US1830046A - Internal combustion engine - Google Patents

Internal combustion engine Download PDF

Info

Publication number
US1830046A
US1830046A US308937A US30893728A US1830046A US 1830046 A US1830046 A US 1830046A US 308937 A US308937 A US 308937A US 30893728 A US30893728 A US 30893728A US 1830046 A US1830046 A US 1830046A
Authority
US
United States
Prior art keywords
cylinders
shaft
cam
main shaft
pistons
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
US308937A
Inventor
White Frank
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.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Priority to US308937A priority Critical patent/US1830046A/en
Application granted granted Critical
Publication of US1830046A publication Critical patent/US1830046A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01BMACHINES OR ENGINES, IN GENERAL OR OF POSITIVE-DISPLACEMENT TYPE, e.g. STEAM ENGINES
    • F01B9/00Reciprocating-piston machines or engines characterised by connections between pistons and main shafts and not specific to preceding groups
    • F01B9/04Reciprocating-piston machines or engines characterised by connections between pistons and main shafts and not specific to preceding groups with rotary main shaft other than crankshaft
    • F01B9/06Reciprocating-piston machines or engines characterised by connections between pistons and main shafts and not specific to preceding groups with rotary main shaft other than crankshaft the piston motion being transmitted by curved surfaces
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B75/00Other engines
    • F02B75/16Engines characterised by number of cylinders, e.g. single-cylinder engines
    • F02B75/18Multi-cylinder engines
    • F02B75/22Multi-cylinder engines with cylinders in V, fan, or star arrangement
    • F02B75/222Multi-cylinder engines with cylinders in V, fan, or star arrangement with cylinders in star arrangement
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01BMACHINES OR ENGINES, IN GENERAL OR OF POSITIVE-DISPLACEMENT TYPE, e.g. STEAM ENGINES
    • F01B9/00Reciprocating-piston machines or engines characterised by connections between pistons and main shafts and not specific to preceding groups
    • F01B9/04Reciprocating-piston machines or engines characterised by connections between pistons and main shafts and not specific to preceding groups with rotary main shaft other than crankshaft
    • F01B9/06Reciprocating-piston machines or engines characterised by connections between pistons and main shafts and not specific to preceding groups with rotary main shaft other than crankshaft the piston motion being transmitted by curved surfaces
    • F01B2009/061Reciprocating-piston machines or engines characterised by connections between pistons and main shafts and not specific to preceding groups with rotary main shaft other than crankshaft the piston motion being transmitted by curved surfaces by cams
    • F01B2009/066Tri-lobe cams

