US3882827A - Four-phase cycle planetating piston internal combustion engine - Google Patents
Four-phase cycle planetating piston internal combustion engine Download PDFInfo
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- US3882827A US3882827A US450290A US45029074A US3882827A US 3882827 A US3882827 A US 3882827A US 450290 A US450290 A US 450290A US 45029074 A US45029074 A US 45029074A US 3882827 A US3882827 A US 3882827A
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- 238000002485 combustion reaction Methods 0.000 title claims abstract description 23
- 238000000819 phase cycle Methods 0.000 title claims description 6
- 239000000446 fuel Substances 0.000 claims abstract description 77
- 238000007789 sealing Methods 0.000 claims abstract description 32
- 238000007906 compression Methods 0.000 claims abstract description 20
- 230000006835 compression Effects 0.000 claims abstract description 17
- 238000010892 electric spark Methods 0.000 abstract description 2
- 238000000926 separation method Methods 0.000 abstract description 2
- 239000007789 gas Substances 0.000 description 3
- 230000000694 effects Effects 0.000 description 2
- 239000003344 environmental pollutant Substances 0.000 description 2
- 230000002093 peripheral effect Effects 0.000 description 2
- 231100000719 pollutant Toxicity 0.000 description 2
- 101100400378 Mus musculus Marveld2 gene Proteins 0.000 description 1
- 241000220317 Rosa Species 0.000 description 1
- 230000006978 adaptation Effects 0.000 description 1
- 239000003795 chemical substances by application Substances 0.000 description 1
- 230000002860 competitive effect Effects 0.000 description 1
- 230000003628 erosive effect Effects 0.000 description 1
- 239000007858 starting material Substances 0.000 description 1
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Classifications
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01C—ROTARY-PISTON OR OSCILLATING-PISTON MACHINES OR ENGINES
- F01C1/00—Rotary-piston machines or engines
- F01C1/30—Rotary-piston machines or engines having the characteristics covered by two or more groups F01C1/02, F01C1/08, F01C1/22, F01C1/24 or having the characteristics covered by one of these groups together with some other type of movement between co-operating members
- F01C1/32—Rotary-piston machines or engines having the characteristics covered by two or more groups F01C1/02, F01C1/08, F01C1/22, F01C1/24 or having the characteristics covered by one of these groups together with some other type of movement between co-operating members having both the movement defined in group F01C1/02 and relative reciprocation between the co-operating members
- F01C1/324—Rotary-piston machines or engines having the characteristics covered by two or more groups F01C1/02, F01C1/08, F01C1/22, F01C1/24 or having the characteristics covered by one of these groups together with some other type of movement between co-operating members having both the movement defined in group F01C1/02 and relative reciprocation between the co-operating members with vanes hinged to the inner member and reciprocating with respect to the outer member
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- 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
- F02B53/00—Internal-combustion aspects of rotary-piston or oscillating-piston engines
- F02B2053/005—Wankel engines
-
- 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
- F02B75/02—Engines characterised by their cycles, e.g. six-stroke
- F02B2075/022—Engines characterised by their cycles, e.g. six-stroke having less than six strokes per cycle
- F02B2075/027—Engines characterised by their cycles, e.g. six-stroke having less than six strokes per cycle four
Definitions
- the piston is tethered by suitable means located at 12 [57] ABSTRACT oclock which restrains rotation of said piston and A cylindrical piston eccentrically planetates within a cylindrical bore formed in the stator to generate with each cycle, on one side of the piston, proceeding clockwise from 6 oclock to 12 oclock, expanding fuel vapor suction and contracting fuel vapor comconfines its movement to planetation thereof as aforesaid.
- Wankel engine suffers competitively when compared with other engines on the basis of gasoline mileage. mileage run between overhauls and particularly. the miles it will run efficiently before replacement of the engine seals becomes necessary.
- the present invention is particularly superior to other modern automotive engines in the very low rate of seal wear and erosion experienced in the operation of this engine by virtue of the great reduction in friction between the stator bore and the cylindrical piston of this engine over the friction produced in reciprocating engines or in the Wankel engine.
- the wear factor in the present invention is thus only a very small fraction of that experienced in modern competitive internal combustion engines.
- FIG. 1 is a diagrammatic fragmentary cross sectional view of a preferred embodiment of the invention showing the piston at its 12 oclock position (dead center).
- FIG. 2 is a view similar to FIG. 1 showing the piston of the invention advanced to its 1:20 oclock position.
- FIG. 3 is a view similar to FIG. 2 showing the piston of the invention advanced to its 4:30 oclock position.
- FIG. 4 is a view similar to FIG. 3 showing the piston of the invention advanced to its 6:30 oclock position.
- FIG. is a view similar to FIG. 4 showing the piston advanced to its 10:30 oclock position.
- FIG. 1 illustrates the preferred embodiment of the present invention which comprises an internal combustion engine 10 which includes a stator ll having a cylindrical bore 12 and an annular cylindrical piston 13 which is mounted for non-rotating planetation within said bore to maintain a constant sealing relation between said piston and said bore and thus performs with each complete power cycle of the engine the four strokes required in any four cycle engine, to wit: a suction stroke; a fuel compression stroke; a combustion stroke; and an exhaust stroke.
- a stator ll having a cylindrical bore 12 and an annular cylindrical piston 13 which is mounted for non-rotating planetation within said bore to maintain a constant sealing relation between said piston and said bore and thus performs with each complete power cycle of the engine the four strokes required in any four cycle engine, to wit: a suction stroke; a fuel compression stroke; a combustion stroke; and an exhaust stroke.
- the hours of the clock will be used to indicate the point within said bore at which said piston makes tangential sealing engagement therewith at any particular moment during a cycle of the engine.
- the bore I2 is closed by parallel end plates 14 which support bearings concentric with said bore in which a shaft 15 journals on which an eccentric hub 16 is fixed.
