US1956922A - Internal combustion engine - Google Patents
Internal combustion engine Download PDFInfo
- Publication number
- US1956922A US1956922A US607388A US60738832A US1956922A US 1956922 A US1956922 A US 1956922A US 607388 A US607388 A US 607388A US 60738832 A US60738832 A US 60738832A US 1956922 A US1956922 A US 1956922A
- Authority
- US
- United States
- Prior art keywords
- crank
- yoke
- piston
- shaft
- cylinders
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Lifetime
Links
- 238000002485 combustion reaction Methods 0.000 title description 5
- 230000035939 shock Effects 0.000 description 4
- 230000006835 compression Effects 0.000 description 3
- 238000007906 compression Methods 0.000 description 3
- 230000000694 effects Effects 0.000 description 3
- 238000004880 explosion Methods 0.000 description 2
- 238000010304 firing Methods 0.000 description 2
- 230000010355 oscillation Effects 0.000 description 2
- 230000000452 restraining effect Effects 0.000 description 2
- 101100400378 Mus musculus Marveld2 gene Proteins 0.000 description 1
- 239000006096 absorbing agent Substances 0.000 description 1
- 235000019169 all-trans-retinol Nutrition 0.000 description 1
- 238000012550 audit Methods 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 230000008878 coupling Effects 0.000 description 1
- 238000010168 coupling process Methods 0.000 description 1
- 238000005859 coupling reaction Methods 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 238000006073 displacement reaction Methods 0.000 description 1
- 239000002360 explosive Substances 0.000 description 1
- 239000000446 fuel Substances 0.000 description 1
Images
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B75/00—Other engines
- F02B75/16—Engines characterised by number of cylinders, e.g. single-cylinder engines
- F02B75/18—Multi-cylinder engines
- F02B75/22—Multi-cylinder engines with cylinders in V, fan, or star arrangement
- F02B75/222—Multi-cylinder engines with cylinders in V, fan, or star arrangement with cylinders in star arrangement
-
- Y—GENERAL 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
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T74/00—Machine element or mechanism
- Y10T74/21—Elements
- Y10T74/2142—Pitmans and connecting rods
- Y10T74/2143—Radial
-
- Y—GENERAL 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
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T74/00—Machine element or mechanism
- Y10T74/21—Elements
- Y10T74/2142—Pitmans and connecting rods
- Y10T74/2144—Yieldable
Definitions
- This invention relatesto internal combustion engines of that type utilizing a plurality of cylinders extending outwardly from a crank case whereby the connectingrods of the pistons in the cylinders can all be mounted so as to exert successive driving forces upon the. crank in the case.
- One of the objects of the invention is to increase the leverage exerted from each piston upon the crank without necessitating the lengthening of the crank.
- a further object is to so arrange the cylinders that their longitudinal axes will be along lines extending in advance of the axis of rotation of the crank whereby the crushing and crystallizing effect resulting from firing on dead centers is practically overcome.
- a still further object is to utilize a resilient master connecting rod joining the crank to a guide piston at one end and to the several driving connecting rods at its other end whereby a cushioning action is set up for relieving side thrusts upon the guide piston resulting from the successive applications of power to the crank end of the resilient master rod.
- a further object is to provide a novel form of yokehead on the resilient master rod to which the connecting rods of the power piston are connected, the points of connection being so located as to insure maximum leverage upon the crank before the initial force of the explosion in each cylinder is expended.
- Another object is to lighten the motor, increase the life thereof by eliminating many of the strains to which a motor of this general type is subjected and to reduce the amount of fuel required for operation.
- Figure 1 is a central vertical section through the motor, some of the cylinders being in elevation and some of them being broken away.
- Figure 2 is a view showing in diagram the action of each power piston-in exerting a thrust in advance of the dead center so as to vary the lever age upon the crank shaft.
- Figure 3 is an enlarged view partly in central vertical section and partly in side elevation of the resilient master rod.
- Figure 4 is a plan view of the yoke-head of the master rod the coupling pins being removed.
- Figure 5 is a section through one of th pins.
- crank case concentric w e yoke referith the bearings 2 of a. crank shaft 3 and this crank case is provided at intervals in its periphery with openings 4 in which are mounted the inner ends of cylinders 5. the crank case by bolting flanges 6 thereto.
- each longitudinal axis a is ex tended in advance of the axis of rotation of the shaft and at no time alines with crank '7.