Definitions

  • This invention relates mainly to internal combustion engines, and particularly to those of light weight, as, for example, airplane engines.
  • the necessity of the use of said train of gearing between the engine and the propeller-shaft is avoided, and the pistonsare connected to .the propeller-shaft in a way to cause reciprocating parts to be self-balancing.
  • several reciprocations of each piston are provided for during each single revolution of the shaft.
  • Figure 1 is a cross-sectional view of the engine taken transversely of the main shaft.
  • Figure 2 is a view of a cross-section extending longitudinally of the main shaft and through a group of diametrically opposite cylinders.
  • Figure 3 is a diagram illustrating an arrangement of valve-operating mechanism.
  • Figure 4 is a view illustrating the arrangement. of the valve-operating cams or camshafts.
  • Figure 5 is a wiring diagram for the ignition devices to illustrate the concurrent firing of three alternate cylinders.
  • Figure 6 is a detail view showing diametrically opposite pistons and details of means fixedly connecting and spacing said pistons for making their cam-followers adhere .to their respective cam-surfaces.
  • Figure 7 illustrates three cam-shafts along which the valve-operating cams may be distributed, and also shows the driving connections of said shafts to the main shaft.
  • the main shaft 15 of the engine is journaled in ends 16-17 of a casing 18, which encloses said shaft and has faces 19 for supporting in radial array around said shaft two groups A and B 'of cylinders 20, each cylinder having a piston 21-.
  • Each group has an even number of cylinders, namely, six 1 spaced degrees apart, and the cylinders of one group are spaced, lengthwise of the main shaft, from the cylinders of the other group as in Figure 2.
  • the pistons reciprocate in the usual fourstroke' cycle for driving the main shaft 15 to which they are operativelyconnected by novel cams 22-23 and connections, there being one cam for each cylinder group A and B.
  • Said cams maybe keyed to the splined main shaft as indicated, and one cam may abut a flange 25 of said shaft and be spaced from the other cam by a sleeve 26;
  • cams being thus located lengthwise of said shaft, so that each cam is in line with the central plane of its cylinder group A or B.
  • a nut 27 may secure the cams on said shaft.
  • Each cam has three lobes 28, all of the same contour, spaced 120 degrees apart and forming alternate rises and drops.
  • Cam-rollers 29 for the several pistons are directly mounted on the inner piston ends, and are preferably of roll or ball bearing type.
  • a transverse bolt 30 may connecteach two pistons that are in line lengthwise of the main shaft, and may serve as a common stud with journals for the rollers 29 of the pistons thus paired, said bolt passing through spacedapart ears 31 formed at the inner end of each piston and between which ears a roller 29 is retained.
  • Each cylinder has a detachable head 32 in which may be fitted poppet-valves 33 for opening and closing fuel intake and exhaust passages 34 and 35, respectively, formed in said head.
  • each piston is opposite another piston diametrically of the main shaft, and that .by reason of the odd number (three) of camlobes 28 the diametrically opposite istons always move in the same direction, an hence I may be positively and rigidly connected, the diametrically opposite cam rise and drop contours being to this end made complementary.
  • the space separating the cams 22-23 lengthwise of the main shaft affords room for such connections between the diametrically opposite pistons, and which connections, in the form of links 36, may be attached to the transverse bolts 30.
  • Each link 36 has an elongated loop 37 to clear the main shaft and its surrounding sleeve 26.
  • Eaehend of a link 36 has a hub 38 in which the bolt 30 is fitted.
  • the length of the link between hubs is such that, in conjunction with the complementary forms of the diametrically opposite cam-surfaces, the rollers 29 of each four pistons thus connected together are always kept in contact with their respective cam-surfaces.
  • Each group of said four pistons may have two links 36 spaced lengthwise of their respective hubs 38 for distributing the pull of the links symmetrically between the cams 22-23, the loops 37 of the several links for the different groups of four connected pistons extending in different planes to clear one another, as indicated by the dot-and-dash lines in Figure 2.
  • For the three groups of four connected pistons three pairs of links 36 are required, as indicated in Figure 1.
  • Each bolt 30 may have a head 82 and a nut 83 to abut the piston ears 31 and keep said bolt in place.
  • the complementary riseand-drop cam-contours are represented as corresponding substantially to uniformly accelerated and decelerated reciprocatory piston movement.
  • the cam-surface 1- between a top t and a bottom 6 of the cam represents a rise; and the surface d between a top t and bottom I) re resents a complementary and diametrical y opposite drop.
  • each piston makes six strokes or two strokes for each camlobe. With a cam having three lobes, each piston therefore completes its four-stroke cycle in two-thirds of a main shaft revolution.
  • three alternate pistons, 120 degrees apart, around said shaft operate concurrently on each stroke in either the A or B group of cylinders.
  • the several pistons with their respective cylinders are numbered from 1 to 6 in group A and from 7 to 12 in grou B, as indicated in Figure 1.
