US1978194A - Internal combustion engine - Google Patents

Internal combustion engine Download PDF

Info

Publication number
US1978194A
US1978194A US517876A US51787631A US1978194A US 1978194 A US1978194 A US 1978194A US 517876 A US517876 A US 517876A US 51787631 A US51787631 A US 51787631A US 1978194 A US1978194 A US 1978194A
Authority
US
United States
Prior art keywords
shaft
cylinders
disks
ring
internal combustion
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
Application number
US517876A
Inventor
Gray Edward
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
EDWARD GRAY ENGINEER Inc
Original Assignee
EDWARD GRAY ENGINEER Inc
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by EDWARD GRAY ENGINEER Inc filed Critical EDWARD GRAY ENGINEER Inc
Priority to US517876A priority Critical patent/US1978194A/en
Application granted granted Critical
Publication of US1978194A publication Critical patent/US1978194A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • 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
    • F02B75/282Engines with two or more pistons reciprocating within same cylinder or within essentially coaxial cylinders the pistons having equal strokes
    • 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
    • F02B75/26Engines with cylinder axes coaxial with, or parallel or inclined to, main-shaft axis; Engines with cylinder axes arranged substantially tangentially to a circle centred on main-shaft axis
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B3/00Engines characterised by air compression and subsequent fuel addition
    • F02B3/06Engines characterised by air compression and subsequent fuel addition with compression ignition