- An elongated cylinder 8 is extended from the crank case 1 and has its inner portion preferably flared toward the crank case, as shown at'9.
- a guide piston 10 the pin 11 of which is embraced by opposed yokes 12 each located at one end of a laminated 13. tended into a socket 14 formed by opposed spring
- the other ends of the two springs are explates 15 and these plates, in turn, are provided with opposed semi-cylindrical port-ions 16 which cooperate to form a bearing sleeve.
- the plates 15 are bolted together close to opposed portions of the sleeve shown at 18. through the socket l4 and those portions springs therein.
- Additional bolts 19 are extended of the As an additional means for holding the plates 15 together they are straddled by a clip 20 the threaded ends of which are extended through a clamping plate 21 and engaged by nuts 22.
- Each of the cylinders 5 has a power piston 27 mounted for reciprocation therein and the pin 28 in each cylinder has a connecting rod 29 which extends inwardly from its cylinder and into a space between the flanges 23 of the yoke.
- the openings 24 in these flanges provide seats for the ends of tubular bearing members 30 through which pins 31 are extended, these pins having heads 32 at one end and washers 33 at their other end for laping the outer sides of the flanges and holding the sleeves 30 against displacement.
- Each pin 31 and its washer 33 can be fastened in place by a nut 34.
- Each of the bearing sleeves 30 is engaged by one of the connecting rods 29and, as shown partlcularly in Figure 2, when a connecting rod is extended axially of its cylinder, as at the instant of firing, the center line thereof is not on a dead center with the crank '7 but extends in advance of the crank so that the explosive force will not exert a crystallizing or crushing effect upon the'parts but will, on the contrary, be expended with a powerful leverage effect on the crank, which leverage will increase as the force of the explosion diminishes.
- the point of connection 31 with the yoke will move with gradually increasing speed in the direction of rotation of the crank.
- the pin 31 is located at a distance from the point d equal to the distance of said point (1 from the axis of shaft 3 and the distance between point d and the nearest point I of the path g described by pin 31 is one-fourth of the smallest diameter of said path. See Figure 2.
- the path a intersects circle h described by point d, as shown in Figure 2. Consequently the back pressure set up by those pistonsj27where exhaust and compression is taking place will be greatly reduced as compared with engines in which the connecting rods are attached directly to the crank shaft.
- At least two pistons will constantly transmit power in substantially the same direction to drive the crankshaftandtoexert alateralthrustagainst themasterconnecting rod13 audits piston 10.
- "nnisflmeisnodangerofthismasterrodexerting a whipping or slapping action such as would occur should the power be transmitted abruptly and intermittently from the pistons to the yoke Importance is attached to the fact that while pin 31 travels in a path which is eccentric to shaft 3 the group of paths and piston assembly are balanced exactly off center of the crank shaft.
- a by-pass 35 is mounted in cylinder 8 so as to permit free reciprocation of piston 10 when desired.
- An engine of the class described including a crank case, a crank shaft therein, cylinders extending outwardly from the case with their longitudinal axes out of line with the axis of rotation of the shaft, pistons mounted for reciprocation in the cylinders, a yoke mounted on the crank of the shaft, connecting rods joining the pistons to the yoke, the point of connection between each rod and the yoke being in advance of the dead center of the crank shaft, and resilient shock absorbing means for restraining the yoke against rotation upon the crank.
- An engine of the class described including a crankcase, a crank shaft therein, cylinders extending outwardly from the case with their 1ongitudinal axes out of line with the axis of rotation of the shaft, pistons mounted on the crank of the shaft, connecting rods joining the pistons to the yoke, the point of connection between each 1 rod and the yoke being in advance of the dead center of the crank shaft, shock absorbing means for restraining the yoke against rotation upon the crank, including a stationary cylinder, a piston mounted for reciprocation therein and a re- 11 silient master rod connected to the yoke and.pivotally joined to said piston.