  • cylin ers 1-3-5 may fire concurrent- 1y, then cylinders 8-10-12, then cylinders 7-9-11, and then cylinders 246, the concurrence of the firing strokes being indicated by the ignition diagram in Figure 5.
  • the ignition diagram in Figure 5 which represents the electrodes e of ignition plugs 39 for the several cylinders of the two groups A and B, the plugs 39 of every three alternate cylinders being represented as having their undergrounded electrodes connected by a wire 40 for simultaneous sparking.
  • the diagram also represents the connections of the wires 40 to a distributor 41 and sparkgenerating source, such as a battery 42 and coil 43.
  • the plugs 39 are inserted in the cylinder-heads 32.
  • cams 44 for operating the poppetvalves 33 rotate at one and a half times the main shaft speed; that is to say, for twothirds of a main shaft revolution, the cams 44 make one revolution.
  • the valve-cams 44 are distributed along three cam-shafts 45 journaled in the ends 16-17 of the casing 18 and spaced around and from the main shaft 15 and between adjacent radial planes of cylinders, as indicated in Figures 1 and 7, so that each cam-shaft may serve four cylinders, that is, two cylinders in each group A and B.
  • Each cam-shaft 45 has fastened thereto a pinion 46, and the three cam-shafts are driven by a common gear 47 fastened to the main shaft and which gear 47 may be connected to each pinion 46, through an intermediate gear 48 which may rotate on a stud 49 carried by the casing end 17.
  • each cam-shaft 45 has spaced therealong eight of the cams 44, that is, one intake and one exhaust cam for each of the four cylinders which said each cam-shaft 45 serves.
  • the intake-cams for the alternate cylinders 1-3-5 are timespaced on their respective cam-shafts 45 to operate their intake-valves concurrently on the concurrent intake-strokes of said cylinders.
  • the exhaust-cams for said three cylinders 1-3-5 are also time-spaced to operate the exhaust-valves on the concurrent exhaust-strokes of said cylinders.
  • Each valve-cam 44 operates its valve through a tappet 53, and a push-rod 54 con- -necting said tappet to a valve-lever 55, rock able on a shaft 56 journaled between bearings 57, which may extend from op osite sides of the cyllnder-head 32, each sha t 56 carrying haust valves of said head 32, Figure 3.
  • the arms 58 of the four-valve levers for said cylinders 17 may be staggered in respect to the similar arms of the four-valve levers for said cylinders 2 and 8, the tappets of cylinders 1 and 7 bein thus interspaced with the tappets for cylinders 2 and 8 to present the eight ta pets in a line corresponding to the line of eight'cams it on the cam-shaft which serves said cylinders 1-7 and 2 -8.
  • the same arrangement is effected for the connections from 'the other cam-shafts to their respective cylinder-valves.
  • the tappets 53 may be guided in blocks 59 having tappet guides 60 and bein secured to the casing 18, Figure 1. Each va ve is closed as by a spring 61
  • the pistons are .of the slipper type, and may be adequately guided to the bottoms of their strokes by extending the cylinder-walls into the casing.
  • a portion 62 of each cylinder-wall may extend substantially to the inner end of the piston when it is at the bottom of its stroke and may be stepped back as at 63 to clear the tops of thecam-lobes 28 and then stepped back further as at 64 to clear the ends ofthe loops 37 of the links 36.
  • the portion 62 may be brought close to the adjacent side of the cam 22 or 23 as at 65, Figure 2.
  • the cylinder-wall-portion which is stepped back to 64 may have a notch 66 .for clearing the hub 38 of the link 36.
  • Roller bearings 67 ma be provided for the main shaft journals. f a screw-propeller be attached-to the main shaft, as at'68, a
  • thrust bearing 69 may be provided adjacent the bearing 67 and retained in the casing-end 16, as shown in Figure 2.
  • a nut 70 threaded on the end of the main shaft serves to transmit the thrust to the thrust bearin 69.
  • a removable cap 71 opposite the end 0 the main shaft in the casing-end 16 facilitates assembly of the parts enclosed in said casingend.
  • the casing-end 17 may also be removable to facilitate assembly.
  • One of the cam-shafts 45 may project through the casing-end 16, and may have a connection 72, Figure 2, to drive the ignition mechanism which includes the distributor 41, Figure 5. 1
  • An internal combustion engine including cylinders, a main shaft, twelve reciprocatory pistons operable in firing and preparatorystrokes toward and from said shaft, said pistons disposed in a radial array surrounding said shaft, means inclusive of evenly-spaced cam-lobes and operatively connecting said pistons and main shaft and effective for producing three firing strokes per piston for two main shaft revolutions, whereby the firing strokes in certain pistons on opposite sides of said shaft may take place concurrently, thereby to balance said strokes and minimize vibration, and means for controlling the intake, compression, explosion and inders.
  • a four-stroke cycle internal combustion engine having a main shaft, twelve radial cylinders surrounding said shaft, a piston in each cylinder, means operatively connecting the pistons and shaft whereby said pistons are reciprocated and said shaft rotated, fuel intake and exhaust valve mechanism, ignition mechanism, the twelve cylinders being arranged to prevent four groups of three cylinders each, said three spaced degrees apart around said shaft, said piston and shaft connecting means and the valve and ignition mechanisms being arranged to effect concurtheir strokes.