- Fitting over the hub I6 is an anti-friction bearing 17 which slideably tits within said annular piston [3, the outside diameter of the piston I3 being such that when so mounted on the shaft 15, the peripheral surface of the piston I3 is always approximately in internal tangential contact with the bore 12 at a point disposed directly opposite the high point 18 of the eccentric hub 16.
- the stator II and piston 13 are associated together through a tethering means 19 which restricts the rotational movement of the piston 13 to a planetating motion of the piston within the bore 12.
- This means also constitutes an abuttment which seals the space between the bore 12 and the piston 13 at 12 o'clock.
- the tethering means 19 includes a flat radial slot 20 formed upwardly from the bore 12 in the stator 11 to slideably accommodate therein an abutment plunger 25.
- This plunger has integrally formed thereon along its lower edge a cylindrical head 26 which slides endwise into a correspondingly shaped recess 27 provided in the periphery of the piston 13 to form a pivotal sealing connection between the plunger 25 and said piston.
- a compressed fuel passage 28 is formed transversely in the plunger 25, this passage being controlled by a slide valve 29 which is slideably mounted in a central slot 30 formed in the plunger 25.
- the slot 20 and abutment plunger 25 are co-extensive in length with the piston 13 and both said piston and plunger make a sealing engagement with the end plates 14.
- stator 11 is provided with a radial slot 31 for slideably receiving a seal vane 32 which is spring biased inwardly from said slot so as to be held constantly in sealing engagement with the peripheral surface of the piston 13.
- the stator 11 is provided with an exhaust port 33 which opens into the bore 12 just in advance of the seal vane 32.
- the stator 11 is also provided with a fuel vapor intake port 34 which opens into bore 12 just beyond seal vane 32 at approximately 6:30 oclock. said port being fitted with a counterbalanced check valve 35 which opens to admit vaporized fuel into said bore in response to a suction produced in the latter and closes to prevent a backflow of said vapor into the port 34 when said suction terminates at the end of the suction stroke of the engine.
- the stator I1 is also provided with a slot 40 coextensive in length with the bore 12 and extending radially outwardly therefrom approximately at l:20 oclock.
- a valve vane 41 Slideably received in said slot is a valve vane 41 which is spring biased normally into sealing relation with the exterior surface of piston I3 but is subject to being cam retracted into open position as shown in hole 45 is provided by the stator 11 through which a spark plug 46 may be inserted into said ignition subchamber for ignition of a fuel charge confined therein.
- the engine is provided with a conventional elec tric magneto and timer (not shown) driven by shaft and connected to the spark plug 46 so as to energize said plug in proper timed relation with rotation of the shaft 15 for igniting a fuel charge contained in ignition sub-chamber 44 in the generating of a power stroke in the engine 10.
- the slide valve 29 and valve vane 41 lo cated respectively at 12 oclock and 1:20 oclock on opposite sides of the ignition sub-chamber 44 are both spring biased radially inwardly into closed position and are correlatively opened respectively by earns 47 and 48 fixed on shaft 15 and connected to said slide valve and valve vane by cam follower rollers 49 and 50.
- seals 56 are T-head in cross section and thus limited in the distance they are free to extend radially from the periphery of said piston.
- the function of seals 56 is to maintain the periphery of the piston in snug sealing contact with the bore 12 so as to substantially prevent leakage between the bore 12 and portions of the periphery of the piston 12 closely juxtaposed in relation to said bore wherever the high point 18 of eccentric hub 16 is disposed at its closest spacing with said stator bore.
- one of the seals 56 is located just clockwise beyond the valve vane 41 when said vane opens as shown in FIG. 2 and remains in sealing engagement with said stator bore until the next successive seal 56 (in a clockwise direction therefrom) comes into sealing relation with said bore as shown in FIG. 3.
- Seals (not shown) provided in the ends of piston 13 maintain sealing contact with the end plates 14.
- the engine 10 must be furnished with a carburetor or other source for vaporized fuel in order for it to operate and this is connected to the fuel inlet port 34.
- the engine 10 requires a self starter which is connected to the shaft 15 so as to turn this over in order to start the engine operating. Two or 3 revolutions of this shaft should always be sufficient to start the engine. A complete cycle of the engine 10 is performed with each revolution of shaft 15.
- FIG. 1 shows the engine at dead center with the high point 18 of the hub 16 being located at 12 oclock.
- the piston 13 is now located in upward tangential contact with the stator bore 12.
- the slide valve 29 at 12 oclock has just been closed shutting off the compressed fuel passage 28, and the valve vane 41 at 1:20 oclock, which has been closed and in sealing engagement with the piston 13 for approximately 180, is about to be opened by cam 48.
- FIG. 1 shows the engine in the middle of a fuel suction stroke which is shown as having been completed in FIG. 3.
- the fuel compression stroke starts with the piston high point 18 at 3 oclock and concludes with the piston at dead center as shown in FIG. 1.
- FIG. 1 shows the engine at dead center with the high point 18 of the hub 16 being located at 12 oclock.
- the piston 13 is now located in upward tangential contact with the stator bore 12.
- the slide valve 29 at 12 oclock has just been closed shutting off the compressed fuel passage 28, and the valve vane 41 at 1:20 oclock
- valve vane 41 is allowed to be spring closed by cam 48 while the slide valve 29 is positively cam opened by cam 47 at approximately 6:30 o'clock as shown in FIG. 4.
- the ignition sub chamber 44 is thus closed off from the space CE (combustion exhaust chamber) as shown in FIG. 4 just as this space comes into communication with the exhaust port 33 and starts to contract, thereby expelling exhaust gases from said chamber through said exhaust port.