Definitions

  • the present invention pertains to a novel internal combustion engine designed particularly to operate by the direct or solid injection of oil or on a modified Diesel principle.
  • the object of the invention is to provide a simple and efficient construction in an engine of this type having opposed pistons in each cylinder.
  • the cylinder assembly consists essentially of a circular series of separate cylinders held by two end housings.
  • the end housings constitute heads which comprise a part of the cooling system and also carry the means for admitting air and exhausting the burned gases.
  • the flow from the cylinders to these means is governed by the position of the pistons in each cylinder.
  • the reciprocating motion of the pistons is converted into rotary motion of the shaft through the medium of swash disks disposed at an angle to the shaft.
  • the disks On the power stroke of the pistons, the disks have a tendency to elongate and bend the shaft.
  • Another object of the invention is to free the shaft from this action of the disks and is accomplished by inserting between the disks a member which permits an initial tension being put on the shaft in such a manner that bending and elongating are prevented.
  • Figs. 2, 3 and 4 are sections on the lines 2-2, 3-3 and 4-4 of Figure 1;
  • Fig. 5 is a section on the line 5:5 of Figure 3;
  • Fig. 6 is an elevation of a modified construction
  • Figs. 7 and 8 are respectively a plan view and vertical section of a modified universal joint
  • Figs. 9 and 10 are respectively a plan view and vertical section of another universal joint; and Figs. 11 and 12 are respectively a vertical section and plan view of still another form of universal joint. Reference to these views will now be made by use of like characters which are employed to designate corresponding parts throughout.
  • the cylinder and water jacket assembly consists of a central assembly of separate cylinders and two end members or housings 2 and 2' as may be seen more clearly in Figure 1.
  • the central assembly consists of cylinders 3 arranged in a circular series. Around the central portion of each cylinder is formed a concentric wall 4 spaced 55 from the cylinder wall to form a water jacket 5.
  • the housings 2 and 2 are of substantially similar construction and may therefore be described together.
  • the inner ends of the hon sings overlap the ends of the cylinders and are formed with bosses 6 and 6 to receive the cylinders.
  • Each housing moreover has a central boss "I, the center of which is the center of the circular series of bosses 6 and 6.
  • the inner ends of the housings abut the ends of the cylinders 3 as shown in Figure 1.
  • the assembly is maintained by a sleeve 8 passed through the bosses 7 and having its ends equipped with nuts 9 which are tightened against partitions 10 and 10' within the housings at the outer ends of the bosses 7, whereby the housings are clamped inwardly against the central assembly of separate cylinders.
  • the housing 2 has another partition 11 between its inner end and the partition 10. Both partitions obviously are apertured for the passage of the cylinders 3 therethrough.
  • the partition 11 forms a water space 12 at the inner end 30 of the housing 2, and this space is brought into communication with the water space 5 of the member 1 by coincident ports 13 formed in the abutting ends of these parts.
  • the partitions l0 and 11 form an air chamber 14 at one end of the cylinders and in communication therewith through ports 15. Suitable intake ports 16-to the chamber 14 are provided preferably at diametrically opposite points in the outer wall of the hous- -ing 2 as shown in Figures 1 and 3.
  • the partition 10' also forms a water space 1? around the cylinders 3, and this space is also brought into communication with the space 5 by coincident ports 18 formed in the abutting parts of the members 3 and 2'.
  • the bosses 6' have a channel formation 19 lying outwardly of the bosses or between the bosses and common to all the bosses.
  • the base of this channel structure forms a ring 20 concentric with theboss 7 as may be seen in Figure 2.
  • the side walls of the channel converge outwardly at 21 to two diametrically opposite exhaust ports 22 in the outer wall of the housing 2'. Communication for exhaust from the cylinders 3 to the channel 19 is provided by ports 23 in the cylinder walls of the channel.
  • An inner circular wall 24 is formed across the exhaust channel 19 at a short distance inwardly of the outer wall of the housing 2' to form a water space 25 afiordingcommunication between the parts of the water space 17 at opposite sides of the channel.
  • the wall 24 is of course interrupted at the exhaust ports 22 and there joined as at 26 to the outer wall of the housing 2'.
  • a water inlet 27 and an outlet 28 are provided respectively at the bottom of the housing 2 and the top of housing 2', in communication with the spaces 17 and 12 respectively as shown in Figure 1. Due to the diagonal relation of the inlet and outlet with respect to the cylinders, the cooling water must flow parallel to the cylinders in passing through the cooling system. The paths from the inlet 27 through any one of the water jackets 5 to the outlet 28 are equal, and there will therefore be an equal distribution or flow of water among the jackets 5.
  • Each of the cylinders 3 contains a pair of opposed pistons 30 equipped with outwardly extending connecting rods 31 which in turn are geared to a power shaft as will presently be described.
  • End plates 32 are secured to the outer ends of the housings 2 and 2' and formed with suitable bearing structures 33 in which is journalled a power shaft 34.
  • the reciprocating motion of the connecting rods 31 is converted into rotary motion on the shaft 34 by means of swash disks 35 surrounding the shaft at an acute angle and splined thereto as at 36 beyond the outer ends of the cylinders.
  • Each such disk is surrounded by a ring structure comprising two parts 37 and 38 threaded one into the other, with ball bearings 39 between the ring and the disk.
  • the function of the ring is merely to carry ball members 40 for providing a universal joint with the connecting rods 31.
  • the outer end of each rod is formed with a spherical socket 41 receiving a portion of one of the balls 40, and the joint is completed by a spherical cap member 42 fitted on each ball and bolted as at 43 to the corresponding socket member 41.
  • Each cylinder is equipped with a nozzle 44 approximately midway between its ends. This nozzle is constructed to spray a charge of atomized fuelinto the space between the pistons when the latter have reached their minimum spacing in compressing a quantity of air therebetween. At this time, the temperature of the compressed air is sufficient to ignite the mixture of air and sprayed fuel, whereupon an expansion or separation of the pistons follows in accordance with the Diesel principle of operation.
  • a compression member or sleeve 45 is mounted around the shaft between the disks 35.
  • the ends of the sleeves are thickened as at 46 to fit snugly around the shaft, while the intermediate part of the sleeve is spaced from the shaft.
  • the ends 46 are abutted by hubs 47 formed as part of the disks 35.