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Valve-Gear Or Valve Arrangements (AREA)

Description

. Nov. 3, 1931. F. WHITE 1,330,046
INTERNAL COMBUSTION ENGINE Filed Sept. 28, 1928 3 Sheets-Sheet l 3 Sheets-sh 2 In venfor:
F. WHITE INTERNAL COMBUSTION ENGINE Filed Sept. 28, 1928 Nov. 3, 1931.
Nov. 3, 1931. F. WHITE INTERNAL COMBUSTION ENGINE s Sheets-Sheet s In van for:
witifi MU I Filed Sept Artur I ll) Patented Nov. 3, 1931 PATENT OFFICE FRANK WHITE, 0! NEW YORK, N. Y.
INTERNAL COMBUSTION ENGINE Application filed September 2a, 1928. Serial No. 308,937.
This invention'relates mainly to internal combustion engines, and particularly to those of light weight, as, for example, airplane engines. V
It is a feature of the present invention to secure very high speed of the reciprocating pistons of the engine, thereby keeping down the size and weight of the engine, and economizing the fuel for the purpose stated, and moreover, to balance the reciprocating parts of the engine, so as to insure smooth running and also to ermit still higher rate of revolution while eeping the propeller-shaft rate down to its aforesaid low limits. The necessity of the use of said train of gearing between the engine and the propeller-shaft is avoided, and the pistonsare connected to .the propeller-shaft in a way to cause reciprocating parts to be self-balancing. Moreover several reciprocations of each piston are provided for during each single revolution of the shaft.
Other features and advantages will hereinafter appear.
In the accompanying drawings,
Figure 1 is a cross-sectional view of the engine taken transversely of the main shaft.
and through some of the cylinders.
Figure 2 is a view of a cross-section extending longitudinally of the main shaft and through a group of diametrically opposite cylinders. I
Figure 3 is a diagram illustrating an arrangement of valve-operating mechanism.
. Figure 4 is a view illustrating the arrangement. of the valve-operating cams or camshafts.
Figure 5 is a wiring diagram for the ignition devices to illustrate the concurrent firing of three alternate cylinders.
Figure 6 is a detail view showing diametrically opposite pistons and details of means fixedly connecting and spacing said pistons for making their cam-followers adhere .to their respective cam-surfaces.
Figure 7 illustrates three cam-shafts along which the valve-operating cams may be distributed, and also shows the driving connections of said shafts to the main shaft.
The main shaft 15 of the engine is journaled in ends 16-17 of a casing 18, which encloses said shaft and has faces 19 for supporting in radial array around said shaft two groups A and B 'of cylinders 20, each cylinder having a piston 21-. Each group has an even number of cylinders, namely, six 1 spaced degrees apart, and the cylinders of one group are spaced, lengthwise of the main shaft, from the cylinders of the other group as in Figure 2. v
The pistons reciprocate in the usual fourstroke' cycle for driving the main shaft 15 to which they are operativelyconnected by novel cams 22-23 and connections, there being one cam for each cylinder group A and B. Said cams maybe keyed to the splined main shaft as indicated, and one cam may abut a flange 25 of said shaft and be spaced from the other cam by a sleeve 26;
the cams being thus located lengthwise of said shaft, so that each cam is in line with the central plane of its cylinder group A or B. A nut 27 may secure the cams on said shaft.
Each cam has three lobes 28, all of the same contour, spaced 120 degrees apart and forming alternate rises and drops. Cam-rollers 29 for the several pistons are directly mounted on the inner piston ends, and are preferably of roll or ball bearing type. A transverse bolt 30 may connecteach two pistons that are in line lengthwise of the main shaft, and may serve as a common stud with journals for the rollers 29 of the pistons thus paired, said bolt passing through spacedapart ears 31 formed at the inner end of each piston and between which ears a roller 29 is retained. For the six radial planes of cylinders there are six bolts 30.
Each cylinder has a detachable head 32 in which may be fitted poppet-valves 33 for opening and closing fuel intake and exhaust passages 34 and 35, respectively, formed in said head.
From Figures 1 and 2, it will .be seen that each piston is opposite another piston diametrically of the main shaft, and that .by reason of the odd number (three) of camlobes 28 the diametrically opposite istons always move in the same direction, an hence I may be positively and rigidly connected, the diametrically opposite cam rise and drop contours being to this end made complementary. The space separating the cams 22-23 lengthwise of the main shaft affords room for such connections between the diametrically opposite pistons, and which connections, in the form of links 36, may be attached to the transverse bolts 30. Each link 36 has an elongated loop 37 to clear the main shaft and its surrounding sleeve 26. Eaehend of a link 36 has a hub 38 in which the bolt 30 is fitted. The length of the link between hubs is such