US3610217A - Balanced-free piston engine - Google Patents

Balanced-free piston engine Download PDF

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US3610217A
US3610217A US868008A US3610217DA US3610217A US 3610217 A US3610217 A US 3610217A US 868008 A US868008 A US 868008A US 3610217D A US3610217D A US 3610217DA US 3610217 A US3610217 A US 3610217A
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power
piston
engine
cylinder
acting
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Anton Braun
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Tectonics Companies Inc
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Assigned to TECTONICS COMPANIES reassignment TECTONICS COMPANIES ASSIGNMENT OF ASSIGNORS INTEREST. SEE DOCUMENT FOR DETAILS Assignors: BRAUN, ANTON T.
Assigned to TECTONICS COMPANIES, INC., A CORP. OF MN reassignment TECTONICS COMPANIES, INC., A CORP. OF MN ASSIGNMENT OF ASSIGNORS INTEREST. Assignors: COMPRESSOR PARTNERS LTD., HILLIARD-LYONS PATENT MANAGEMENT, INC., A CORP. OF KY, HLPM NETHERLANDS BV, A DUTCH CORP.
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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
    • F02B71/00—Free-piston engines; Engines without rotary main shaft
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01B—MACHINES OR ENGINES, IN GENERAL OR OF POSITIVE-DISPLACEMENT TYPE, e.g. STEAM ENGINES
    • F01B9/00—Reciprocating-piston machines or engines characterised by connections between pistons and main shafts, not specific to groups F01B1/00 - F01B7/00
    • F01B9/04—Reciprocating-piston machines or engines characterised by connections between pistons and main shafts, not specific to groups F01B1/00 - F01B7/00 with rotary main shaft other than crankshaft
    • F01B9/047—Reciprocating-piston machines or engines characterised by connections between pistons and main shafts, not specific to groups F01B1/00 - F01B7/00 with rotary main shaft other than crankshaft with rack and pinion

Definitions

  • Unsymmetrical, synchronized, balanced, free piston engines are disclosed in which a pair of alternately acting power pistons are interconnected to form a double-acting power piston, in which the power piston is connected to the movable member of an energy absorbing device to be driven by the engine in order to provide the reciprocatory power input to that energy absorbing device, the double-acting power piston, the movable member, and the connection between them defining a power assembly, and in which the movement of the power assembly in the engine is balanced by the oppositely directed translational movement, with respect to the engine housing, of a counterbalancing movable weight associated with a synchronizer-balancer.
  • Engines incorporating energy absorbing devices in the form of a pump, an electrical generator, and a double-acting reciprocal compressor are specifically shown. Also specifically shown are two single-acting power sections which may be used together in place of the one double-acting power section.
  • This invention relates to free piston engines, and particularly to unsymmetrical, synchronized, balanced, free piston engines, and more particularly to unsymmetrical, synchronized, balanced, free piston engines in which at least two alternately acting power pistons provide the power necessary to drive the reciprocally movable member of an energy absorbing device.
  • Prior free piston engines which are unsymmetrical, synchronized, and balanced and which use a power section to provide power to the reciprocally movable member of an energy absorbing device and a bouncer section to return the power piston to a point in the power cylinder where repetitive combustion can occur.
  • a bouncer compressor may be a disadvantage, however, in that stagnant air within a bouncer compressor may become fouled by lubricating oil and present a control problem. Further, an engine using a bouncer compressor to return the power piston does not have a naturally equal stroke-time function on both strokes of the movable member of the energy absorbing device.
  • free piston engines according to the present invention are unsymmetrical, synchronized, balanced, free piston engines wherein at least two alternately acting power sections, that is, two power sections where one section is providing power on its power stroke while the other section is accepting power on its compression stroke provide power to the engine, wherein each power section is connected with the movable member of an energy absorbing device to be driven by the engine to form a power assembly such that the power piston within each power section is connected to move together as a unit with the movable member of the energy absorbing device and the remaining parts of the power assembly, and wherein the engine is balanced by the mechanically synchronized movement of a counterbalancing movable weight arranged to have transla tional movement with respect to the housing of the free piston engine in a direction opposite to the direction of movement of the power assembly.
