US2229545A - Engine - Google Patents

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US2229545A
US2229545A US253687A US25368739A US2229545A US 2229545 A US2229545 A US 2229545A US 253687 A US253687 A US 253687A US 25368739 A US25368739 A US 25368739A US 2229545 A US2229545 A US 2229545A
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Prior art keywords
groove
crankshaft
piston
pistons
cross head
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Expired - Lifetime
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US253687A
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Harry A Beckstrom
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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
    • F01B9/00Reciprocating-piston machines or engines characterised by connections between pistons and main shafts and not specific to preceding groups
    • F01B9/02Reciprocating-piston machines or engines characterised by connections between pistons and main shafts and not specific to preceding groups with crankshaft
    • F01B9/026Rigid connections between piston and rod; Oscillating pistons
    • 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 and not specific to preceding groups
    • F01B9/02Reciprocating-piston machines or engines characterised by connections between pistons and main shafts and not specific to preceding groups with crankshaft
    • 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
    • F02B75/24Multi-cylinder engines with cylinders arranged oppositely relative to main shaft and of "flat" type
    • F02B75/246Multi-cylinder engines with cylinders arranged oppositely relative to main shaft and of "flat" type with only one crankshaft of the "pancake" type, e.g. pairs of connecting rods attached to common crankshaft bearing
    • 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
    • Y10T74/18248Crank and slide
    • Y10T74/18256Slidable connections [e.g., scotch yoke]

Definitions

  • My invention relates to engines, particularly of the internal combustion type, and has among its objects and advantages the provision of novel means for converting reciprocatory motion of the pistons into rotary motion of the crank shaft.
  • An object of my invention is to provide an engine including reciprocatory'pistons and a crankshaft wherein novel means are provided for operatively connecting the pistons with the crankshaft for rotating the latter.
  • a further object is to provide an engine including opposed pistons xedly related to a cross head guided in a reciprocatory path wherein novel means are employed for operatively connecting the cross head with the crankshaft.
  • the crankshaft is connected with the cross head in such manner that the power of a particular piston delivers a powerful leverage on the crank pin through the medium of the cross head.
  • the construction is such that the stroke or movement of the cross head and pistons is less in a large degree than the diameter of the circle described by the crank pin of the crankshaft.
  • Figure 1 is a view of the cross head showing the manner in. which the pistons are connected therewith with the crankshaft positioned to rer ceive the power to be applied by one piston;
  • Figure 2 is a similar View illustrating the crankshaft rotated forty-five degrees
  • Figure 3 is a view similar to Figure 1 illustrating the piston and cross head assembly rotated ninety degrees about its longitudinal axis;
  • Figure 4 is a sectional view valong the line 4-4 of Figure 2;
  • Figure 5 is a sectional View along the line 5--5 of Figure 2.
  • pistons I0, I2, I4 and I6 each of which is provided with a piston rod I8.
  • Each piston rod I8 is branched at 20 and bored for the reception of bolts 22 threaded into the Iiange 24 of the cross head 26.
  • pistons I0 and I2 are axially aligned with the. pistons I4 and I6, while all the pistons lie in a common plane.
  • Cross head 26 includes a body 28 which may be cast integrally with the flanges 24.
  • Body 28 is in the nature of 50 a relatively thick plate of rectangular conguration arranged at right angles to the plane deiining the alignment o-f the cylinders I0 to I6, inclusive.
  • Flanges 24 are interconnected with the body 28 through the medium of reinforcing Webs 30.
  • Webs 30 terminate short of the two edges 32 of the body 28 to provide ribs 34 which are slidably guided in grooves 36 in the crankcase 35.
  • One face of the body 28 is provided with a generally -elliptically shaped recess 38, the bottom of which is fashioned to provide a similarly shaped groove or race 46.
  • the arm 42 of the crankshaft 44 is provided with a pin 46 which extends into the recess 38 and is provided with a semicircular extension 48 arranged to ride in the groove 40, as illustrated in Figure 1.
  • Pin 46 includes an end 50 which lies adjacent the bottom face 52 of the recess 38.
  • Figures 1 and 2 illustrate the groove 48 as terminating in opposed semi-circular pockets 54 the transverse axes of which intersect the major axis of the groove 4I).
  • Extension 48 fits snugly in ⁇ the groove 40 with its face 56 contacting the wall 56 of the groove and its curved face 66 contacting the wall 62.
  • the crankshaft 44 rotates in the direction of the arrow 64 of Figures 1 and 2.
  • Walls 58 and 62 o-n one side of the elliptical groove 48 are dened by the radiuses 66 having axes positioned slightly to one side of the axis line 68 of the cross head 26 and the piston assembly.
  • the faces 58 and 62 on the other side of the groove are defined by the radiuses 'I0 having axes located on the opposite side of the axis line 68.
  • the major axis 'I2 of the ellipse defined by the groove 46 is arranged at slightly more than ninety degr-ees from the axis line 68 as at 'I4 and 16.
  • Figure 1 illustrates the position of the crankshaft 44 when the piston ⁇ Ill is in the firing positon, at which time the arm 42 is positioned preferably at an angle of about forty-five degrees from the axis line 68.
  • the crankshaft will be rotated in the direction of the arrow 64.
  • the arm 42 With the crankshaft positioned according to Figure 1 in the firing position of the piston I6, the arm 42 is so positioned as toI derive full leverage from the piston, thus employing or utilizing all power from the explosion to turn the crankshaft.
  • Figure 2 illustrates the crankshaft rotated forty-five degrees beyond the position of Figure 1, at which time the curved face of the extension 48 lies inside the curvature of one of the pockets 54.
  • crankshaft Further rotation of the crankshaft brings the extension 48 into the other side of the groove 4G after which it moves therein to the position where one of the pistons on the other end of the cross head delivers power to the extension 48 at the moment the crankshaft has rotated 180 from the position of Figure 1.
  • the engine may embody the four-cycle principle as well as conventional valves and ignition system. Obviously, more or less cylinders may be employed than herein described without departing from the spirit of the invention. My invention eliminates individual connecting rods for the pistons. While I have described the firing position of the crankshaft as being fortyve degrees past center, it will be understood that this angularity may be varied. In any event, the firing position is such as to derive a powerful leverage from the explosion.
  • the curved face 6B of the extension will continue or have a limited thrust action on the wall 62 of that side of the groove until it reaches a position at the other end of the groove corresponding to the position of Figure l.
  • the pockets 54 are of such curvature as to fit closely about the face 6l] of the extension and are of such depth as to permit entrance, rotation and exit in a precise manner.
  • a guide a reciprocatory piston, a crosshead slidably guided by said guide, a fixed connection between said piston and the crosshead, said crosshead being provided with a groove of generally elliptical conguration, with the major axis of said groove intersecting the axis of said piston, a crankshaft having a crank pin operating in said groove to rotate the crankshaft through reciprocatory motion of the crosshead, said crank pin having a relatively wide and flat face arranged to have contacting relation with the two inner walls of said groove and a curved face arranged to have contacting relation with the outer walls of said groove, the outer walls of said groove being materially wider than the inner walls, said curved face having contacting relation with the full width of the outer walls, said groove being provided with a pocket at each end for rotatably receiving the crank pin during transfer of the latter from one side of the groove to the other, said crank pin having a reach circular in cross section adapted to rotate inside said pockets for guiding the crank pin during transfer of its relatively wide and fiat
  • a guide a reciprocatory piston, a crosshead slidably guided by said guide, a fixed connection between said piston and the crosshead, said crosshead being provided with a groove of generally elliptical conguratiomwith the major axis of said groove intersecting the axis of said piston, a crankshaft having a crank pin having an end extension operating in said groove to rotate the crankshaft through reciprocatory motion of the crosshead, said end extension having a rst face arranged to have selective contacting engagement with the two inner walls of said groove and a curved face arranged to have selective contacting engagement with the outer walls of said groove, the outer walls of said groove being materially wider than the inner walls and said groove being provided with a pocket at each end for rotatably receiving the crank pin during transfer of said end extension from one side of the groove to the other.