that, in conjunction with the complementary forms of the diametrically opposite cam-surfaces, the rollers 29 of each four pistons thus connected together are always kept in contact with their respective cam-surfaces. Each group of said four pistons may have two links 36 spaced lengthwise of their respective hubs 38 for distributing the pull of the links symmetrically between the cams 22-23, the loops 37 of the several links for the different groups of four connected pistons extending in different planes to clear one another, as indicated by the dot-and-dash lines in Figure 2. For the three groups of four connected pistons three pairs of links 36 are required, as indicated in Figure 1. Each bolt 30 may have a head 82 and a nut 83 to abut the piston ears 31 and keep said bolt in place.
In the drawings, the complementary riseand-drop cam-contours are represented as corresponding substantially to uniformly accelerated and decelerated reciprocatory piston movement. Referring to Figure 6 and the direction of rotation indicated by the arrow, the cam-surface 1- between a top t and a bottom 6 of the cam represents a rise; and the surface d between a top t and bottom I) re resents a complementary and diametrical y opposite drop.
In each main shaft revolution, each piston makes six strokes or two strokes for each camlobe. With a cam having three lobes, each piston therefore completes its four-stroke cycle in two-thirds of a main shaft revolution. For balancing all the strokes of said cycle from opposite sides of the main shaft to minimize vibration, three alternate pistons, 120 degrees apart, around said shaft operate concurrently on each stroke in either the A or B group of cylinders. For explaining the cycle sequence, the several pistons with their respective cylinders are numbered from 1 to 6 in group A and from 7 to 12 in grou B, as indicated in Figure 1. Thus cylin ers 1-3-5 may fire concurrent- 1y, then cylinders 8-10-12, then cylinders 7-9-11, and then cylinders 246, the concurrence of the firing strokes being indicated by the ignition diagram in Figure 5. which represents the electrodes e of ignition plugs 39 for the several cylinders of the two groups A and B, the plugs 39 of every three alternate cylinders being represented as having their undergrounded electrodes connected by a wire 40 for simultaneous sparking. The diagram also represents the connections of the wires 40 to a distributor 41 and sparkgenerating source, such as a battery 42 and coil 43. The plugs 39 are inserted in the cylinder-heads 32.
Inasmuch as each piston completes its fourstroke cycle in two-thirds of a main shaft revolution, cams 44 for operating the poppetvalves 33 rotate at one and a half times the main shaft speed; that is to say, for twothirds of a main shaft revolution, the cams 44 make one revolution. The valve-cams 44 are distributed along three cam-shafts 45 journaled in the ends 16-17 of the casing 18 and spaced around and from the main shaft 15 and between adjacent radial planes of cylinders, as indicated in Figures 1 and 7, so that each cam-shaft may serve four cylinders, that is, two cylinders in each group A and B. Each cam-shaft 45 has fastened thereto a pinion 46, and the three cam-shafts are driven by a common gear 47 fastened to the main shaft and which gear 47 may be connected to each pinion 46, through an intermediate gear 48 which may rotate on a stud 49 carried by the casing end 17.
As indicated 1n Figure 4, each cam-shaft 45 has spaced therealong eight of the cams 44, that is, one intake and one exhaust cam for each of the four cylinders which said each cam-shaft 45 serves. The intake-cams for the alternate cylinders 1-3-5 are timespaced on their respective cam-shafts 45 to operate their intake-valves concurrently on the concurrent intake-strokes of said cylinders. Similarly, the exhaust-cams for said three cylinders 1-3-5 are also time-spaced to operate the exhaust-valves on the concurrent exhaust-strokes of said cylinders. In like manner are the intake-cams for each of the alternate-cylinder groups 8-10-12, 7-9-11 and 2-4-6 timed to operate their intake-valves concurrently for the intakestrokes of their respective groups, the exhaust-cams for each group 8-10-12, 7-9-11 and 2-46 being also timed for concurrence of their valve-operation. Figure 4 indicates by each cross-line 50, timing coincidence of three cams, one on each camshaft, for the intake and exhaust strokes cf the several alternate-cylinder groups 1-3-5, etc. For additional support each cam-shaft 45 may have a middle port-ion 51 journaled in a bearing 52 extended from the casing 18,- Figure 7.
Each valve-cam 44 operates its valve through a tappet 53, and a push-rod 54 con- -necting said tappet to a valve-lever 55, rock able on a shaft 56 journaled between bearings 57, which may extend from op osite sides of the cyllnder-head 32, each sha t 56 carrying haust valves of said head 32, Figure 3.