  • the outer end of one of the hubs bears against a stop collar 48 on the-shaft 34.
  • the outer end of the hub of the other disk is engaged by a nut 49 threaded on the shaft. This nut is adjusted to bind the disks against the sleeve 45.
  • the pushing action of the connecting rods 31 on the disks 35 tends to rock the latter about the ends of the members 45 and thus to elongate the shaft 34 by the outward force against the members 48 and 59.
  • the shaft is placed in a condition of initial tension by suificient tightening of the nut 49.
  • the intermediate parts, namely the sleeve 45 and hubs 47 are of sufiiciently low compressibility to resist the reaction of the tension in the shaft and to maintain the shaft in its condition of initial tension.
  • the magnitude of this tension is greater than the tension or elongation effect produced upon the members 48 and 49 through the connecting rods and hubs of the disks as described, and hence the latter tendency is ineffective on the shaft.
  • each of the housings 2 and 2' is formed with a track 2a extending lengthwise of the shaft 34 and curved about the center of oscillation of the corresponding disk 35.
  • Each of the rings has a stem 37a extending therefrom on which is slidably mounted a block 37b received in the track to move therein.
  • either disk may be advanced or retarded with respect to the other so that they will be unsymmetrical with respect to a vertical plane passed transversely through the cylinders 3.
  • the nut 49 is removed and the connecting rods 31 are removed from the balls 40.
  • Theswash disk 35 is then slipped off the splines 36 and is rotated slightly while the shaft 34 remains stationary, and it is then replaced on the splines, the nut 49 is replaced, and the connecting rods re-assembled on the balls 40.
  • disk within the housing 2' for example, is advanced, a piston connected thereto will close the exhaust ports 23 of the corresponding cylinder before the air admission ports 15 in the same cylinder are closed. This will result in supercharging of the cylinder with compressed air.
  • the water jackets are replaced by cooling fins 50 formed exteriorly on the cylinders.
  • the air intake channel and the exhaust channel are built up from the cylinders as indicated by the numerals 51 and 52.
  • Figures 7 to 12 inclusive illustrate various other constructions for providing a universal connection between the connecting rods and the In Figures 7 and 8, the ring swash disk rings.
  • the part 53 is formed with an upstanding lug 56 through which is passed a pin 57.
  • a ring 58 surrounds the pin and has bearings 59 in which the ends of the pin are received.
  • the ring further has a peripheral groove 60 in which is mounted a spring ring 61.
  • the connecting rod 62 has its outer end formed as a ring 63 adapted to be fitted over the ring 58 When the spring ring 61 is compressed in the groove 60.
  • the ring 63 has an inner groove 64 adapted to register with the groove 60, whereupon the spring ring 61 enters partially into the latter groove to hold the parts together while permitting relative rotation therebetween on an axis perpendicular to that of the pin 57.
  • screws may be turned in tapped holes 63' in the outer ring until the spring ring 81 is forced entirely into the groove 60, after which the outer ring may be withdrawn.
  • the ring surrounding the swash disk also comprises two parts 65 and 66 tied together by a bolt 6'7.
  • Thepart 66 is formed with a pair of spaced ears 68 between which is journalled a block 69 on trunnions '70.
  • the block also has trunnions 71 extending therefrom on an axis perpendicular to that of the members 70.
  • connecting rod comprises two similar pieces '72 bolted together at 73 and formed each with an offset portion '74 at each end to provide forks adapted to be journalled on the trunnions '71 and on a similar block 75 journalled in the piston 76,.
  • a universal joint is provided between the piston and the rod and between the rod and the swash disk ring.
  • the swash disk ring consists of two parts 77 and '78 bolted together at 79.
  • the connecting rod 80 has its outer end fcrmed'with a ball 81 received in a socket82 into which the ball 81 is mounted prior to the application of the section '77.
  • the latter has a like socket 83 engaging the ball and thereby preventing it frombeing withdrawn in any direction.
  • the section 78 has a slot 84 communicating with the socket 82 thereof.
  • An internal combustion engine comprising parallel cylinders, a shaft between said cylinders and parallel thereto, a pair of opposed pistons in each cylinder, a pair of swash disks on said shaft at the ends of said cylinders, a ring rotatably mounted on each, disk, connecting rods extending from said pistons and having universal connections with said ring, a sleeve surrounding said shaft between said disks and enga ed thereby, and means on said shaft engaging the outer sides of said disks and holding said shaft under initial tension.
  • An internal combustion engine comprising parallel cylinders, a shaft between said cylinders and parallel thereto, a pair of opposed pistons in each cylinder, a. pair of swash disks on said shaft at the ends of said cylinders, a ring rotatably mounted on each disk, connecting rods extending from said pistons and having universal connections with said ring, a sleeve surrounding aid shaft between said disks, and means binding said disks against the ends of said sleeve and holding said shaft under initial tension.
  • An internal combustion engine comprising parallel cylinders, a shaft between said cylinders and parallel thereto, a pair of opposed pistons in each cylinder, a pair of swash disks on said shaft at the ends of said cylinders, connecting rods extending from said pistons and joined to said disks, means for holding said disks in spaced relation, and means engaging said disks for holding said shaft tinder initial tension.
  • An internal combustion engine comprising parallel cylinders, a shaft between said cylinders and parallel thereto, a pair of opposed pistons in each cylinder, a pair of swash disks on said shaft at the ends of said cylinders, a ring rotatably mounted on each disk, connecting rods extending from said pistons and having universal connections with said ring, means for holding said disks in spaced relation, and means engaging said disks for holding said shaft under initial tension.
  • An internal combustion engine comprising parallel cylinders, a shaft between said cylinders and parallel thereto, a pair of opposed pistons in each cylinder, a pair of swash disks on said shaft at the ends of said cylinders, connecting rods extending from said pistons and joined to said disks, a sleeve surrounding said shaft between said disks and engaged thereby, and means on said shaft engaging the outer sides of said disks and holding said shaft under initial tension.
  • An internal combustion engine comprising parallel cylinders, a shaft between said cylinders and parallel thereto, a pair of opposed pistons in each cylinder, a pair of swash disks on said shaft at the ends of said-cylinders, connecting rods extending from said pistons and joined to said disks, a sleeve surrounding said shaft between said disks, and means binding said disks against the ends of said sleeve and holding said shaft under initial tension.