Description

Ja. 2l, 1941. H, ABECKSTROM v 2,229,545-
ENGINE File'd Jan. so, 1959 sheets-sheet 1 ATTO R N EYS Jan. 21, 1941.
H. A. BECKSTROM ENGINE Filed Jan. so. 19:59
2 Sheets-Sheet 2 INVENTOR ATTCRNEYSv Patented Jan. 21, 1941 UNITED STATES PATENT OFFICE 3 Claims.
My invention relates to engines, particularly of the internal combustion type, and has among its objects and advantages the provision of novel means for converting reciprocatory motion of the pistons into rotary motion of the crank shaft.
An object of my invention is to provide an engine including reciprocatory'pistons and a crankshaft wherein novel means are provided for operatively connecting the pistons with the crankshaft for rotating the latter.
A further object is to provide an engine including opposed pistons xedly related to a cross head guided in a reciprocatory path wherein novel means are employed for operatively connecting the cross head with the crankshaft. The crankshaft is connected with the cross head in such manner that the power of a particular piston delivers a powerful leverage on the crank pin through the medium of the cross head. At the same time, the construction is such that the stroke or movement of the cross head and pistons is less in a large degree than the diameter of the circle described by the crank pin of the crankshaft.
In the accompanying drawings:
Figure 1 is a view of the cross head showing the manner in. which the pistons are connected therewith with the crankshaft positioned to rer ceive the power to be applied by one piston;
Figure 2 is a similar View illustrating the crankshaft rotated forty-five degrees;
Figure 3 is a view similar to Figure 1 illustrating the piston and cross head assembly rotated ninety degrees about its longitudinal axis;
Figure 4 is a sectional view valong the line 4-4 of Figure 2; and
Figure 5 is a sectional View along the line 5--5 of Figure 2.
In the embodiment selected to illustrate my 40 invention, I make use of pistons I0, I2, I4 and I6 each of which is provided with a piston rod I8. Each piston rod I8 is branched at 20 and bored for the reception of bolts 22 threaded into the Iiange 24 of the cross head 26. According to 45 Figure 3, pistons I0 and I2 are axially aligned with the. pistons I4 and I6, while all the pistons lie in a common plane. Cross head 26 includes a body 28 which may be cast integrally with the flanges 24. Body 28 is in the nature of 50 a relatively thick plate of rectangular conguration arranged at right angles to the plane deiining the alignment o-f the cylinders I0 to I6, inclusive. Flanges 24 are interconnected with the body 28 through the medium of reinforcing Webs 30.
Webs 30 terminate short of the two edges 32 of the body 28 to provide ribs 34 which are slidably guided in grooves 36 in the crankcase 35.
One face of the body 28 is provided with a generally -elliptically shaped recess 38, the bottom of which is fashioned to provide a similarly shaped groove or race 46. The arm 42 of the crankshaft 44 is provided with a pin 46 which extends into the recess 38 and is provided with a semicircular extension 48 arranged to ride in the groove 40, as illustrated in Figure 1. Pin 46 includes an end 50 which lies adjacent the bottom face 52 of the recess 38. Figures 1 and 2 illustrate the groove 48 as terminating in opposed semi-circular pockets 54 the transverse axes of which intersect the major axis of the groove 4I).
Extension 48 fits snugly in` the groove 40 with its face 56 contacting the wall 56 of the groove and its curved face 66 contacting the wall 62. In operation, the crankshaft 44 rotates in the direction of the arrow 64 of Figures 1 and 2. Walls 58 and 62 o-n one side of the elliptical groove 48 are dened by the radiuses 66 having axes positioned slightly to one side of the axis line 68 of the cross head 26 and the piston assembly. The faces 58 and 62 on the other side of the groove are defined by the radiuses 'I0 having axes located on the opposite side of the axis line 68. Thus the major axis 'I2 of the ellipse defined by the groove 46 is arranged at slightly more than ninety degr-ees from the axis line 68 as at 'I4 and 16.
Figure 1 illustrates the position of the crankshaft 44 when the piston` Ill is in the firing positon, at which time the arm 42 is positioned preferably at an angle of about forty-five degrees from the axis line 68. As the piston I0 is driven in the direction of the arrow 'I8 the crankshaft will be rotated in the direction of the arrow 64. With the crankshaft positioned according to Figure 1 in the firing position of the piston I6, the arm 42 is so positioned as toI derive full leverage from the piston, thus employing or utilizing all power from the explosion to turn the crankshaft. Figure 2 illustrates the crankshaft rotated forty-five degrees beyond the position of Figure 1, at which time the curved face of the extension 48 lies inside the curvature of one of the pockets 54. Further rotation of the crankshaft brings the extension 48 into the other side of the groove 4G after which it moves therein to the position where one of the pistons on the other end of the cross head delivers power to the extension 48 at the moment the crankshaft has rotated 180 from the position of Figure 1.