As shown in Figure 3, in which for convenience of illustration the cylinders 17 are assumed to be parallel to cylinders 28, the arms 58 of the four-valve levers for said cylinders 17 may be staggered in respect to the similar arms of the four-valve levers for said cylinders 2 and 8, the tappets of cylinders 1 and 7 bein thus interspaced with the tappets for cylinders 2 and 8 to present the eight ta pets in a line corresponding to the line of eight'cams it on the cam-shaft which serves said cylinders 1-7 and 2 -8. The same arrangement is effected for the connections from 'the other cam-shafts to their respective cylinder-valves. The tappets 53 may be guided in blocks 59 having tappet guides 60 and bein secured to the casing 18, Figure 1. Each va ve is closed as by a spring 61 The two groups of cylinders or pistons. A-B, twelve in all, afford four groups of three alternate pistons each, and the cycles of which four groups may be evenly phased as measured by angular displacement of the main shaft. Inasmuch as a cycle for each of said four groups is completed in twothirds of a main shaft revolution and the cycles for the several groups are evenly phased, it is evident that, for a whole main shaft revolution, cycles are evenly phased. Hence there are six evenly'phased' powerstrokes in each main shaft revolution; The adequate number, even phasing, and balancing of the power-stroke from opposite sides of the main shaft, as aforesaid, provide smooth power output and freedom from vibration, the latter being efi'ected not only in respect to the piston-masses and their connections without the use of special counter- Weights or similar devices, which of themselves contribute no power and reduce the efliciency of the engine and increase its weight, but also in respect to the firing forces, the compression forces, etc., of the fourstroke c cle. Y
The pistons are .of the slipper type, and may be adequately guided to the bottoms of their strokes by extending the cylinder-walls into the casing. To this end, a portion 62 of each cylinder-wall may extend substantially to the inner end of the piston when it is at the bottom of its stroke and may be stepped back as at 63 to clear the tops of thecam-lobes 28 and then stepped back further as at 64 to clear the ends ofthe loops 37 of the links 36. The portion 62 may be brought close to the adjacent side of the cam 22 or 23 as at 65, Figure 2. The cylinder-wall-portion which is stepped back to 64 may have a notch 66 .for clearing the hub 38 of the link 36.
Roller bearings 67 ma be provided for the main shaft journals. f a screw-propeller be attached-to the main shaft, as at'68, a
thrust bearing 69 may be provided adjacent the bearing 67 and retained in the casing-end 16, as shown in Figure 2. A nut 70 threaded on the end of the main shaft serves to transmit the thrust to the thrust bearin 69. A removable cap 71 opposite the end 0 the main shaft in the casing-end 16 facilitates assembly of the parts enclosed in said casingend. The casing-end 17 may also be removable to facilitate assembly.
One of the cam-shafts 45 may project through the casing-end 16, and may have a connection 72, Figure 2, to drive the ignition mechanism which includes the distributor 41, Figure 5. 1
Variations may be restorted to within the scope of the invention, and portions of the improvements may be used .without others.
Having thus described my invention, I claim:
1. An internal combustion engine including cylinders, a main shaft, twelve reciprocatory pistons operable in firing and preparatorystrokes toward and from said shaft, said pistons disposed in a radial array surrounding said shaft, means inclusive of evenly-spaced cam-lobes and operatively connecting said pistons and main shaft and effective for producing three firing strokes per piston for two main shaft revolutions, whereby the firing strokes in certain pistons on opposite sides of said shaft may take place concurrently, thereby to balance said strokes and minimize vibration, and means for controlling the intake, compression, explosion and inders. and pistons also spaced radially around said .shaft, the second bank being spaced lengthwise of the shaft from the first bank, means operatively connecting said pistons and shaft, and means whereby the cycles occurring in the two banks are phased at even intervals as measured by angular displacement of said shaft.
3. A four-stroke cycle internal combustion engine having a main shaft, twelve radial cylinders surrounding said shaft, a piston in each cylinder, means operatively connecting the pistons and shaft whereby said pistons are reciprocated and said shaft rotated, fuel intake and exhaust valve mechanism, ignition mechanism, the twelve cylinders being arranged to prevent four groups of three cylinders each, said three spaced degrees apart around said shaft, said piston and shaft connecting means and the valve and ignition mechanisms being arranged to effect concurtheir strokes.
FRANK WHITE.
US308937A 1928-09-28 1928-09-28 Internal combustion engine Expired - Lifetime US1830046A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US308937A US1830046A (en) 1928-09-28 1928-09-28 Internal combustion engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US308937A US1830046A (en) 1928-09-28 1928-09-28 Internal combustion engine