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Cylinder Crankcases Of Internal Combustion Engines (AREA)

Description

E; GRAY ,9 8,19
INTERNAL COMBUSTION ENGINE Filed Feb. 24, 1931 3 Sheet sSheet l Oct. 23, 1934. E. GRAY I INTERNAL COMBUSTION ENGINE I Filed Feb.
' s Sheets-Sheet 2 Ell/111111, Illlllllllllllllllllliiilllllllln mini 7 INVENTOR UNITED STATES PATENT OFFICE INTERNAL COMBUSTION ENGINE Edward Gray, Detroit, Mich., assignor to Edward Gray, Engineer, Inc., Detroit, llIich., a corporation of Michigan Application February 24, 1931, Serial No. 517,876
7 Claims.
The present invention pertains to a novel internal combustion engine designed particularly to operate by the direct or solid injection of oil or on a modified Diesel principle.
The object of the invention is to provide a simple and efficient construction in an engine of this type having opposed pistons in each cylinder. In keeping with this object, the cylinder assembly consists essentially of a circular series of separate cylinders held by two end housings. The end housings constitute heads which comprise a part of the cooling system and also carry the means for admitting air and exhausting the burned gases. The flow from the cylinders to these means is governed by the position of the pistons in each cylinder.
The reciprocating motion of the pistons is converted into rotary motion of the shaft through the medium of swash disks disposed at an angle to the shaft. On the power stroke of the pistons, the disks have a tendency to elongate and bend the shaft. Another object of the invention is to free the shaft from this action of the disks and is accomplished by inserting between the disks a member which permits an initial tension being put on the shaft in such a manner that bending and elongating are prevented.
The invention is fully disclosed by way of example in the following description and in the accompanying drawings, in which- Figure 1 is a longitudinal section of an engine constructed according to the invention;
Figs. 2, 3 and 4 are sections on the lines 2-2, 3-3 and 4-4 of Figure 1;
Fig. 5 is a section on the line 5:5 of Figure 3;
Fig. 6 is an elevation of a modified construction;
Figs. 7 and 8 are respectively a plan view and vertical section of a modified universal joint;
40 Figs. 9 and 10 are respectively a plan view and vertical section of another universal joint; and Figs. 11 and 12 are respectively a vertical section and plan view of still another form of universal joint. Reference to these views will now be made by use of like characters which are employed to designate corresponding parts throughout.
The cylinder and water jacket assembly consists of a central assembly of separate cylinders and two end members or housings 2 and 2' as may be seen more clearly in Figure 1. The central assembly consists of cylinders 3 arranged in a circular series. Around the central portion of each cylinder is formed a concentric wall 4 spaced 55 from the cylinder wall to form a water jacket 5.
It will also be seen in Figure 1 that the wall 4 is considerably shorter than the cylinder 3 which it surrounds and in fact occupies a position midway between the ends of the cylinder,
The housings 2 and 2 are of substantially similar construction and may therefore be described together. The inner ends of the hon sings overlap the ends of the cylinders and are formed with bosses 6 and 6 to receive the cylinders. Each housing moreover has a central boss "I, the center of which is the center of the circular series of bosses 6 and 6. The inner ends of the housings abut the ends of the cylinders 3 as shown in Figure 1. The assembly is maintained by a sleeve 8 passed through the bosses 7 and having its ends equipped with nuts 9 which are tightened against partitions 10 and 10' within the housings at the outer ends of the bosses 7, whereby the housings are clamped inwardly against the central assembly of separate cylinders.
' The housing 2 has another partition 11 between its inner end and the partition 10. Both partitions obviously are apertured for the passage of the cylinders 3 therethrough. The partition 11 forms a water space 12 at the inner end 30 of the housing 2, and this space is brought into communication with the water space 5 of the member 1 by coincident ports 13 formed in the abutting ends of these parts. The partitions l0 and 11 form an air chamber 14 at one end of the cylinders and in communication therewith through ports 15. Suitable intake ports 16-to the chamber 14 are provided preferably at diametrically opposite points in the outer wall of the hous- -ing 2 as shown in Figures 1 and 3.
The partition 10' also forms a water space 1? around the cylinders 3, and this space is also brought into communication with the space 5 by coincident ports 18 formed in the abutting parts of the members 3 and 2'.
The bosses 6' have a channel formation 19 lying outwardly of the bosses or between the bosses and common to all the bosses. The base of this channel structure forms a ring 20 concentric with theboss 7 as may be seen in Figure 2. At two points, the side walls of the channel converge outwardly at 21 to two diametrically opposite exhaust ports 22 in the outer wall of the housing 2'. Communication for exhaust from the cylinders 3 to the channel 19 is provided by ports 23 in the cylinder walls of the channel.
An inner circular wall 24 is formed across the exhaust channel 19 at a short distance inwardly of the outer wall of the housing 2' to form a water space 25 afiordingcommunication between the parts of the water space 17 at opposite sides of the channel. The wall 24 is of course interrupted at the exhaust ports 22 and there joined as at 26 to the outer wall of the housing 2'. A water inlet 27 and an outlet 28 are provided respectively at the bottom of the housing 2 and the top of housing 2', in communication with the spaces 17 and 12 respectively as shown in Figure 1. Due to the diagonal relation of the inlet and outlet with respect to the cylinders, the cooling water must flow parallel to the cylinders in passing through the cooling system. The paths from the inlet 27 through any one of the water jackets 5 to the outlet 28 are equal, and there will therefore be an equal distribution or flow of water among the jackets 5.