The engine may embody the four-cycle principle as well as conventional valves and ignition system. Obviously, more or less cylinders may be employed than herein described without departing from the spirit of the invention. My invention eliminates individual connecting rods for the pistons. While I have described the firing position of the crankshaft as being fortyve degrees past center, it will be understood that this angularity may be varied. In any event, the firing position is such as to derive a powerful leverage from the explosion.
In arranging the firing position considerably beyond the axis line 68, I provide a construction which minimizes lateral thrust on the guides for the cross head. Because of the formation of the groove or race 40, the cross head moves a distance considerably less than the diameter described by the extension 48. In an arrangement such as that illustrated, the travel of the cross head and pistons is less 'by twenty-iive per cent than the diameterof the circle.
As the extension 158 moves beyond the position of Figure 2 and enters the approached end of the groove 40, the curved face 6B of the extension will continue or have a limited thrust action on the wall 62 of that side of the groove until it reaches a position at the other end of the groove corresponding to the position of Figure l. The pockets 54 are of such curvature as to fit closely about the face 6l] of the extension and are of such depth as to permit entrance, rotation and exit in a precise manner.
Without further elaboration, the foregoing will so fully illustrate my invention that others may, by applying current knowledge, readily adapt the same for use under various conditions of service.
I claim:
l. In an engine, a guide, a reciprocatory piston, a crosshead slidably guided by said guide, a xed connection between said piston and the crosshead, said crosshead being provided with a groove of generally elliptical conguration, with the major axis of said groove intersecting the axis of said piston, a crankshaft having a crank pin operating in said groove to rotate the crankshaft through reciprocatory motion of the crosshead, said crank pin having a relatively wide and flat face arranged to have contacting relation with the two inner walls of said groove and a curved face arranged to have contacting relation with the outer walls of said groove, the outer walls of said groove being materially wider than the inner walls, and said curved face having contacting relation with the full width of the outer walls.
2. In an engine, a guide, a reciprocatory piston, a crosshead slidably guided by said guide, a fixed connection between said piston and the crosshead, said crosshead being provided with a groove of generally elliptical conguration, with the major axis of said groove intersecting the axis of said piston, a crankshaft having a crank pin operating in said groove to rotate the crankshaft through reciprocatory motion of the crosshead, said crank pin having a relatively wide and flat face arranged to have contacting relation with the two inner walls of said groove and a curved face arranged to have contacting relation with the outer walls of said groove, the outer walls of said groove being materially wider than the inner walls, said curved face having contacting relation with the full width of the outer walls, said groove being provided with a pocket at each end for rotatably receiving the crank pin during transfer of the latter from one side of the groove to the other, said crank pin having a reach circular in cross section adapted to rotate inside said pockets for guiding the crank pin during transfer of its relatively wide and fiat face from one inner wall to the other inner wall of the groove.
3. In an engine, a guide, a reciprocatory piston, a crosshead slidably guided by said guide, a fixed connection between said piston and the crosshead, said crosshead being provided with a groove of generally elliptical conguratiomwith the major axis of said groove intersecting the axis of said piston, a crankshaft having a crank pin having an end extension operating in said groove to rotate the crankshaft through reciprocatory motion of the crosshead, said end extension having a rst face arranged to have selective contacting engagement with the two inner walls of said groove and a curved face arranged to have selective contacting engagement with the outer walls of said groove, the outer walls of said groove being materially wider than the inner walls and said groove being provided with a pocket at each end for rotatably receiving the crank pin during transfer of said end extension from one side of the groove to the other.
HARRY A. BECKSTROM.
US253687A 1939-01-30 1939-01-30 Engine Expired - Lifetime US2229545A (en)