- An engine of the class described including a shaft having a crank, a split yoke carried by the crank, a resilient master rod'fixedly connected to the yoke, a cylinder, a piston in the cylinder and connected to the master rod whereby reciprocation and oscillation of the'yoke is set up by rotation of the crank, fixed cylinders, power pistons therein,'connecting rods extending from said pistons, and means joining each connecting rod to the yoke at a point out of line with the dead center of the crank and in the direction of rotation of the crank when the piston of said rod is at its point of maximum compression whereby said point of connection is caused to travel in a path intersecting the path of movement of the said rods at points in advance of the dead center of the crank and guiding the points of connection in paths eccentric to the shaft thereby to increase crank vantage on the power strokes and reduce back pressure vantage by each piston during its exhaust and compression strokes, said means including a yoke on the crank, a resilient master rod fixed to and
- An engine including a shaft having a crank, radial cylinders, pistons in the cylinders, con-
Description
2 Sheets-Sheet l elder/map.
May 1, 1934. J. D. INGRAM INTERNAL COMBUSTION ENGINE Filed April 25, 1932 May 1, 1934. J. D. INGRAM INTERNAL COMBUSTION ENGINE Filed April 25, 1932 2 Sheets-Sheet 2 momma Patented May 1934 UNITED STATES PATENT OFFICE 1,956,922 INTERNAL COMBUSTION ENGINE Joseph D. Ingram, La Jolla, Calif. Application April 25, 1932, Serial No. 607,388
6 Claims.
This invention relatesto internal combustion engines of that type utilizing a plurality of cylinders extending outwardly from a crank case whereby the connectingrods of the pistons in the cylinders can all be mounted so as to exert successive driving forces upon the. crank in the case.
One of the objects of the invention is to increase the leverage exerted from each piston upon the crank without necessitating the lengthening of the crank.
A further object is to so arrange the cylinders that their longitudinal axes will be along lines extending in advance of the axis of rotation of the crank whereby the crushing and crystallizing effect resulting from firing on dead centers is practically overcome. I
A still further object is to utilize a resilient master connecting rod joining the crank to a guide piston at one end and to the several driving connecting rods at its other end whereby a cushioning action is set up for relieving side thrusts upon the guide piston resulting from the successive applications of power to the crank end of the resilient master rod.
A further object is to provide a novel form of yokehead on the resilient master rod to which the connecting rods of the power piston are connected, the points of connection being so located as to insure maximum leverage upon the crank before the initial force of the explosion in each cylinder is expended.
Another object is to lighten the motor, increase the life thereof by eliminating many of the strains to which a motor of this general type is subjected and to reduce the amount of fuel required for operation.
With the foregoing and other objects in view which will appear as the description proceeds, the invention resides in the combination and arrangement of parts and in the details of construction hereinafter described and claimed, it being understood that changes in the precise embodiment of the invention herein disclosed may be made'within thescope of what is c'iaimed without departing from the spirit of the invention.
In the accompanying drawings the preferred form of the invention has been shown.
In said drawings;
Figure 1 is a central vertical section through the motor, some of the cylinders being in elevation and some of them being broken away.
Figure 2 is a view showing in diagram the action of each power piston-in exerting a thrust in advance of the dead center so as to vary the lever age upon the crank shaft.
Figure 3 is an enlarged view partly in central vertical section and partly in side elevation of the resilient master rod.
Figure 4 is a plan view of the yoke-head of the master rod the coupling pins being removed.
Figure 5 is a section through one of th pins.
Referring to the figures by characters of ence, 1 designates a crank case concentric w e yoke referith the bearings 2 of a. crank shaft 3 and this crank case is provided at intervals in its periphery with openings 4 in which are mounted the inner ends of cylinders 5. the crank case by bolting flanges 6 thereto.
These cylinders can be secured to When the cylinders are properly located their longitudinal axes will be out of line with the axis 0 f rotation of crank shaft 3 and, as indicated particularly in Figure 2, each longitudinal axis a is ex tended in advance of the axis of rotation of the shaft and at no time alines with crank '7.
An elongated cylinder 8 is extended from the crank case 1 and has its inner portion preferably flared toward the crank case, as shown at'9. In this cylinder 8 is mounted a guide piston 10 the pin 11 of which is embraced by opposed yokes 12 each located at one end of a laminated 13. tended into a socket 14 formed by opposed spring The other ends of the two springs are explates 15 and these plates, in turn, are provided with opposed semi-cylindrical port-ions 16 which cooperate to form a bearing sleeve.
In addition to the bolts 1'7 which are used for holding the yokes or split sleeve 12 in engagement with pin 11, the plates 15 are bolted together close to opposed portions of the sleeve shown at 18. through the socket l4 and those portions springs therein.
Additional bolts 19 are extended of the As an additional means for holding the plates 15 together they are straddled by a clip 20 the threaded ends of which are extended through a clamping plate 21 and engaged by nuts 22.
tric with sleeve 16. If desired those ends of the flanges remote from socket 14 can be formed with alining sleeves 25 for receiving tie bolts wch thus constitute a further means for pr spreading of sleeve 16. Sleeve 16, plates 15 and flanges 23 form a yoke and the laminated springs 13 constitute a resilient master rod which connects this yoke to the pin 11 in piston 10.