- the fuel vapor sucked into chamber SC is compressed and expelled from said chamber through compressed fuel passage 28 and into the ignition subchamber 44. It will readily be seen by comparing FIG. 4 and FIG. 1, that during this interval.
- the compressed fuel thus delivered to sub-chamber 44 is further compressed between the walls of said subchamber which include the stator bore 12, the periphery of piston 13, the abutment plunger 25 and the valve vane 41.
- the slide valve 29 is cam closed at approximately 12 oclock to confine in the ignition sub-chamber 44 the compressed fuel charge delivered thereto, the slide valve 29 remaining thus closed until the conclusion of the power stroke to be effected by the ignition of said charge.
- the cam 48 functions to open the valve vane 41 so that this is withdrawn radially from engagement with the periphery of the piston 13 as shown in FIG. 2.
- Seal 56a is now already in sealing engagement with the bore 12 at a location close to and on the clockwise side of valve vane 41 as shown in FIG. 2.
- the high point 18 of eccentric hub 16 is about on a radius with the center of combustion chamber 44.
- the engine 10 is preferably provided with a series of glow plugs or pods 57 which are countersunk in the bore 13 between the valve vane 41 and the exhaust port 33. These plugs are heated by a short running of the engine to an incandescent temperature. While the engine continues to run therefore, the plugs 57 improve combustion and continue to ignite and burn combustible pollutants remaining mixed with the combustion products after the exhaust port opens.
- While the engine of the invention is described as preferably having seal vane 32 located at 6 o'clock and exhaust port 33 located at 5:30 oclock and valve 35 located at 6:30 oclock. these three elements may as a group be located as much as or more clockwise or counterclockwise from their preferred positions aforesaid. The purpose of such a counter clockwise shift in located would be to shorten the power stroke of the engine and lengthen the suction-compression stroke thereof, and thus invest the engine with a higher compression ratio. A similar clockwise shift would. of course, accomplish the opposite effect.
- Engine 10 although disclosed as preferably operat ing on vaporized fuel inhaled from a carburetor. is also readily adaptable to be operated as a diesel type engine in which case the air fuel component would be inhaled through valve from the atmosphere and compressed and delivered into sub chamber 44 and the combustible fuel component would be injected directly into the ignition sub chamber 44 by a timed device of the type commonly employed in diesel engine practice.
- the engine 10 is an adaptation to internal combustion engine practice of the well known Kinney tethered planetating piston pump and that this engine is adapted to employ any of the various types of piston tethering means proven successful in the design of said pumps.
- stator having a cylindrical bore closed by end walls providing a pair of bearings co-axial with said bore;
- first, second and third abutment means radially biased respectively at about 12 o'clock, 1:20 oclock and 6 oclock to seal off the free space between said piston and bore at said respective circumferentially spaced points to produce a fuel vapor suction and compression chamber extending clockwise from 6 to 12 oclock, a fuel vapor expansion and exhaust chamber extending clockwise from 12 to 6 oclock, and a fuel charge confinement and ignition sub-chamber extending clockwise between 12 and 1:20 oclock;
- stator means in said stator providing a fuel inlet port for admitting gaseous fuel into said suction and compression chamber when the latter is in its suction phase;
- first cam controlled passage means delivering compressed gaseous fuel directly from said suctioncompression chamber to said ignition subchamber, and then shutting said passage means;
- tethering means connected peripherally to said piston to limit the rotation of said piston relative to said stator to a planetating movement in said bore.
- stator is provided with a slot extending radially from said bore at 12 oclock;
- said first cam controlled passage means being embodied in said first abutment means and delivering a compressed fuel charge directly therethrough into said ignition sub-chamber.
- stator and piston elements are hollowed out in the area of said ignition sub-chamber to provide the compression ratio designed for the engine, and wherein slots ex end radially from the stator bore at 1:20 and at 6 o'clock to slideably receive the second and third abutments which are spring biased from said slots into sealing relation with said piston.
- stator having a cylindrical bore closed by end walls providing a pair of bearings co-axial with said bore;
- a seal vane radially slideable in said last recited slot and spring biased constantly into sealing relation with the periphery of said piston, said piston plunger and seal vane dividing the vacant space in said stator into a fuel vapor suction and compression chamber extending clockwise from said vane to said plunger, and a combustion and exhaust chamber extending clockwise from said plunger to said vane;
- stator means in said stator providing a fuel inlet port for delivering carbureted fuel vapor into said bore at about 6:30 oclock;
- valve vane radially slideably extensible from said last recited slot into sealing relation with said piston
- stator and piston elements being hollowed out in the area where they tangentially meet between 12 o'clock and 1:20 oclock to provide an ignition sub-chamber which during a power stroke of said engine, comprises an upper portion of said combustion-exhaust chamber;
- cam means coordinately actuating said valve vane and compressed fuel valve to close said valve vane while a compressed fuel charge is being delivered through said passage into said ignition subchamber, to close said compressed fuel valve at the conclusion of said delivery, to open said valve vane upon the ignition of said fuel charge, to produce a power stroke, to reclose said valve vane at the conclusion of said power stroke and then reopen said compressed fuel valve to admit another compressed fuel charge through said passage into said ignition sub-chamber.