  • Free piston engines of the present invention are simple and compact engines which provide twice the work output per cycle with the same capacity synchronizer and with significantly less than a factor of two increase in the overall size and weight of the engine as compared to prior engines using bouncer compressors to return the power piston.
  • the bouncer compressor is, in fact, eliminated in engines according to the present invention since a high rate of pressure rise occurs alternately in each combustion chamber as the respective power piston approaches its top-deadcenter position.
  • This high rate of pressure rise in the combustion chamber renders the engine relatively stlff at both ends of its stroke; that is, the power pistons traveling in one direction are caused to stop and return" or to travel in the opposite direction by force which increases at a very high rate as the power pistons approach their top-deadcenter positions, all without a bouncer compressor.
  • This stiff characteristic of the engine is particularly useful when the energy absorbing device is a double acting reciprocal compressor because the stiff" characteristic prevents any significant compressor piston travel beyond the desired nominal point, i.e. it permits a low overstroke requirement to be adopted in the compressor which, in turn, results in the compressor being able to have a small clearance volume per given output, or a high volumetric efficiency.
  • Free piston engines according to the present invention also have a naturally equal stroke-time function on both strokes of the movable member of the energy absorbing device driven by the engine. Where a hydrostatic pump is the energy absorbing device driven by the engine, large dampers or accumulators would be needed to smooth the flow without this naturally equal stroke-time function provided by engines of the present invention. Engines of the present invention allow the smallest damper size for any given pump. Where an AC generator is the energy absorbing device driven by the engine, an unacceptably high DC component would be provided from the AC generator because of the asymmetry of the output waveform without this naturally equal stroke-time function provided by engines of the present invention. Engines of the present invention allow the smallest DC component for any given electrical generator.
  • the unsymmetrical, synchronized, balanced, free piston engines of the present invention may be used as a simple, compact, relatively small and lightweight power unit for operating various types of energy absorbing devices, such as reciprocal compressors, pumps, generators, and the like. That is, because of the flexible nature of the present invention, it is readily adaptable to perform as a power package and to provide power to various types of energy absorbing devices which accept a reciprocatory power input.
  • FIG. 1 is a vertical cross-sectional view of an embodiment of the improved, free piston engine of the present invention shown with a double-acting power section connected with an energy absorbing device.
  • FIG. 2 is a vertical cross-sectional view taken along the section line 2-2 of FIG. 1.
  • FIG. 3 is a schematic, vertical, cross-sectional view of another embodiment of the improved, free piston engine of the present invention shown as connected with an energy absorbing device in the form of a fluid pump.
  • FIG. 4 is a schematic, vertical, cross-sectional view of still another embodiment of the improved, free piston engine of the present invention shown connected with an energy absorbing device in the form of an electrical generator.
  • FIG. 5 is a schematic, vertical, cross-sectional view of still another embodiment of the improved, free piston engine of the present invention shown connected with an energy absorbing device in the form of a double-acting reciprocal compressor.
  • FIGS. 6 and 7 are pressure-volume curves illustrating a major advantage of engines according to the present invention.
  • FIG. 8 is a graphical representation of velocity plotted versus stroke to illustrate another major advantage of engines according to the present invention.
  • FIGS. 9 and 10 show vertical cross-sectional views of two single-acting power sections which together may be advantageously used with engines according to the present invention in place of the one double-acting power section shown in FIG. 1.
  • FIG. 1 Embodiment An improved, balanced, free piston engine 11 of the present invention is generally shown in FIGS. 1 and 2.
  • the free piston engine 11 includes a power section 12, and a synchronizerbalancer section 13.
  • An energy absorbing device, shown diagrammatically at 14, is spaced from the right end of the synchronizer-balancer section 13.
  • the energy absorbing device 14 may be a liquid pump, an electrical generator, a double-acting reciprocal compressor, or any other device which utilizes or absorbs reciprocatory power.
  • the power section 12 includes a cylindrical housing 15 which has a power cylinder 16 formed therein.
  • a double-acting power piston 17 is positioned within the cylinder 16 for reciprocal movement therein substantially parallel to the longitudinal axis of the cylinder 16.