Publications (1)

Publication Number Publication Date
US1830046A true US1830046A (en) 1931-11-03

Family

ID=23195993

Family Applications (1)

Application Number Title Priority Date Filing Date
US308937A Expired - Lifetime US1830046A (en) 1928-09-28 1928-09-28 Internal combustion engine

Country Status (1)

Country Link
US (1) US1830046A (en)

Cited By (21)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2477061A (en) * 1943-05-11 1949-07-26 Orville E Irving Radial engine
US3584610A (en) * 1969-11-25 1971-06-15 Kilburn I Porter Internal combustion engine
DE2434804A1 (en) * 1974-07-19 1976-02-05 Ruapehu Pty Ltd Motor with first and secondary rotors - e.g. for combustion engine hydraulic motor, has second rotors mounted rotatable on first rotor vanes
DE2616370A1 (en) * 1975-04-16 1976-10-28 Victor W Farris ROTARY ROTARY PISTON COMBUSTION ENGINE
FR2599084A1 (en) * 1986-05-21 1987-11-27 Innovations Atel Const Internal combustion engine without connecting rods or crankshaft of the type having the cylinders in a star formation
US4848282A (en) * 1986-11-28 1989-07-18 Ateliers De Constructions Et D'innovations Combustion engine having no connecting rods or crankshaft, of the radial cylinder type
US5315967A (en) * 1993-04-16 1994-05-31 Harry Schoell Internal combustion rotary engine having a stacked arrangement of cylinders
WO1995018915A1 (en) * 1994-01-01 1995-07-13 Chen Fei Chang An engine with reciprocating coupling pistons and with one cam for each cylinder group
DE19547625A1 (en) * 1995-02-15 1996-08-22 Media Tech Vertriebs Gmbh Radial piston engine or machine
US5634441A (en) * 1996-01-16 1997-06-03 W. Parker Ragain Power transfer mechanism
US5839411A (en) * 1993-04-16 1998-11-24 Schoell; Harry Rotary fuel pump and combination fuel injector/spark plug
US20050217617A1 (en) * 2004-04-01 2005-10-06 Chaney Ray O Piston-cam engine
US20070068468A1 (en) * 2005-09-27 2007-03-29 Irick David K Rotary to reciprocal power transfer device
US7219631B1 (en) * 2003-02-24 2007-05-22 O'neill James Leo High torque, low velocity, internal combustion engine
US20070227345A1 (en) * 2004-04-29 2007-10-04 Francisco Javier Ruiz Martinez Balanced Rotary Engine
US20080127916A1 (en) * 2004-11-18 2008-06-05 S&S Cycle Inc. Vehicle and Propulsion System Including an Internal Combustion Engine
EP2066889A1 (en) * 2006-09-07 2009-06-10 Revetec Holdings Limited Improved opposed piston combustion engine
CN104105841A (en) * 2011-12-07 2014-10-15 马丁·罗伯特·舒特拉 Engine
WO2017014712A1 (en) * 2015-07-23 2017-01-26 Махаббад Мустафаевич ГУСЕЙНОВ Huseynli engine
RU2787435C1 (en) * 2022-08-05 2023-01-09 Василий Васильевич Благонравов Free piston internal combustion engine
US11725576B2 (en) * 2016-05-16 2023-08-15 Frank J. Ardezzone Internal combustion engine with adaptable piston stroke