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Abstract
A cylindrical piston eccentrically planetates within a cylindrical bore formed in the stator to generate with each cycle, on one side of the piston, proceeding clockwise from 6 o''clock to 12 o''clock, expanding fuel vapor suction and contracting fuel vapor compression strokes and, on the opposite side of the piston, proceeding from 12 o''clock to 6 o''clock, expanding combustion and contracting exhaust strokes. A shaft journaled concentrically on said stator has fixed thereto an eccentric on which the piston is concentrically mounted. A traveling tangential sealing engagement is maintained between the piston and stator bore to progressively generate said strokes. The fuel vapor inhaled and then compressed on said suction and compression strokes is delivered at 12 o''clock at the moment of maximum compression directly into an ignition sub chamber located between 12 o''clock and 1:20 o''clock, and is forthwith ignited by an electric spark. Controlled separation of the free spaces on opposite sides of the piston within the stator bore is effected in the vertical diametral plane of said bore by radially reciprocable vanes and confinement of the fuel charge in the ignition sub chamber pending the ignition of said charge employs separate cam operated radial valves located respectively at 12 o''clock and 1:20 o''clock. The exhaust stroke terminates at an exhaust port provided in the stator at approximately 5:30 o''clock and fuel vapors are fed to the engine through an inlet port located in the stator at approximately 6:30 o''clock. The piston is tethered by suitable means located at 12 o''clock which restrains rotation of said piston and confines its movement to planetation thereof as aforesaid.
Description
[ 1 May 13, 1975 United States Patent 1 Williams FOUR-PHASE CYCLE PLANETATING pression strokes and, on the opposite side of the piston, proceeding from 12 oclock to 6 oclock, expanding combustion and contracting exhaust strokes. A
PISTON INTERNAL COMBUSTION ENGINE [76] Inventor: Robert H. Williams, Rt. 2, Bandera,
Tex. 78003 shaft journaled concentrically on said stator has fixed thereto an eccentric on which the piston is concentrically mounted. A traveling tangential sealing engage- [22] Filed: Mar. 12, 1974 [21] App]. No.: 450,290
ment is maintained between the piston and stator bore to progressively generate said strokes. The fuel vapor inhaled and then compressed on said suction and com- [52] US. 123/817; 418/67 pression strokes is delivered at 12 o'clock at the mo- [51] F02b 53/00 Int. ment of maximum compression directly into an igni- Field of Search tion sub chamber located between 12 oclock and 418/67 1:20 oclock, and is forthwith ignited by an electric spark. Controlled separation of the free spaces on op- References Cited posite sides of the piston within the stator bore is ef- UNITED STATES PATENTS fected in the vertical diametral plane of said bore by 244 673 Rose 418/65 radially reciprocable vanes and confinement of the 2 344159 3/1944 Meek Q33:I::IIIIIIIIIIQT8/67 X fuel charge in the ignition Sub Chamber Pending the FOREIGN PATENTS OR APPLICATIONS ignition of said charge employs separate cam operated radial valves located respectively at 12 oclock and 300,194 9/1965 Netherlands....................... 123/827 1:20 oclock, The exhaust stroke terminates at an exhaust port provided in the stator at approximately Primary Examiner-C. J. HuSar 5:30 oclock and fuel vapors are fed to the engine Assistant Examiner-Michael KOCZO, Jr. through an inlet port located in the stator at approximately 6:30 oclock.
Attorney, Agent, or Firm-Dana E. Keech The piston is tethered by suitable means located at 12 [57] ABSTRACT oclock which restrains rotation of said piston and A cylindrical piston eccentrically planetates within a cylindrical bore formed in the stator to generate with each cycle, on one side of the piston, proceeding clockwise from 6 oclock to 12 oclock, expanding fuel vapor suction and contracting fuel vapor comconfines its movement to planetation thereof as aforesaid.
6 Claims, 5 Drawing Figures PATENTEU MAY 1 31975 SHEET 2 OF I FOlR-IHASIC CYCLE ILANICTA'IING PISTON INTERNAL COMBUSTION ENGINE SUMMARY OF THE INVENTION One of the most advanced of the internal combustion engines in general use in automotive vehicles is known as the Wankel rotary engine. It is an object ofthe present invention to provide an engine which can successfully compete with if not supercede the Wankel engine by outperforming it.
For one thing. the Wankel engine suffers competitively when compared with other engines on the basis of gasoline mileage. mileage run between overhauls and particularly. the miles it will run efficiently before replacement of the engine seals becomes necessary.
It is an object of the present invention to provide an internal combustion engine capable of favorably competing with the Wankel engine to its performance in all of the respects above mentioned. The present invention is particularly superior to other modern automotive engines in the very low rate of seal wear and erosion experienced in the operation of this engine by virtue of the great reduction in friction between the stator bore and the cylindrical piston of this engine over the friction produced in reciprocating engines or in the Wankel engine. The wear factor in the present invention is thus only a very small fraction of that experienced in modern competitive internal combustion engines.
BRIEF DESCRIPTION OF THE DRAWINGS FIG. 1 is a diagrammatic fragmentary cross sectional view of a preferred embodiment of the invention showing the piston at its 12 oclock position (dead center).
FIG. 2 is a view similar to FIG. 1 showing the piston of the invention advanced to its 1:20 oclock position.
FIG. 3 is a view similar to FIG. 2 showing the piston of the invention advanced to its 4:30 oclock position.
FIG. 4 is a view similar to FIG. 3 showing the piston of the invention advanced to its 6:30 oclock position.
FIG. is a view similar to FIG. 4 showing the piston advanced to its 10:30 oclock position.
DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENT The drawings illustrate the preferred embodiment of the present invention which comprises an internal combustion engine 10 which includes a stator ll having a cylindrical bore 12 and an annular cylindrical piston 13 which is mounted for non-rotating planetation within said bore to maintain a constant sealing relation between said piston and said bore and thus performs with each complete power cycle of the engine the four strokes required in any four cycle engine, to wit: a suction stroke; a fuel compression stroke; a combustion stroke; and an exhaust stroke.
For convenience in describing the engine 10 and its operation, the hours of the clock will be used to indicate the point within said bore at which said piston makes tangential sealing engagement therewith at any particular moment during a cycle of the engine.