  • the piston includes a first or outer power face 18, a second or inner power face 19 and a generally annular portion 21 interconnecting the outer power face 18 and the inner power face 19 such that they reciprocate together as a unit and form a single, alternately acting, doubleacting, power piston.
  • Piston rings 22 are carried in grooves formed in the piston 17 for minimizing the leakage of gases between cylinder 16 and the piston 17.
  • the left end 23 of the housing 15 is closed by a cylinder head 24 which is bolted to the end 23 of the housing 15 by a plurality of bolts, one of which is shown at 25.
  • the cylinder head 24 together with the outer power face 18 of the piston 17 define a first or outer combustion chamber 26 in the cylinder 16.
  • a conventional fuel injector unit 27 is positioned in an aperture 28 formed in the cylinder head 24 so that its inner end communicates with chamber 26.
  • the right end 29 of the housing 15 is closed by a cylinder head 34 which is bolted to the end 29 of the housing 15 by a plurality of bolts, one of which is shown at 30.
  • cylinder head 34 together with the inner face 19 of the piston 17 define a second or inner combustion chamber 31 in the cylinder 16.
  • a further conventional fuel injector unit 32 is positioned in an aperture 33 formed in the cylinder head 34 so that the inner end of fuel injector 32 communicates with the inner combustion chamber 31.
  • the inner cylinder head 34 also forms a wall between the power section 12 and the synchronizer-balancer section 13, and, in order to provide a connection between the power section and the synehronizer-balancer section, the cylinder head 34 has a central aperture 36 formed therein so that the central longitudinal axes of the aperture 36 and the cylinder 16 are coaxial.
  • Conventional combustion chamber shaft seals 37 are positioned in the aperture 36, for reasons hereinafter explained. Shaft seals 37 must withstand the temperature and pressure of the combustion chamber 31, but seals of this kind are well known in the art.
  • a duct 39 is shown connected with housing 15 to provide communication between a plurality of peripherally spaced duel inlet ports, one of which dual ports is shown fonned in the housing 15 at 41a and 41b, and a source of air or fuel-air mixture, not shown.
  • a plurality of peripherally spaced duel exhaust ports or openings, one of which dual ports is shown formed in housing 15 at 42a and 42b, permit combustion gas in the combustion chambers 226 and 31 to be exhausted from cylinder 16.
  • the outermost edges of the ports 41a and 41b are positioned such that the projection of these outennost edges on the central longitudinal axis of cylinder 16 is within the projection of the outermost edges of the ports 42a and 42b on the central longitudinal axis of cylinder 16.
  • the ports 41 and 42 are further arranged, relative to the combustion chambers 26 and 31, so that the chambers will be properly scavenged during normal operation of the engine. That is, as the power piston 17 approaches its rightmost position, exhaust ports 420 are opened, and exhaust gases can blowdown" to the approximate pressure of the fresh charge of air or fuel-air mixture that exists in duct 39 at the time inlet ports 41a are opened. As the inlet ports 41a are opened by piston 17, the air or fuel-air mixture from the source, not shown, can enter chamber 26 through duct 39 and ports 41a, and this fresh charge of air or fuel-air mixture can scavenge chamber 26 to provide a fresh charge for the next power stroke in chamber 26. With the piston 17 traveling towards its leftmost position, exhaust gases within combustion chamber 31 can similarly blowdown" through exhaust ports 42b, and chamber 31 can be similarly scavenged through duct 39, inlet ports 41b, and exhaust ports 42b.
  • the power piston 17 and all other main pistons within the engine are a part of and move with a power assembly 43 that includes, in addition, all other parts of the engine which move with and are connected with power piston 17.
  • These parts include the movable member of the energy absorbing device 14, and the means for connecting the main pistons together and for interconnecting the main pistons with the movable member of the energy absorbing device.
  • the main pistons and the movable member of the energy absorbing device form parts of the power assembly and always move together as a unit within the engines of the present invention.
  • piston 17 is fastened to the left end of a shaft 44 by means of a bolt 45.
  • the right end of shaft 44 is connected with the left end of a double rack member 46.
