously it will be clear that power may be applied successively to the intergeared crank shafts through successive power strokes of the pistons providing a substantially two-thirds revolution of eachcrank shaft. I
'From 'the. foregoing description and a study of the drawings it will be apparent that I have thus provided air-engine of novel design embodying several' characteristics and features of advantage whereby the efficiency will be greatly increased and power and smoothness of operation likewise increased. Owing to the absence of a large number of parts, resulting from the simplicity in the design, it will be seen that there is little to get out of order and that the mechanism should have a long and satisfactory life.
lVhile I have shown and described the preferred embodiment of the invention, it should be understood that I reserve the right to make such changes in the form, construction and arrangement of parts as will not depart from the spirit of the invention or the scope of the subjoined claims.
Having thus described the invention, I claim i 1. In an engine, a crankcase, a cylinder mounted thereon, a piston reciprocating in the cylinder and carrying a piston rod, a pair of parallel crank shafts journalled through the crank case lying in a plane at right angles to the longitudinal axis of the cylinder and disposed at equal distances from the longitudinal median line of the cylinder greater than the cylinder radius, intermeshing gears and fly wheels on said spaced crank shafts, cranks on each of said shafts in line with the cylinder and oppositely disposed, a pair of pitmen pivotally connected in common to the piston rod and having their other ends pivotally connected to said cranks, the points of pivotal connection of the pitmen with the piston rod and cranks being in substantial alinement at the beginning of the power stroke of the piston.
2. In an engine, a crank case, a plurality of cylinders mounted thereon, a piston recipro-. eating in each cylinder and carrying a piston rod, a pair of parallel crank shafts jour-' 40 nalled through the crank case with their axes lying in a plane at right angles to the longi-' tudinal axis of the cylinder and disposed at equal distances from the longitudinal axis of the cylinder greater than the piston radius, intermeshing gears on the crank shafts for reverse rotation thereof and a fly wheel on each shaft, a pair of cranks on each of said crank shafts in line with each cylinder, the cranks so alined being oppositely disposed. a pair of pitmen pivotally connected in common to each piston rod and having their other ends pivotally mounted on the alined oppositelyf disposed vcranks of their cylinders, the relative proportion of crank and pitman length and piston rod travel being such, as will, at the beginning of the power stroke of the piston, position the pivotal points of the pitman connections to their respective piston rods and cranks in substantial alinement with the said right angular plane of the crank shafts axes with the pair of cranks extended oppositely outward from the longitudinal median lines of the cylinders.
Intestimony whereof I afiix my signature.
CHARLES G. CANFIELD.
US33533A 1925-05-28 1925-05-28 Engine Expired - Lifetime US1701439A (en)

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Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2417910A (en) * 1942-06-20 1947-03-25 Robert D Bruegger Internal-combustion engine
US2775899A (en) * 1954-04-26 1957-01-01 Clayton L Vagneur Mechanical movement for reciprocating machines
US2885855A (en) * 1953-11-06 1959-05-12 Philips Corp Hot-gas reciprocating machine of the displacer-piston type
US2963854A (en) * 1958-03-28 1960-12-13 Philips Corp Hot-gas reciprocating engine
US3023629A (en) * 1958-07-26 1962-03-06 Zahnradfabrik Friedrichshafen Booster steering mechanism for motor vehicles
US3521615A (en) * 1968-12-03 1970-07-28 Earl M Trammell Jr Internal combustion engine
US4898041A (en) * 1987-05-04 1990-02-06 Islas John J Drive linkage for reciprocating engine
US5359908A (en) * 1990-12-06 1994-11-01 Rolando Poeta System for reversibly transforming rotary motion into self-guided rectilinear motion
US20120085301A1 (en) * 2010-01-29 2012-04-12 Islas John J Internal Combustion Engine with Exhaust-Phase Power Extraction Serving Cylinder Pair(s)

Cited By (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2417910A (en) * 1942-06-20 1947-03-25 Robert D Bruegger Internal-combustion engine
US2885855A (en) * 1953-11-06 1959-05-12 Philips Corp Hot-gas reciprocating machine of the displacer-piston type
US2775899A (en) * 1954-04-26 1957-01-01 Clayton L Vagneur Mechanical movement for reciprocating machines
US2963854A (en) * 1958-03-28 1960-12-13 Philips Corp Hot-gas reciprocating engine
US3023629A (en) * 1958-07-26 1962-03-06 Zahnradfabrik Friedrichshafen Booster steering mechanism for motor vehicles
US3521615A (en) * 1968-12-03 1970-07-28 Earl M Trammell Jr Internal combustion engine
US4898041A (en) * 1987-05-04 1990-02-06 Islas John J Drive linkage for reciprocating engine
US5359908A (en) * 1990-12-06 1994-11-01 Rolando Poeta System for reversibly transforming rotary motion into self-guided rectilinear motion
US20120085301A1 (en) * 2010-01-29 2012-04-12 Islas John J Internal Combustion Engine with Exhaust-Phase Power Extraction Serving Cylinder Pair(s)
US8381692B2 (en) * 2010-01-29 2013-02-26 John J. Islas Internal combustion engine with exhaust-phase power extraction serving cylinder pair(s)

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