The bore I2 is closed by parallel end plates 14 which support bearings concentric with said bore in which a shaft 15 journals on which an eccentric hub 16 is fixed. Fitting over the hub I6 is an anti-friction bearing 17 which slideably tits within said annular piston [3, the outside diameter of the piston I3 being such that when so mounted on the shaft 15, the peripheral surface of the piston I3 is always approximately in internal tangential contact with the bore 12 at a point disposed directly opposite the high point 18 of the eccentric hub 16.
The stator II and piston 13 are associated together through a tethering means 19 which restricts the rotational movement of the piston 13 to a planetating motion of the piston within the bore 12. This means also constitutes an abuttment which seals the space between the bore 12 and the piston 13 at 12 o'clock. provides a passage for compressed fuel vapor horizontally through said tethering means and includes a cam con trolled valve for closing and opening said passage as required in the operation of the engine. The tethering means 19 includes a flat radial slot 20 formed upwardly from the bore 12 in the stator 11 to slideably accommodate therein an abutment plunger 25. This plunger has integrally formed thereon along its lower edge a cylindrical head 26 which slides endwise into a correspondingly shaped recess 27 provided in the periphery of the piston 13 to form a pivotal sealing connection between the plunger 25 and said piston. A compressed fuel passage 28 is formed transversely in the plunger 25, this passage being controlled by a slide valve 29 which is slideably mounted in a central slot 30 formed in the plunger 25. The slot 20 and abutment plunger 25 are co-extensive in length with the piston 13 and both said piston and plunger make a sealing engagement with the end plates 14. Thus, throughout the operation of the engine 10 and the resulting planetation of the piston 13 and the vertical reciprocation of plunger 25, the latter completely closes off the space between the bore 12 and the piston 13 produced by the planetation of the latter in said bore. excepting when the slide valve 29 is opened to allow compressed fuel to flow through the passage 28. a function which will be made clear in describing the operation of the engine.
At 6 oclock, the stator 11 is provided with a radial slot 31 for slideably receiving a seal vane 32 which is spring biased inwardly from said slot so as to be held constantly in sealing engagement with the peripheral surface of the piston 13.
At approximately 5:30 oclock. the stator 11 is provided with an exhaust port 33 which opens into the bore 12 just in advance of the seal vane 32.
The stator 11 is also provided with a fuel vapor intake port 34 which opens into bore 12 just beyond seal vane 32 at approximately 6:30 oclock. said port being fitted with a counterbalanced check valve 35 which opens to admit vaporized fuel into said bore in response to a suction produced in the latter and closes to prevent a backflow of said vapor into the port 34 when said suction terminates at the end of the suction stroke of the engine.
The stator I1 is also provided with a slot 40 coextensive in length with the bore 12 and extending radially outwardly therefrom approximately at l:20 oclock. Slideably received in said slot is a valve vane 41 which is spring biased normally into sealing relation with the exterior surface of piston I3 but is subject to being cam retracted into open position as shown in hole 45 is provided by the stator 11 through which a spark plug 46 may be inserted into said ignition subchamber for ignition of a fuel charge confined therein.
The engine is provided with a conventional elec tric magneto and timer (not shown) driven by shaft and connected to the spark plug 46 so as to energize said plug in proper timed relation with rotation of the shaft 15 for igniting a fuel charge contained in ignition sub-chamber 44 in the generating of a power stroke in the engine 10. The slide valve 29 and valve vane 41 lo cated respectively at 12 oclock and 1:20 oclock on opposite sides of the ignition sub-chamber 44 are both spring biased radially inwardly into closed position and are correlatively opened respectively by earns 47 and 48 fixed on shaft 15 and connected to said slide valve and valve vane by cam follower rollers 49 and 50.
Provided in the periphery of piston 13 at suitable circumferentially spaced positions around said periphery, are axially aligned radial slots 55 in which are mounted narrow flat seals 56 which are T-head in cross section and thus limited in the distance they are free to extend radially from the periphery of said piston. The function of seals 56 is to maintain the periphery of the piston in snug sealing contact with the bore 12 so as to substantially prevent leakage between the bore 12 and portions of the periphery of the piston 12 closely juxtaposed in relation to said bore wherever the high point 18 of eccentric hub 16 is disposed at its closest spacing with said stator bore. Thus one of the seals 56 is located just clockwise beyond the valve vane 41 when said vane opens as shown in FIG. 2 and remains in sealing engagement with said stator bore until the next successive seal 56 (in a clockwise direction therefrom) comes into sealing relation with said bore as shown in FIG. 3. Seals (not shown) provided in the ends of piston 13 maintain sealing contact with the end plates 14.
OPERATION To distinguish between the seals 56 in describing the operation of the engine 10, these will be individually identified by adding a different small case letter to the reference numeral 56.
Although not shown on the drawings, it is understood that the engine 10 must be furnished with a carburetor or other source for vaporized fuel in order for it to operate and this is connected to the fuel inlet port 34.
It is also assumed that the engine 10 requires a self starter which is connected to the shaft 15 so as to turn this over in order to start the engine operating. Two or 3 revolutions of this shaft should always be sufficient to start the engine. A complete cycle of the engine 10 is performed with each revolution of shaft 15.