  • a second shaft 48 arranged in axial alignment with shaft 44, is connected to the right end of double rack member 46 and interconnects the rack member 46 with the reciprocally movable portion of the energy absorbing device 14.
  • the power assembly 43 includes the power piston 17, the shaft 44, the double rack member 46, the shaft 48, and the reciprocally movable portion of the energy absorbing device 14, together with the bolt 45, and any other fastening means utilized to interconnect the aforementioned parts, and the piston rings 22 carried by the piston.
  • the component parts of the power assembly 43 are described more fully hereinafter.
  • the shaft 44 interconnecting the power piston 17 and the double rack member 46 extends into the synchronizer section 13 of the engine through the aperture 36 formed in the cylinder head 34 and is sealed by the conventional combustion chamber shaft seals 37 positioned in this aperture 36 so as to minimize the leakage of gas and lubricant between the shaft and the aperture.
  • the synchronizer section 13 includes housing 49, which, as noted above, has its left end closed by cylinder head 34. Bolts 35, two of which are shown in FIG. 1, are used to fasten the housing 49 to cylinder head 34.
  • An end wall 51 closes the right end of the housing 49 and is formed integrally with a sidewall 52 of the housing 49, as shown in FIG. 1.
  • the end wall 51 could also be a separate member attached to the housing 49 by a plurality of bolts.
  • the end wall 51 has a central aperture 58 positioned so that its central axis is coaxial to the central axis of shaft 44.
  • the second shaft 48 extends through the aperture 58 formed in the wall 51, and a conventional shaft seal 59 is mounted in the aperture 58 so as to minimize the leakage of gas and lubricant between the shaft 48 and the aperture 58.
  • the engine 1 1 includes a synchronizer-balancer assembly 62 mounted within the housing 49.
  • the synchronizer-balancer assembly 62 is connected with the power assembly 43 through a double rack member 46 which may also be termed a first means of the balancing and synchronizing assembly.
  • the balancing and synchronizing assembly 62 also includes a pair of pinions 63 and 64 which are mounted for rotation about fixed axes on a pair of shafts 65 and 66, respectively.
  • the ends of the shafts 65 and 66 are supported by a pair of fixed sideplates 67 and 68, which are positioned on opposite sides of the double rack member 46.
  • One end of each of the plates 67 and 68 is secured to the right face of the cylinder head 34 and the other ends 69 thereof project to the right from the cylinder head 34 towards the end wall 51 of the housing 49.
  • the plates 67 and 68 are spaced an equidistance from the double rack member 46 so that the member 46 can slide freely between the plates 67 and 68, and are positioned so that the plates are substantially parallel to each other and to the longitudinal central axis of the power assembly 43.
  • the shafts 65 and 66 are supported by the plates 67 and 68 approximately midway between the cylinder head 34 and the end wall 51 and are positioned vertically on opposite sides of the longitudinal central axis of the double rack member 46 and equidistant from the member 46, with the central longitudinal axes of the shafts 65 and 66 being arranged at 9 to the central longitudinal axis of the power assembly 43.
  • the distance between the plates 67 and 68 is sufficient so that the pinions 63 and 64 can rotate freely between the plates.
  • the double rack member 46 includes upper and lower racks 71 and 72 which are formed in back-to-back fashion so that the teeth thereof project substantially radially outwardly from the member 46.
  • the teeth of the racks 71 and 72 are arranged so that there is always engagement between the teeth of the racks 71 and 72 and the teeth of the pinions 63 and 64, respectively, whereby reciprocatory movement of the power assembly, and thus the racks 71 and 72, causes corresponding rotary movement of the pinions 63 and 64.
  • the synchronizer-balancer assembly 62 further includes a pair of movable wall members 73 and 74 which are positioned adjacent to and parallel with the fixed sideplates 67 and 68, respectively, with the movable members 73 and 74 being positioned a greater distance from the double rack member 46 than the plates 67 and 68 so that the movable members 73 and 74 can slide freely with respect to the fixed plates 67 and 68.
  • a pair of racks 75 and 76 are carried by and positioned between the upper and lower ends of the movable wall members 73 and 74, as shown in FIG. 2.