Each of the cylinders 5 has a power piston 27 mounted for reciprocation therein and the pin 28 in each cylinder has a connecting rod 29 which extends inwardly from its cylinder and into a space between the flanges 23 of the yoke. The openings 24 in these flanges provide seats for the ends of tubular bearing members 30 through which pins 31 are extended, these pins having heads 32 at one end and washers 33 at their other end for laping the outer sides of the flanges and holding the sleeves 30 against displacement. Each pin 31 and its washer 33 can be fastened in place by a nut 34.
Each of the bearing sleeves 30 is engaged by one of the connecting rods 29and, as shown partlcularly in Figure 2, when a connecting rod is extended axially of its cylinder, as at the instant of firing, the center line thereof is not on a dead center with the crank '7 but extends in advance of the crank so that the explosive force will not exert a crystallizing or crushing effect upon the'parts but will, on the contrary, be expended with a powerful leverage effect on the crank, which leverage will increase as the force of the explosion diminishes. For example, as the piston 27 moves inwardly the point of connection 31 with the yoke will move with gradually increasing speed in the direction of rotation of the crank. For example; should the pin 31 move from point b to point e, the distance thus travelled would be twice the distance from d to e travelled by the crank '7. Thus the leverage exerted is much greater than that which could be obtained by any direct connection between the connecting rod 29 and the crank '7 because the thrust is along. lines more remote from the dead center.
The several pistons operate in rapid succession, the action of each piston being duplicated by that of the others. Obviously the exertion of thrust along lines in advance of the point of connection between the yoke and the crank will tend to set up an excessive transverse pressure,
or whipping action -upon the guide piston 10. This isgreatly reduced, however, by utilizing the resilient master rod 13 which acts as a shock absorber and insures smooth and quiet operation. It is evident that by using along master rod the movement of the yoke out of the plane of its piston will be correspondingly reduced, thereby reducing the elliptic circles and side thrust that destroy balance at high speed. The average service plane wears out three motors, due mostly to the fact that the yoke is attached to a short power rod.
The pin 31 is located at a distance from the point d equal to the distance of said point (1 from the axis of shaft 3 and the distance between point d and the nearest point I of the path g described by pin 31 is one-fourth of the smallest diameter of said path. See Figure 2. The path a intersects circle h described by point d, as shown in Figure 2. Consequently the back pressure set up by those pistonsj27where exhaust and compression is taking place will be greatly reduced as compared with engines in which the connecting rods are attached directly to the crank shaft.
In an engine constructed as described, at least two pistonswill constantly transmit power in substantially the same direction to drive the crankshaftandtoexert alateralthrustagainst themasterconnecting rod13 audits piston 10. "nnisflmeisnodangerofthismasterrodexerting a whipping or slapping action such as would occur should the power be transmitted abruptly and intermittently from the pistons to the yoke Importance is attached to the fact that while pin 31 travels in a path which is eccentric to shaft 3 the group of paths and piston assembly are balanced exactly off center of the crank shaft. A by-pass 35 is mounted in cylinder 8 so as to permit free reciprocation of piston 10 when desired.
What is claimed is:
1. An engine of the class described including a crank case, a crank shaft therein, cylinders extending outwardly from the case with their longitudinal axes out of line with the axis of rotation of the shaft, pistons mounted for reciprocation in the cylinders, a yoke mounted on the crank of the shaft, connecting rods joining the pistons to the yoke, the point of connection between each rod and the yoke being in advance of the dead center of the crank shaft, and resilient shock absorbing means for restraining the yoke against rotation upon the crank.
2. An engine of the class described including a crankcase, a crank shaft therein, cylinders extending outwardly from the case with their 1ongitudinal axes out of line with the axis of rotation of the shaft, pistons mounted on the crank of the shaft, connecting rods joining the pistons to the yoke, the point of connection between each 1 rod and the yoke being in advance of the dead center of the crank shaft, shock absorbing means for restraining the yoke against rotation upon the crank, including a stationary cylinder, a piston mounted for reciprocation therein and a re- 11 silient master rod connected to the yoke and.pivotally joined to said piston.