FIG. 1 shows the engine at dead center with the high point 18 of the hub 16 being located at 12 oclock. The piston 13 is now located in upward tangential contact with the stator bore 12. The slide valve 29 at 12 oclock has just been closed shutting off the compressed fuel passage 28, and the valve vane 41 at 1:20 oclock, which has been closed and in sealing engagement with the piston 13 for approximately 180, is about to be opened by cam 48. FIG. 1 shows the engine in the middle of a fuel suction stroke which is shown as having been completed in FIG. 3. The fuel compression stroke starts with the piston high point 18 at 3 oclock and concludes with the piston at dead center as shown in FIG. 1. As shown in FIG. 4, the valve vane 41 is allowed to be spring closed by cam 48 while the slide valve 29 is positively cam opened by cam 47 at approximately 6:30 o'clock as shown in FIG. 4. The ignition sub chamber 44 is thus closed off from the space CE (combustion exhaust chamber) as shown in FIG. 4 just as this space comes into communication with the exhaust port 33 and starts to contract, thereby expelling exhaust gases from said chamber through said exhaust port. As the high point 18 of hub 16 continues from the point where this is shown in FIG. 4 to its dead center position shown in FIG. 1, the fuel vapor sucked into chamber SC is compressed and expelled from said chamber through compressed fuel passage 28 and into the ignition subchamber 44. It will readily be seen by comparing FIG. 4 and FIG. 1, that during this interval. the compressed fuel thus delivered to sub-chamber 44 is further compressed between the walls of said subchamber which include the stator bore 12, the periphery of piston 13, the abutment plunger 25 and the valve vane 41. As shown in FIG. 1, the slide valve 29 is cam closed at approximately 12 oclock to confine in the ignition sub-chamber 44 the compressed fuel charge delivered thereto, the slide valve 29 remaining thus closed until the conclusion of the power stroke to be effected by the ignition of said charge. Just as that ignition occurs or possibly just before said ignition, the cam 48 functions to open the valve vane 41 so that this is withdrawn radially from engagement with the periphery of the piston 13 as shown in FIG. 2. Seal 56a is now already in sealing engagement with the bore 12 at a location close to and on the clockwise side of valve vane 41 as shown in FIG. 2. At this moment, the high point 18 of eccentric hub 16 is about on a radius with the center of combustion chamber 44.
The effect of the expansion of the fuel charge by its ignition in ignition sub-chamber 44 is to apply tangential torque forces to the piston 13 along those portions of the periphery of said piston coming within the compass of seal 56a and seal 56b as the planetation of said piston advances to the point shown in FIG. 3 where the high point 18 of eccentric hub 16 is at 4:30 oclock. In fact, seal 56b is still in sealing contact with the bore 12 in this view and the expansive pressure of the gases of combustion are still effective in applying tangential torque forces to the piston 13 so long as seal 56d remains in sealing engagement with bore 12.
A complete cycle of operation of the engine 10 has now been described. From the phase shown in FIG. 4 with the high point 18 at 6:30 oclock and just passing over the fuel inlet port 34, a suction stroke is starting which will cause the counter balanced check valve 35 to automatically open and vaporized fuel to be sucked into the suction-compression chamber generated by the travel of the piston 13 between the positions in which this is shown in FIG. 4 to the position in which it is shown in FIG. 5 and in fact, FIGS. 1 and 2.
To facilitate the burning of all pollutants remaining in the gases of combustion produced in each power stroke, the engine 10 is preferably provided with a series of glow plugs or pods 57 which are countersunk in the bore 13 between the valve vane 41 and the exhaust port 33. These plugs are heated by a short running of the engine to an incandescent temperature. While the engine continues to run therefore, the plugs 57 improve combustion and continue to ignite and burn combustible pollutants remaining mixed with the combustion products after the exhaust port opens.
While the engine of the invention is described as preferably having seal vane 32 located at 6 o'clock and exhaust port 33 located at 5:30 oclock and valve 35 located at 6:30 oclock. these three elements may as a group be located as much as or more clockwise or counterclockwise from their preferred positions aforesaid. The purpose of such a counter clockwise shift in located would be to shorten the power stroke of the engine and lengthen the suction-compression stroke thereof, and thus invest the engine with a higher compression ratio. A similar clockwise shift would. of course, accomplish the opposite effect.
It is further to be understood that the engine 10 is an adaptation to internal combustion engine practice of the well known Kinney tethered planetating piston pump and that this engine is adapted to employ any of the various types of piston tethering means proven successful in the design of said pumps.
The disclosure of a specific preferred embodiment of the present invention in this application is for illustrative purposes only. the full scope of the invention to be found in the claims construed in the light of the doctrine of mechanical equivalents.
I claim:
1. In a four-phase cycle planetating piston internal combustion engine. the combination of:
a stator having a cylindrical bore closed by end walls providing a pair of bearings co-axial with said bore;
a shaft journalling in said bearings;
an eccentric fixed on said shaft;
a cylindrical annular piston within which said eccentric journals, said piston being co-extensive axially with said bore and of such an outside diameter as to remain in a progressively shifting approximately tangentially sealing contact with said bore as said shaft rotates;
first, second and third abutment means radially biased respectively at about 12 o'clock, 1:20 oclock and 6 oclock to seal off the free space between said piston and bore at said respective circumferentially spaced points to produce a fuel vapor suction and compression chamber extending clockwise from 6 to 12 oclock, a fuel vapor expansion and exhaust chamber extending clockwise from 12 to 6 oclock, and a fuel charge confinement and ignition sub-chamber extending clockwise between 12 and 1:20 oclock;
means in said stator providing an exhaust port opening from said bore at an advanced point in said ex pansion and exhaust chamber;
means in said stator providing a fuel inlet port for admitting gaseous fuel into said suction and compression chamber when the latter is in its suction phase;
first cam controlled passage means delivering compressed gaseous fuel directly from said suctioncompression chamber to said ignition subchamber, and then shutting said passage means;
second cam controlled means for opening said second abutment means in timely relation with and following the shutting of said passage means;
a timely actuated ignition means for igniting a fuel charge confined by said ignition sub-chamber at the beginning of a power stroke: and
tethering means connected peripherally to said piston to limit the rotation of said piston relative to said stator to a planetating movement in said bore.
2. An engine recited in claim 1 wherein said stator is provided with a slot extending radially from said bore at 12 oclock;
said first abutment means slideable in said slot; and
means making a sealed hinged connection between said piston and the inner edge of said first abutment means;
said first cam controlled passage means being embodied in said first abutment means and delivering a compressed fuel charge directly therethrough into said ignition sub-chamber.