  • a plurality of pins or rivets extend through the racks 75 and 76 and the ends of the movable members 73 and 74 and are used to secure the racks 75 and 76 to the movable members 73 and 74.
  • the racks 75 and 76 are positioned so that the teeth thereof project toward the teeth of the racks 71 and 72, respectively, i,e., project substantially radially inwardly relative to the double rack member 46, and engage the pinions 63 and 64, respectively, substantially diametrically opposite the points of engagement between the teeth of the pinions 63 and 64 and the racks 71 and 72, respectively.
  • the synchronizer-balancer assembly 62 and more specifically the counterbalancing part of assembly 62 which includes racks 75 and 76 and the members 73 and 74, can reciprocate freely along its central longitudinal axis with respect to the housing 49 and to any relatively fixed member therein and with respect to any parts of the power assembly 43.
  • the racks 75 and 76 are secured together by the movable members 73 and 74 so as to prevent relative movement therebetween and because the racks 71 and 72 are integrally formed in a back-to-back relationship on the double rack member 46, the normal components of the forces created by the transmission of forces between the teeth of the racks and pinions are balanced.
  • the unique structure and structural arrangement of the engine permits the total length of the engine to be substantially equal to four times the swept stroke of the piston 17, plus the length required for the energy absorbing device 14.
  • engine 1 1 the operation of engine 1 1 is as follows: combustion occurs in chamber 26 near the top-deadcenter position of piston 17, i.e. when the piston 17 has moved to its leftmost operating position, and such combustion, together with any other energy in the engine 11 or the device 14 available to support the rightward movement of the power assembly 43, causes the piston 17 and the rest of power assembly 43 including the connecting part of the synchronizer-balancer assembly, rack member 46, to be moved to the right with respect to the engine housing, in a translational manner.
  • combustion chamber 26 and combustion chamber 31 are alternately acting in that gas within combustion chamber 26 is expanding and providing energy to the engine while gas within combustion chamber 31 is being compressed and accepting energy from the engine, and vice versa.
  • FIG. 3 Embodiment
  • the engine 100 shown schematically in FIG. 3, includes a power section 12 and synchronizer-balancer section 13 which are substantially identical in structure and mode of operation to the power section 12 and the synchronizer-balancer section 13, respectively, of engine 11.
  • Engine 100 is substantially identical to engine 11 of FIG. 1 except that energy absorbing device 14, represented diagrammatically in FIG. 1, is specifically shown as a hydrostatic pump 104 driven by engine 100.
  • the pump 104 includes a pump housing 105 which may be integrally formed with the synchronizer housing 49, or may be separated from the engine as shown in FIG. 1.
  • the housing 105 includes a pair of main bores 106 and 107 which are formed on opposite sides of the central longitudinal axis of the power assembly 43 and which have their central longitudinal axes aligned and disposed at an angle of substantially 90 with respect to the central longitudinal axis of the power assembly 43.
  • the bore 106 is closed at its radially outer end, with respect to the central longitudinal axis of the power assembly 43, except for transverse inlet and outlet bores 108 and 109 which communicate with the bore 106 adjacent to its outer end.
  • Plungers 124 and 125 are positioned for reciprocal movement in the bores 106 and 107, respectively, and conventional seals, not shown, are used to prevent leakage therebetween.
  • Pumping chambers 126 and 127 are defined in the bores 106 and 107, respectively, between the radially outer ends of the bores and the radially outer ends of the plungers 124 and 125. As the plungers reciprocally move within their respective bores, liquid may be alternately sucked into and expelled from the pumping chambers through their inlet and outlet bores, respectively, in a conventional manner.
  • Cam followers 128 and 129 are mounted on the radially inner ends of plungers 124 and 125.
  • a cam member 131 is mounted within the housing for reciprocal movement therein in a direction substantially parallel to the central longitudinal axis of the power assembly 43.
  • the cam 131 has a pair of cam surfaces 132 and 133 formed thereon and is designed so that the cam followers 128 and 129 remain in contact with the surfaces 132 and 133, respectively, at all times and so that the plungers 124 and 125 always move in the opposite directions in their respective bores during the operation of the pump 104. This reduces the pressure waves in the discharge of the pump.