, 3. In an engine of the class described the combination with a shaft havingv a crank, a crank case housing the crank and cylinders extending outwardly from the case, of power pistons mounted for reciprocation in the cylinders along lines out of line with the dead center of the crank, a yoke mounted on the crank, a resilient shock ab sorbing master rod rigidly connected to the yoke 1 and mounted to oscillate and reciprocate, and rods connecting the power pistons to the yoke at points spaced from the center of the crank a distance equal to that between the center of the crank and the axial center of the shaft, each of said points being in advance of dead center of the crank whereby the point of connection between the connecting rod and the yoke will travel at twice the speed of the axial center of the yoke, during the power stroke.
4. An engine of the class described including a shaft having a crank, a split yoke carried by the crank, a resilient master rod'fixedly connected to the yoke, a cylinder, a piston in the cylinder and connected to the master rod whereby reciprocation and oscillation of the'yoke is set up by rotation of the crank, fixed cylinders, power pistons therein,'connecting rods extending from said pistons, and means joining each connecting rod to the yoke at a point out of line with the dead center of the crank and in the direction of rotation of the crank when the piston of said rod is at its point of maximum compression whereby said point of connection is caused to travel in a path intersecting the path of movement of the said rods at points in advance of the dead center of the crank and guiding the points of connection in paths eccentric to the shaft thereby to increase crank vantage on the power strokes and reduce back pressure vantage by each piston during its exhaust and compression strokes, said means including a yoke on the crank, a resilient master rod fixed to and extending from the yoke and mounted for oscillation and reciprocation, and a stationary guide for the outer end of the master rod.
6. An engine including a shaft having a crank, radial cylinders, pistons in the cylinders, con-
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US607388A US1956922A (en) | 1932-04-25 | 1932-04-25 | Internal combustion engine |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US607388A US1956922A (en) | 1932-04-25 | 1932-04-25 | Internal combustion engine |
Publications (1)
Publication Number | Publication Date |
---|---|
US1956922A true US1956922A (en) | 1934-05-01 |
Family
ID=24432055
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US607388A Expired - Lifetime US1956922A (en) | 1932-04-25 | 1932-04-25 | Internal combustion engine |
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Country | Link |
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US (1) | US1956922A (en) |
Cited By (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2550392A (en) * | 1946-05-10 | 1951-04-24 | John Venning & Company Ltd | Hydraulic reciprocating pump |
US2561000A (en) * | 1946-02-21 | 1951-07-17 | Hartford Nat Bank & Trust Co | Wobbler drive mechanism |
US2848202A (en) * | 1956-01-06 | 1958-08-19 | William E Leibing | Degasser |
US2903909A (en) * | 1955-06-14 | 1959-09-15 | Engel Wolfgang | Pitmans or links for sewing machine transmissions |
US2941419A (en) * | 1956-03-12 | 1960-06-21 | Allis Chalmers Mfg Co | Pitman |
US4596160A (en) * | 1983-01-14 | 1986-06-24 | Ac Energi Aps | Mechanism for transferring movements between first and second linearly displaceable bodies |
US4945866A (en) * | 1987-03-26 | 1990-08-07 | Chabot Jr Bertin R | Altered piston timing engine |
US20110252903A1 (en) * | 2011-04-27 | 2011-10-20 | Flight Medical Innovations Ltd. | Mechanical ventilator |
-
1932
- 1932-04-25 US US607388A patent/US1956922A/en not_active Expired - Lifetime
Cited By (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2561000A (en) * | 1946-02-21 | 1951-07-17 | Hartford Nat Bank & Trust Co | Wobbler drive mechanism |
US2550392A (en) * | 1946-05-10 | 1951-04-24 | John Venning & Company Ltd | Hydraulic reciprocating pump |
US2903909A (en) * | 1955-06-14 | 1959-09-15 | Engel Wolfgang | Pitmans or links for sewing machine transmissions |
US2848202A (en) * | 1956-01-06 | 1958-08-19 | William E Leibing | Degasser |
US2941419A (en) * | 1956-03-12 | 1960-06-21 | Allis Chalmers Mfg Co | Pitman |
US4596160A (en) * | 1983-01-14 | 1986-06-24 | Ac Energi Aps | Mechanism for transferring movements between first and second linearly displaceable bodies |
US4945866A (en) * | 1987-03-26 | 1990-08-07 | Chabot Jr Bertin R | Altered piston timing engine |
US20110252903A1 (en) * | 2011-04-27 | 2011-10-20 | Flight Medical Innovations Ltd. | Mechanical ventilator |
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