3. An engine as recited in claim 2 wherein at least one of said stator and piston elements is hollowed out in the area of said ignition sub-chamber to provide the compression ratio designed for the engine, and wherein slots ex end radially from the stator bore at 1:20 and at 6 o'clock to slideably receive the second and third abutments which are spring biased from said slots into sealing relation with said piston.
4. In a four-phase cycle planetating piston internal combustion engine, the combination of:
a stator having a cylindrical bore closed by end walls providing a pair of bearings co-axial with said bore;
a shaft journaling in said bearings;
an eccentric fixed on said shaft;
a cylindrical annular piston journalling on said eccentric and being co-extensive with said bore and of such an outside diameter as to remain in tangential sealing contact with said bore as said shaft rotates;
there being a slot in said stator extending radially from said bore at 12 oclock;
a plunger plate slideable in said slot;
means making a sealed hinged connection between said piston and the inner edge of said plunger plate;
there being a slot in said stator extending radially from said bore at approximately 6 oclock;
a seal vane radially slideable in said last recited slot and spring biased constantly into sealing relation with the periphery of said piston, said piston plunger and seal vane dividing the vacant space in said stator into a fuel vapor suction and compression chamber extending clockwise from said vane to said plunger, and a combustion and exhaust chamber extending clockwise from said plunger to said vane;
means on said stator providing an exhaust port opening from said bore at about 5:30 o'clock;
means in said stator providing a fuel inlet port for delivering carbureted fuel vapor into said bore at about 6:30 oclock;
there being a slot in said stator extending radially from said bore at approximately 1:20 oclock;
a valve vane radially slideably extensible from said last recited slot into sealing relation with said piston;
there being a fuel vapor passage extending through said plunger approximately tangential with said piston;
a compressed-fuel valve controlling said passage;
at least one of said stator and piston elements being hollowed out in the area where they tangentially meet between 12 o'clock and 1:20 oclock to provide an ignition sub-chamber which during a power stroke of said engine, comprises an upper portion of said combustion-exhaust chamber;
cam means coordinately actuating said valve vane and compressed fuel valve to close said valve vane while a compressed fuel charge is being delivered through said passage into said ignition subchamber, to close said compressed fuel valve at the conclusion of said delivery, to open said valve vane upon the ignition of said fuel charge, to produce a power stroke, to reclose said valve vane at the conclusion of said power stroke and then reopen said compressed fuel valve to admit another compressed fuel charge through said passage into said ignition sub-chamber.
5. An engine as recited in claim 1 wherein said fuel inlet port is provided with a check valve preventing backflow of fuel from said fuel suction compression chamber.
6. An engine as recited in claim 1 wherein the periphcry of said piston is provided with radial slots in which narrow flat sealing vanes are trapped so as to be biased to extend radially from said slots a short distance only from the periphery of said piston so that said vane progressively makes sealing engagement coextensive with the length of said piston with said stator bore so as to impose the main burden of maintaining sealing engagement between said piston and said bore upon said
Claims (6)
1. In a four-phase cycle planetating piston internal combustion engine, the combination of: a stator having a cylindrical bore closed by end walls providing a pair of bearings co-axial with said bore; a shaft journalling in said bearings; an eccentric fixed on said shaft; a cylindrical annular piston within which said eccentric journals, said piston being co-extensive axially with said bore and of such an outside diameter as to remain in a progressively shifting approximately tangentially sealing contact with said bore as said shaft rotates; first, second and third abutment means radially biased respectively at about 12 o''clock, 1:20 o''clock and 6 o''clock to seal off the free space between said piston and bore at said respective circumferentially spaced points to produce a fuel vapor suction and compression chamber extending clockwise from 6 to 12 o''clock, a fuel vapor expansion and exhaust chamber extending clockwise from 12 to 6 o''clock, and a fuel charge confinement and ignition sub-chamber extending clockwise between 12 and 1:20 o''clock; means in said stator providing an exhaust port opening from said bore at an advanced point in said expansion and exhaust chamber; means in said stator providing a fuel inlet port for admitting gaseous fuel into said suction and compression chamber when the latter is in its suction phase; first cam controlled passage means delivering compressed gaseous fuel directly from said suction-compression chamber to said ignition sub-chamber, and then shutting said passage means; second cam controlled means for opening said second abutment means in timely relation with and following the shutting of said passage means; a timely actuated ignition means for igniting a fuel charge confined by said ignition sub-chamber at the beginning of a power stroke; and tethering means connected peripherally to said piston to limit the rotation of said piston relative to said stator to a planetating movement in said bore.
2. An engine as recited in claim 1 wherein said stator is provided with a slot extending radially from said borE at 12 o''clock; said first abutment means slideable in said slot; and means making a sealed hinged connection between said piston and the inner edge of said first abutment means; said first cam controlled passage means being embodied in said first abutment means and delivering a compressed fuel charge directly therethrough into said ignition sub-chamber.
3. An engine as recited in claim 2 wherein at least one of said stator and piston elements is hollowed out in the area of said ignition sub-chamber to provide the compression ratio designed for the engine, and wherein slots extend radially from the stator bore at 1:20 and at 6 o''clock to slideably receive the second and third abutments which are spring biased from said slots into sealing relation with said piston.