  • the cam surfaces 132 and 136 can be designed so that relatively uniform fluid velocities may be achieved in the discharge from the pump.
  • the cam 131 constitutes a part of the power assembly 43 of engine 100. More specifically, the shaft 48 connects the left end of the cam 131 with the rack member 46.
  • the generator 151 includes the generator housing 152 which, like pump housing 105, may be integral with the synchronizer housing 49.
  • An annular stator arrangement 153 including a conventional core of magnetic material with windings of conductive material formed thereon, is positioned within the housing 152, and a conventional armature 154 is mounted for reciprocal movement within the stator arrangement 153 to conventionally magnetically coact with stator arrangement 153.
  • Annature 154 is connected with the shaft 48 to form a part of the power assembly 43.
  • a second compressor chamber 169 is formed in the compressor cylinder 164 between a left face 171 of compressor piston '165 and and end wall 51 of synchronizer section 13.
  • a set of intake and discharge valves two of which are shown at 172 and 173, respectively, are positioned in the housing 162 adjacent chamber 167 to permit the ingress of fluid to be compressed into chamber 167 and egress of compressed fluid from chamber 167.
  • a set of intake and discharge valves two of which are shown at 174 and 175, respectively, are positioned in housing 162 adjacent chamber 169 to permit the ingress of fluid to be compressed into chamber 169 and the egress of compressed fluid from chamber 169.
  • gas or fluid within chamber 169 is compressed and discharged through valve 175 while, simultaneously, gas or fluid is being sucked into chamber 167 through intake valve 172.
  • the gas or fluid in chamber 167 is compressed and discharged through discharge valve 173 while, simultaneously, gas or fluid is sucked into chamber 169 through intake valve 174, and the cycle is repeated.
  • a major advantage of the engines according to the present invention is that they can provide twice the work output per cycle with the same capacity synchronizer and with substantially less than a factor of two increase in overall size and weight, as compared to prior engines needing a bouncer compressor to supply return energy.
  • FIGS. 6 and 7. show pressure-volume curves for a prior engine having an output compressor and a bouncer compressor providing at least a portion of the return energy necessary for sustained operation of the engine.
  • FIG. 7 shows pressure-volume curves for the engines of the present invention. The notation ss represents the length of the swept stroke of the engine.
  • the compressor piston begins to compress fluid within the output compressor chamber, and the compressor piston continues to compress this fluid until point 2.
  • the output compressor discharge valves open and the continued movement of the compressor piston forces the compressed fluid from the output compressor at substantially constant pressure.
  • the compressor piston is caused to reverse direction, and the output compressor discharge valves close.
  • the pressure in the output compressor chamber rapidly drops as the volume increases behind the returning compressor piston.
  • the pressure within the output compressor chamber falls below atmospheric pressure, and the compressor inlet or suction valves open to admit the air which will be compressed and expelled during the next compressor stroke.
  • the work done on the air by the compressor piston during the compressor-compression stroke is proportional to the area under the curve 1, 2, 3.
  • the work returned to the system by the compressor piston during the compressor-expansion stroke is the area under the curve 3, 4, 1.
  • the area enclosed by the curve 1, 2, 3, 4 is a measure of the output work done by the output compressor piston during a single cycle.
  • the pressure within the bouncer compressor increases as the volume decreases along curve 2, 1. Also, the pressure within the bouncer compressor decreases as the volume increases, along curve 1, 2.
  • the work done by the bouncer compressor piston during a single cycle is the area beneath the curve 2, 1 while the work returned to the system by the bouncer compressor piston during the same cycle is the area beneath the curve 1, 2.
  • no network output is provided by the bouncer compressor piston since the area beneath these curves is substantially equal under the assumed ideal conditions.
  • one side of a compressor piston acts as an output compressor piston and the other side acts as a bouncer piston, and the network output per cycle is proportional to one times the area enclosed by the curve 1, 2, 3, 4.
  • FIG. 7 shows that if both sides of a compressor piston, such as sides 168 and 171 of piston 168, each act as output compressor pistons, as allowed by engines of the present invention, the network output per cycle is proportional to two times the area enclosed by the curve 1, 2, 3, 4 which is twice the network output as in the case represented by FIG. 6.