Each of the cylinders 3 contains a pair of opposed pistons 30 equipped with outwardly extending connecting rods 31 which in turn are geared to a power shaft as will presently be described. End plates 32 are secured to the outer ends of the housings 2 and 2' and formed with suitable bearing structures 33 in which is journalled a power shaft 34.
The reciprocating motion of the connecting rods 31 is converted into rotary motion on the shaft 34 by means of swash disks 35 surrounding the shaft at an acute angle and splined thereto as at 36 beyond the outer ends of the cylinders. Each such disk is surrounded by a ring structure comprising two parts 37 and 38 threaded one into the other, with ball bearings 39 between the ring and the disk. The function of the ring is merely to carry ball members 40 for providing a universal joint with the connecting rods 31. The outer end of each rod is formed with a spherical socket 41 receiving a portion of one of the balls 40, and the joint is completed by a spherical cap member 42 fitted on each ball and bolted as at 43 to the corresponding socket member 41. Inasmuch as the reciprocation of the connecting rods cannot pull or push the disks 35 in the direction of piston travel, the rings 37, 38 are compelled to change their angular position relatively to the shaft 34, which is permitted only by rotary movement of the disks on their centers. This movement results in rotation of the shaft since the disks are splined to the shaft.
Each cylinder is equipped with a nozzle 44 approximately midway between its ends. This nozzle is constructed to spray a charge of atomized fuelinto the space between the pistons when the latter have reached their minimum spacing in compressing a quantity of air therebetween. At this time, the temperature of the compressed air is sufficient to ignite the mixture of air and sprayed fuel, whereupon an expansion or separation of the pistons follows in accordance with the Diesel principle of operation.
The pistons in separating produce a strain in the disks 35 which tends to elongate and bend the shaft 34. In order to overcome this tendency, a compression member or sleeve 45 is mounted around the shaft between the disks 35. The ends of the sleeves are thickened as at 46 to fit snugly around the shaft, while the intermediate part of the sleeve is spaced from the shaft. The ends 46 are abutted by hubs 47 formed as part of the disks 35. The outer end of one of the hubs bears against a stop collar 48 on the-shaft 34. The outer end of the hub of the other disk is engaged by a nut 49 threaded on the shaft. This nut is adjusted to bind the disks against the sleeve 45.
The pushing action of the connecting rods 31 on the disks 35 tends to rock the latter about the ends of the members 45 and thus to elongate the shaft 34 by the outward force against the members 48 and 59. To overcome this tendency, the shaft is placed in a condition of initial tension by suificient tightening of the nut 49. The intermediate parts, namely the sleeve 45 and hubs 47, are of sufiiciently low compressibility to resist the reaction of the tension in the shaft and to maintain the shaft in its condition of initial tension. The magnitude of this tension is greater than the tension or elongation effect produced upon the members 48 and 49 through the connecting rods and hubs of the disks as described, and hence the latter tendency is ineffective on the shaft.
In order to prevent rotation of the rings 37, 38 with the disks 35, each of the housings 2 and 2' is formed with a track 2a extending lengthwise of the shaft 34 and curved about the center of oscillation of the corresponding disk 35. Each of the rings has a stem 37a extending therefrom on which is slidably mounted a block 37b received in the track to move therein. By this means, the rotation is confined to the disks 35 and shaft 34.
By reason of the splined mounting of the disks 35 on the shaft 34, either disk may be advanced or retarded with respect to the other so that they will be unsymmetrical with respect to a vertical plane passed transversely through the cylinders 3. To make such an advancing or retarding adjustment the nut 49 is removed and the connecting rods 31 are removed from the balls 40.
Theswash disk 35 is then slipped off the splines 36 and is rotated slightly while the shaft 34 remains stationary, and it is then replaced on the splines, the nut 49 is replaced, and the connecting rods re-assembled on the balls 40. disk within the housing 2', for example, is advanced, a piston connected thereto will close the exhaust ports 23 of the corresponding cylinder before the air admission ports 15 in the same cylinder are closed. This will result in supercharging of the cylinder with compressed air.
In the modification shown in Figure 6, the water jackets are replaced by cooling fins 50 formed exteriorly on the cylinders. The air intake channel and the exhaust channel are built up from the cylinders as indicated by the numerals 51 and 52.
Figures 7 to 12 inclusive illustrate various other constructions for providing a universal connection between the connecting rods and the In Figures 7 and 8, the ring swash disk rings. is formed in two parts 53 and 54 secured together by a bolt 55. The part 53 is formed with an upstanding lug 56 through which is passed a pin 57. A ring 58 surrounds the pin and has bearings 59 in which the ends of the pin are received. The ring further has a peripheral groove 60 in which is mounted a spring ring 61. The connecting rod 62 has its outer end formed as a ring 63 adapted to be fitted over the ring 58 When the spring ring 61 is compressed in the groove 60. The ring 63 has an inner groove 64 adapted to register with the groove 60, whereupon the spring ring 61 enters partially into the latter groove to hold the parts together while permitting relative rotation therebetween on an axis perpendicular to that of the pin 57. To separate the rings 58 and 63, screws may be turned in tapped holes 63' in the outer ring until the spring ring 81 is forced entirely into the groove 60, after which the outer ring may be withdrawn.