4. In a four-phase cycle planetating piston internal combustion engine, the combination of: a stator having a cylindrical bore closed by end walls providing a pair of bearings co-axial with said bore; a shaft journaling in said bearings; an eccentric fixed on said shaft; a cylindrical annular piston journalling on said eccentric and being co-extensive with said bore and of such an outside diameter as to remain in tangential sealing contact with said bore as said shaft rotates; there being a slot in said stator extending radially from said bore at 12 o''clock; a plunger plate slideable in said slot; means making a sealed hinged connection between said piston and the inner edge of said plunger plate; there being a slot in said stator extending radially from said bore at approximately 6 o''clock; a seal vane radially slideable in said last recited slot and spring biased constantly into sealing relation with the periphery of said piston, said piston plunger and seal vane dividing the vacant space in said stator into a fuel vapor suction and compression chamber extending clockwise from said vane to said plunger, and a combustion and exhaust chamber extending clockwise from said plunger to said vane; means on said stator providing an exhaust port opening from said bore at about 5:30 o''clock; means in said stator providing a fuel inlet port for delivering carbureted fuel vapor into said bore at about 6:30 o''clock; there being a slot in said stator extending radially from said bore at approximately 1:20 o''clock; a valve vane radially slideably extensible from said last recited slot into sealing relation with said piston; there being a fuel vapor passage extending through said plunger approximately tangential with said piston; a compressed-fuel valve controlling said passage; at least one of said stator and piston elements being hollowed out in the area where they tangentially meet between 12 o''clock and 1:20 o''clock to provide an ignition sub-chamber which, during a power stroke of said engine, comprises an upper portion of said combustion-exhaust chamber; cam means coordinately actuating said valve vane and compressed fuel valve to close said valve vane while a compressed fuel charge is being delivered through said passage into said ignition sub-chamber, to close said compressed fuel valve at the conclusion of said delivery, to open said valve vane upon the ignition of said fuel charge, to produce a power stroke, to reclose said valve vane at the conclusion of said power stroke and then reopen said compressed fuel valve to admit another compressed fuel charge through said passage into said ignition sub-chamber.
5. An engine as recited in claim 1 wherein said fuel inlet port is provided with a check valve preventing backflow of fuel from said fuel suction compression chamber.
6. An engine as recited in claim 1 wherein the periphery of said piston is provided with radial slots in which narrow flat sealing vanes are trapped so as to be biased to extend radially from said slots a short distance only from the periphery of said piston so tHat said vane progressively makes sealing engagement co-extensive with the length of said piston with said stator bore so as to impose the main burden of maintaining sealing engagement between said piston and said bore upon said vanes.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US450290A US3882827A (en) | 1974-03-12 | 1974-03-12 | Four-phase cycle planetating piston internal combustion engine |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US450290A US3882827A (en) | 1974-03-12 | 1974-03-12 | Four-phase cycle planetating piston internal combustion engine |
Publications (1)
Publication Number | Publication Date |
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US3882827A true US3882827A (en) | 1975-05-13 |
Family
ID=23787511
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US450290A Expired - Lifetime US3882827A (en) | 1974-03-12 | 1974-03-12 | Four-phase cycle planetating piston internal combustion engine |
Country Status (1)
Country | Link |
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US (1) | US3882827A (en) |
Cited By (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4286555A (en) * | 1978-10-30 | 1981-09-01 | Williams Robert H | Rotary internal combustion engine |
US4342295A (en) * | 1979-04-18 | 1982-08-03 | Williams Robert H | Rotary internal combustion engine |
US4342297A (en) * | 1979-04-18 | 1982-08-03 | Williams Robert H | Rotary internal combustion engine |
US4342296A (en) * | 1979-04-18 | 1982-08-03 | Williams Robert H | Rotary internal combustion engine |
US5348455A (en) * | 1993-05-24 | 1994-09-20 | Tecumseh Products Company | Rotary compressor with rotation preventing pin |
US20080044306A1 (en) * | 2004-06-24 | 2008-02-21 | Lyubcho Kirilov Georgiev | Device-Operating Module |
US9334792B2 (en) | 2012-02-21 | 2016-05-10 | Rotary Innovations, Llc | Straight shaft rotary engine |
CN105971840A (en) * | 2016-07-01 | 2016-09-28 | 沈炜 | Annular inflator |
CN106194730A (en) * | 2016-08-19 | 2016-12-07 | 陶如意 | A kind of reciprocating-piston air pump |
Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US244673A (en) * | 1881-07-19 | Thomas eose | ||
US2344159A (en) * | 1942-08-24 | 1944-03-14 | Meeks Lonnie | Rotary internal combustion engine |
-
1974
- 1974-03-12 US US450290A patent/US3882827A/en not_active Expired - Lifetime
Patent Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US244673A (en) * | 1881-07-19 | Thomas eose | ||
US2344159A (en) * | 1942-08-24 | 1944-03-14 | Meeks Lonnie | Rotary internal combustion engine |
Cited By (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4286555A (en) * | 1978-10-30 | 1981-09-01 | Williams Robert H | Rotary internal combustion engine |
US4342295A (en) * | 1979-04-18 | 1982-08-03 | Williams Robert H | Rotary internal combustion engine |
US4342297A (en) * | 1979-04-18 | 1982-08-03 | Williams Robert H | Rotary internal combustion engine |
US4342296A (en) * | 1979-04-18 | 1982-08-03 | Williams Robert H | Rotary internal combustion engine |
US5348455A (en) * | 1993-05-24 | 1994-09-20 | Tecumseh Products Company | Rotary compressor with rotation preventing pin |
US20080044306A1 (en) * | 2004-06-24 | 2008-02-21 | Lyubcho Kirilov Georgiev | Device-Operating Module |
US7762228B2 (en) * | 2004-06-24 | 2010-07-27 | Lyubcho Kirilov Georgiev | Device-operating module |
US9334792B2 (en) | 2012-02-21 | 2016-05-10 | Rotary Innovations, Llc | Straight shaft rotary engine |
CN105971840A (en) * | 2016-07-01 | 2016-09-28 | 沈炜 | Annular inflator |
CN105971840B (en) * | 2016-07-01 | 2018-08-07 | 王美燕 | annular inflator |
CN106194730A (en) * | 2016-08-19 | 2016-12-07 | 陶如意 | A kind of reciprocating-piston air pump |
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