Cited By (38)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2477061A (en) * 1943-05-11 1949-07-26 Orville E Irving Radial engine
US3584610A (en) * 1969-11-25 1971-06-15 Kilburn I Porter Internal combustion engine
DE2434804A1 (en) * 1974-07-19 1976-02-05 Ruapehu Pty Ltd Motor with first and secondary rotors - e.g. for combustion engine hydraulic motor, has second rotors mounted rotatable on first rotor vanes
DE2616370A1 (en) * 1975-04-16 1976-10-28 Victor W Farris ROTARY ROTARY PISTON COMBUSTION ENGINE
US4038949A (en) * 1975-04-16 1977-08-02 Farris Victor W Rotary-radial internal combustion engine
FR2599084A1 (en) * 1986-05-21 1987-11-27 Innovations Atel Const Internal combustion engine without connecting rods or crankshaft of the type having the cylinders in a star formation
US4848282A (en) * 1986-11-28 1989-07-18 Ateliers De Constructions Et D'innovations Combustion engine having no connecting rods or crankshaft, of the radial cylinder type
US5839411A (en) * 1993-04-16 1998-11-24 Schoell; Harry Rotary fuel pump and combination fuel injector/spark plug
US5315967A (en) * 1993-04-16 1994-05-31 Harry Schoell Internal combustion rotary engine having a stacked arrangement of cylinders
WO1995018915A1 (en) * 1994-01-01 1995-07-13 Chen Fei Chang An engine with reciprocating coupling pistons and with one cam for each cylinder group
US5836234A (en) * 1994-01-01 1998-11-17 Chen; Feichang Single CAM reciprocating linked piston type engine
DE19547625A1 (en) * 1995-02-15 1996-08-22 Media Tech Vertriebs Gmbh Radial piston engine or machine
US5634441A (en) * 1996-01-16 1997-06-03 W. Parker Ragain Power transfer mechanism
US7219631B1 (en) * 2003-02-24 2007-05-22 O'neill James Leo High torque, low velocity, internal combustion engine
US20050217617A1 (en) * 2004-04-01 2005-10-06 Chaney Ray O Piston-cam engine
US7017534B2 (en) 2004-04-01 2006-03-28 Chaney Ray O Piston-cam engine
US20070227345A1 (en) * 2004-04-29 2007-10-04 Francisco Javier Ruiz Martinez Balanced Rotary Engine
US20080127916A1 (en) * 2004-11-18 2008-06-05 S&S Cycle Inc. Vehicle and Propulsion System Including an Internal Combustion Engine
US8511273B2 (en) 2004-11-18 2013-08-20 S & S Cycle, Inc. Cylinder head of an internal combustion engine
US8919321B2 (en) 2004-11-18 2014-12-30 S & S Cycle, Inc. Internal combustion engine with lubrication system
US20090241869A1 (en) * 2004-11-18 2009-10-01 Burgess Geoffrey W Vehicle and propulsion system including an internal combustion engine
US8726869B2 (en) 2004-11-18 2014-05-20 S & S Cycle, Inc. Internal combustion engine with plate-mounted cam drive system
US7703423B2 (en) 2004-11-18 2010-04-27 S & S Cycle, Inc. Vehicle and propulsion system including an internal combustion engine
US8011333B2 (en) 2004-11-18 2011-09-06 S & S Cycle, Inc. Vehicle and propulsion system including an internal combustion engine
US7475627B2 (en) 2005-09-27 2009-01-13 Ragain Air Compressors, Inc. Rotary to reciprocal power transfer device
US20070068468A1 (en) * 2005-09-27 2007-03-29 Irick David K Rotary to reciprocal power transfer device
JP2010502877A (en) * 2006-09-07 2010-01-28 レヴェテック ホールディングス リミテッド Improved opposed piston combustion engine
AU2007294489B2 (en) * 2006-09-07 2013-03-14 Revetec Holdings Limited Improved opposed piston combustion engine
US8245673B2 (en) * 2006-09-07 2012-08-21 Revetec Holdings Limited Opposed piston combustion engine
US20090314232A1 (en) * 2006-09-07 2009-12-24 Bradley Howell-Smith Opposed piston combustion engine
EP2066889A1 (en) * 2006-09-07 2009-06-10 Revetec Holdings Limited Improved opposed piston combustion engine
EP2066889B1 (en) * 2006-09-07 2017-08-02 Revetec Holdings Limited Improved opposed piston combustion engine
CN104105841A (en) * 2011-12-07 2014-10-15 马丁·罗伯特·舒特拉 Engine
US20140318483A1 (en) * 2011-12-07 2014-10-30 Martin Robert Shutlar Engine
EP2815073A4 (en) * 2011-12-07 2015-09-30 Martin Robert Shutlar An engine
WO2017014712A1 (en) * 2015-07-23 2017-01-26 Махаббад Мустафаевич ГУСЕЙНОВ Huseynli engine
US11725576B2 (en) * 2016-05-16 2023-08-15 Frank J. Ardezzone Internal combustion engine with adaptable piston stroke
RU2787435C1 (en) * 2022-08-05 2023-01-09 Василий Васильевич Благонравов Free piston internal combustion engine

Similar Documents

Publication Publication Date Title
US1830046A (en) Internal combustion engine
US2169236A (en) Internal combustion engine
US1580249A (en) Internal-combustion engine
US2163052A (en) Explosive engine
US1764147A (en) Internal-combustion engine
US2303025A (en) Internal combustion engine
US2675791A (en) Internal-combustion engine
US1893045A (en) Internal combustion engine
US1722950A (en) Internal-combustion engine
US1802881A (en) Internal-combustion engine
US2852837A (en) Internal combustion engines and methods of manufacturing such engines
US1716621A (en) Rotary internal-combttstiolir engine
US1639333A (en) Explosive engine
US1835138A (en) Internal-combustion engine
US1283375A (en) Engine.
USRE15019E (en) Internal-combustion engine
US1688610A (en) Internal-combustion engine
US1711882A (en) Internal-combustion engine
US1776760A (en) Internal-combustion engine
US2398864A (en) Internal-combustion engine
US1816406A (en) Aeroplane engine
US2332056A (en) Engine
US1690144A (en) Internal-combustion engine
US3384058A (en) Overhead camshaft engine
US1366636A (en) Internal-combustion engine