In the construction shown in Figures 9 and 10, the ring surrounding the swash disk also comprises two parts 65 and 66 tied together by a bolt 6'7. Thepart 66 is formed with a pair of spaced ears 68 between which is journalled a block 69 on trunnions '70. The block also has trunnions 71 extending therefrom on an axis perpendicular to that of the members 70. The
connecting rod comprises two similar pieces '72 bolted together at 73 and formed each with an offset portion '74 at each end to provide forks adapted to be journalled on the trunnions '71 and on a similar block 75 journalled in the piston 76,. Thus, a universal joint is provided between the piston and the rod and between the rod and the swash disk ring. r
In the modification shown in Figures 11 and 12, the swash disk ring consists of two parts 77 and '78 bolted together at 79. The connecting rod 80 has its outer end fcrmed'with a ball 81 received in a socket82 into which the ball 81 is mounted prior to the application of the section '77. The latter has a like socket 83 engaging the ball and thereby preventing it frombeing withdrawn in any direction. The section 78 has a slot 84 communicating with the socket 82 thereof. When it is desired to remove the ball from the swash disk ring, the section 77 is'released and withdrawn. The ball 81 is also withdrawn in the same direction, and after it, has been removed from the socket 82, the rod 80 may be passed through the slot 84.
Although specific embodiments of the invention have been illustrated and described, it will be understood that ,various alterations in the details of construction may be made without departing from the scope of the invention, as indicated by the appended claims.
What I claim is:- r
1. In an internal combustion engine, a circular series of separate cylinders, end members at the ends of said cylinders, said cylinders and end members having water jackets formed therewith, means of communication between said jackets, a sleeve passed through the center of said series and through said end members, and means on said sleeve for binding said members to said cylinders.
2. An internal combustion engine comprising parallel cylinders, a shaft between said cylinders and parallel thereto, a pair of opposed pistons in each cylinder, a pair of swash disks on said shaft at the ends of said cylinders, a ring rotatably mounted on each, disk, connecting rods extending from said pistons and having universal connections with said ring, a sleeve surrounding said shaft between said disks and enga ed thereby, and means on said shaft engaging the outer sides of said disks and holding said shaft under initial tension.
3. An internal combustion engine comprising parallel cylinders, a shaft between said cylinders and parallel thereto, a pair of opposed pistons in each cylinder, a. pair of swash disks on said shaft at the ends of said cylinders,a ring rotatably mounted on each disk, connecting rods extending from said pistons and having universal connections with said ring, a sleeve surrounding aid shaft between said disks, and means binding said disks against the ends of said sleeve and holding said shaft under initial tension.
4. An internal combustion engine comprising parallel cylinders, a shaft between said cylinders and parallel thereto, a pair of opposed pistons in each cylinder, a pair of swash disks on said shaft at the ends of said cylinders, connecting rods extending from said pistons and joined to said disks, means for holding said disks in spaced relation, and means engaging said disks for holding said shaft tinder initial tension.
5. An internal combustion engine comprising parallel cylinders, a shaft between said cylinders and parallel thereto, a pair of opposed pistons in each cylinder, a pair of swash disks on said shaft at the ends of said cylinders, a ring rotatably mounted on each disk, connecting rods extending from said pistons and having universal connections with said ring, means for holding said disks in spaced relation, and means engaging said disks for holding said shaft under initial tension. I 6. An internal combustion engine comprising parallel cylinders, a shaft between said cylinders and parallel thereto, a pair of opposed pistons in each cylinder, a pair of swash disks on said shaft at the ends of said cylinders, connecting rods extending from said pistons and joined to said disks, a sleeve surrounding said shaft between said disks and engaged thereby, and means on said shaft engaging the outer sides of said disks and holding said shaft under initial tension. 7
-7. An internal combustion engine comprising parallel cylinders, a shaft between said cylinders and parallel thereto, a pair of opposed pistons in each cylinder, a pair of swash disks on said shaft at the ends of said-cylinders, connecting rods extending from said pistons and joined to said disks, a sleeve surrounding said shaft between said disks, and means binding said disks against the ends of said sleeve and holding said shaft under initial tension.
EDWARD GRAY.
US517876A 1931-02-24 1931-02-24 Internal combustion engine Expired - Lifetime US1978194A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US517876A US1978194A (en) 1931-02-24 1931-02-24 Internal combustion engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US517876A US1978194A (en) 1931-02-24 1931-02-24 Internal combustion engine