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Cited By (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2513514A (en) * 1945-10-08 1950-07-04 Robert A Poage Piston and crankshaft connecting means for internal-combustion engines
US2995042A (en) * 1958-03-03 1961-08-08 Thompson Ramo Wooldridge Inc Switch actuator
US3584172A (en) * 1969-04-01 1971-06-08 Kenneth Owen Switch operating mechanism
US3753386A (en) * 1971-03-03 1973-08-21 F Scott Valve actuator
US4409855A (en) * 1982-04-09 1983-10-18 Martin Kokus Motion to rotary motion
US4449494A (en) * 1981-10-29 1984-05-22 Compagnie Du Moteur Energitique C.M.E. Inc. Internal combustion engine
US4791898A (en) * 1986-12-02 1988-12-20 R P & M Engines, Inc. V-engine with yoke
US5879145A (en) * 1995-01-17 1999-03-09 Knorr-Bremse Systems Fur Nutzfahrzeuge Gmbh Integrated cylinder liner and valve plate for a compressor
US20050175480A1 (en) * 2002-05-31 2005-08-11 Xiufeng Gao Yoke mechanism for compressor
US20070047719A1 (en) * 2005-09-01 2007-03-01 Vishal Dhawan Voice application network platform

Cited By (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2513514A (en) * 1945-10-08 1950-07-04 Robert A Poage Piston and crankshaft connecting means for internal-combustion engines
US2995042A (en) * 1958-03-03 1961-08-08 Thompson Ramo Wooldridge Inc Switch actuator
US3584172A (en) * 1969-04-01 1971-06-08 Kenneth Owen Switch operating mechanism
US3753386A (en) * 1971-03-03 1973-08-21 F Scott Valve actuator
US4449494A (en) * 1981-10-29 1984-05-22 Compagnie Du Moteur Energitique C.M.E. Inc. Internal combustion engine
US4409855A (en) * 1982-04-09 1983-10-18 Martin Kokus Motion to rotary motion
US4791898A (en) * 1986-12-02 1988-12-20 R P & M Engines, Inc. V-engine with yoke
US5879145A (en) * 1995-01-17 1999-03-09 Knorr-Bremse Systems Fur Nutzfahrzeuge Gmbh Integrated cylinder liner and valve plate for a compressor
US20050175480A1 (en) * 2002-05-31 2005-08-11 Xiufeng Gao Yoke mechanism for compressor
US7287458B2 (en) * 2002-05-31 2007-10-30 Lg Electronics Inc. Yoke mechanism for compressor
US20070047719A1 (en) * 2005-09-01 2007-03-01 Vishal Dhawan Voice application network platform

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