Publications (1)

Publication Number Publication Date
US1978194A true US1978194A (en) 1934-10-23

Family

ID=24061594

Family Applications (1)

Application Number Title Priority Date Filing Date
US517876A Expired - Lifetime US1978194A (en) 1931-02-24 1931-02-24 Internal combustion engine

Country Status (1)

Country Link
US (1) US1978194A (en)

Cited By (20)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2421868A (en) * 1943-04-23 1947-06-10 Ransom Y Bovee Barrel type engine
US2650676A (en) * 1948-04-22 1953-09-01 P R I M Sa Holding De Perfecti Lubrication of wobble plate internal-combustion engines
US2664866A (en) * 1943-12-27 1954-01-05 Frank L Fulke Internal-combustion engine
US3212483A (en) * 1963-04-23 1965-10-19 Vernon W Balzer Reciprocating machinery
US4216747A (en) * 1977-09-07 1980-08-12 Nippon Soken, Inc. Uniflow, double-opposed piston type two-cycle internal combustion engine
US4905637A (en) * 1985-04-12 1990-03-06 Edwin Ott Diesel aircraft engine--also convertible for other applications--optimized for high output, high supercharge and total energy utilization
US5273012A (en) * 1992-12-17 1993-12-28 Brock James E Swash plate engine with fixed torque reaction member
US6003480A (en) * 1995-11-20 1999-12-21 Q-Tre Pty Ltd Wobble plate engine
US6968751B2 (en) 2004-01-21 2005-11-29 Innovation Engineering, Inc. Axial piston machines
US20080302343A1 (en) * 2007-05-30 2008-12-11 High Density Powertrain, Inc. Super Charged Engine
US20080314688A1 (en) * 2004-06-10 2008-12-25 Achates Power, Inc. Internal combustion engine with provision for lubricating pistons
US20110194796A1 (en) * 2010-02-05 2011-08-11 Schaeffler Technologies Gmbh & Co. Kg Angled Bore Bearing
US20110271932A1 (en) * 2010-04-27 2011-11-10 Achates Power, Inc. Combustion chamber constructions for opposed-piston engines
US20120073541A1 (en) * 2010-08-16 2012-03-29 Achates Power, Inc. Fuel injection spray patterns for opposed-piston engines
US9211797B2 (en) 2013-11-07 2015-12-15 Achates Power, Inc. Combustion chamber construction with dual mixing regions for opposed-piston engines
US9309807B2 (en) 2011-05-18 2016-04-12 Achates Power, Inc. Combustion chamber constructions for opposed-piston engines
US9453459B2 (en) 2013-12-09 2016-09-27 Joachim Horsch Internal combustion engine
US9512779B2 (en) 2010-04-27 2016-12-06 Achates Power, Inc. Swirl-conserving combustion chamber construction for opposed-piston engines
US10180115B2 (en) 2010-04-27 2019-01-15 Achates Power, Inc. Piston crown bowls defining combustion chamber constructions in opposed-piston engines
US10865706B1 (en) * 2018-08-10 2020-12-15 Steven F Lowe Spherical linear two stroke engine

Cited By (25)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2421868A (en) * 1943-04-23 1947-06-10 Ransom Y Bovee Barrel type engine
US2664866A (en) * 1943-12-27 1954-01-05 Frank L Fulke Internal-combustion engine
US2650676A (en) * 1948-04-22 1953-09-01 P R I M Sa Holding De Perfecti Lubrication of wobble plate internal-combustion engines
US3212483A (en) * 1963-04-23 1965-10-19 Vernon W Balzer Reciprocating machinery
US4216747A (en) * 1977-09-07 1980-08-12 Nippon Soken, Inc. Uniflow, double-opposed piston type two-cycle internal combustion engine
US4905637A (en) * 1985-04-12 1990-03-06 Edwin Ott Diesel aircraft engine--also convertible for other applications--optimized for high output, high supercharge and total energy utilization
US5273012A (en) * 1992-12-17 1993-12-28 Brock James E Swash plate engine with fixed torque reaction member
US6003480A (en) * 1995-11-20 1999-12-21 Q-Tre Pty Ltd Wobble plate engine
US6968751B2 (en) 2004-01-21 2005-11-29 Innovation Engineering, Inc. Axial piston machines
US20080314688A1 (en) * 2004-06-10 2008-12-25 Achates Power, Inc. Internal combustion engine with provision for lubricating pistons
US8281755B2 (en) * 2004-06-10 2012-10-09 Achates Power, Inc. Internal combustion engine with provision for lubricating pistons
US20080302343A1 (en) * 2007-05-30 2008-12-11 High Density Powertrain, Inc. Super Charged Engine
US7823546B2 (en) * 2007-05-30 2010-11-02 High Density Powertrain, Inc. Super charged engine
US20110194796A1 (en) * 2010-02-05 2011-08-11 Schaeffler Technologies Gmbh & Co. Kg Angled Bore Bearing
US20110271932A1 (en) * 2010-04-27 2011-11-10 Achates Power, Inc. Combustion chamber constructions for opposed-piston engines
US8800528B2 (en) * 2010-04-27 2014-08-12 Achates Power, Inc. Combustion chamber constructions for opposed-piston engines
US9512779B2 (en) 2010-04-27 2016-12-06 Achates Power, Inc. Swirl-conserving combustion chamber construction for opposed-piston engines
US9593627B2 (en) 2010-04-27 2017-03-14 Achates Power, Inc. Combustion chamber constructions for opposed-piston engines
US10180115B2 (en) 2010-04-27 2019-01-15 Achates Power, Inc. Piston crown bowls defining combustion chamber constructions in opposed-piston engines
US20120073541A1 (en) * 2010-08-16 2012-03-29 Achates Power, Inc. Fuel injection spray patterns for opposed-piston engines
US8820294B2 (en) * 2010-08-16 2014-09-02 Achates Power, Inc. Fuel injection spray patterns for opposed-piston engines
US9309807B2 (en) 2011-05-18 2016-04-12 Achates Power, Inc. Combustion chamber constructions for opposed-piston engines
US9211797B2 (en) 2013-11-07 2015-12-15 Achates Power, Inc. Combustion chamber construction with dual mixing regions for opposed-piston engines
US9453459B2 (en) 2013-12-09 2016-09-27 Joachim Horsch Internal combustion engine
US10865706B1 (en) * 2018-08-10 2020-12-15 Steven F Lowe Spherical linear two stroke engine

Similar Documents

Publication Publication Date Title
US1978194A (en) Internal combustion engine
US8033265B2 (en) Rotary piston internal combustion engine
US4003351A (en) Rotary engine
CA2263332A1 (en) Improvements in axial piston rotary engines
US2287472A (en) Crankshaft and connecting rod connection
US1853563A (en) Internal combustion engine
US5765451A (en) Slipper bearing assembly for radial internal combustion engine
US5645027A (en) Orbiting piston combustion engine
US3874348A (en) Rotary internal combustion engine
US1980924A (en) Rotary gas engine
US1965548A (en) Internal combustion engine
US11428150B2 (en) System and method for rotational combustion engine
US3147638A (en) Crankshaft apparatus
US3599425A (en) Steam engines
US2935055A (en) Concentric valve internal combustion engine
US3492977A (en) Internal combustion engine
US1744157A (en) Internal-combustion engine
US2280645A (en) Internal combustion engine
US3242913A (en) Compression ignition engine
US2393542A (en) Two-cycle gas engine cylinder piston and valve mechanism
US2071125A (en) Internal combustion engine
US1280058A (en) Explosive-engine.
US1576837A (en) Internal-combustion engine
US1766385A (en) Internal-combustion engine
US1315847A (en) Rotary engine