  • FIG. 8 shows the velocity versus stroke relationship between the power assemblies of engines according to the present invention, in solid line 176, and prior engines, in dashed line 177, both with respect to the swept stroke of the engine. Both curves start at the origin, as it represents the left endpoint of the power assembly where the power assembly is at zero velocity. Both curves return to the axis at the right endpoint of their power assemblies where again the velocities are zero.
  • This naturally equal stroke-time function may be particularly important in association with certain energy absorbing devices.
  • the energy absorbing device in the form of the electrical generator 151 associated with engine 150 it was noted above that substantially identical waveforms were produced upon the rightward and the leftward stroke of the engine. As discussed, this is particularly important in alternating current wave generators, such as used with engine 150, to minimize the DC component of the generator output and in pumps, such as used with engine 100, to minimize the size of the dampers of accumulators used with the pump.
  • this naturally equal stroke-time function may be important for compressors such as used with engine 160.
  • FIGS. 9 and 10 Embodiments FIGS. 9 and 10 show two single-acting power sections which may be placed on opposite ends of synchronizer housing 49 to provide power to the engine in place of the one double-acting power section 12 shown connected to one end of synchronizer housing 49 in FIG. 1.
  • power section 180 includes single-acting intake ports 41 and single-acting outlet ports 42 rather than the dual ports 41a, 41b and 42a, 42b of power section 12.
  • the power section 180 includes an integral, radially outwardly extending portion 187 which has a generally annular chamber 188 formed about the right end 189 of cylinder 16.
  • the chamber 188 communicates with the end portion 191 of cylinder 16 to the right of the inner face 184 of the piston 182.
  • the right end of housing portion 187, and thus the housing 15, are fastened to a wall 34 by a plurality of bolts, two of which are shown at 35, so the wall closes both the right end of chamber 188 and the left end of the synchronizer section 13.
  • Conventional one-way valves are positioned in the housing 15 and control the ingress of the air or fuel-air mixture into the chamber 188 of power section 180.
  • a second single-acting power stage is shown in FIG. in the form of a single-acting power section 200 having a penetrated cylinder head 34.
  • Power section 200 includes a single-acting power piston 202 which is again arranged for reciprocal motion within cylinder 16.
  • Power section 200 is substantially identical in construction and mode of operation to power section 180, except as noted herein and except that power section 200 is arranged to be alternately acting with power section 180. That is, power section 200 provides power to the engine on the power stroke of power piston 202 at the same time that power section 180 accepts power from the engine on the compression stroke of power piston 182.
  • Housing 187 of power section 200 is arranged to be connected to the right end of synchronizer housing 49.
  • End wall 51 is shown as a separate piece and no longer integrally formed-with sidewalls 52 of housing 49 of synchronizer section 13. Instead, end wall 51 and the remainder of housing 187 of power section 200 are arranged to be attached to sidewalls 52 of housing 49 in the same fashion as housing and wall 34 of power section 180 are attached to housing 49.
  • Piston 202 is then attached to move with shaft 48.
  • Shaft 48 penetrates cylinder head 34 of power section 200, as shaft 44 penetrates cylinder head 34 in FIG. 1, and shaft 48 is again available to attach to the reciprocally movable member of an energy absorbing device.
  • engines according to the present invention may have single-acting power section 180 attached to the left end of synchronizer section 13 and single-acting power section 200 coaxially attached to the right end of synchronizer section 13 and yet function in the same fashion as does engine 11. Further, the positions of power sections 180 and 200 may be reversed. Also, single-acting power sections, such as power section 180, may be placed coaxially upon both extreme ends of the engine, beyond the energy absorbing device, and yield the benefit that identical power sections may be used.
  • main pistons as used herein is meant to include only those pistons which perform the main or principal operating functions of the free piston engines of the present invention.
  • the main pistons should be distinguished from so called auxiliary pistons such as oil pump pistons, water pump pistons, fuel pump pistons, and the like which may also be used in or on engines of the present invention and which may move either with or in the opposite direction to the main pistons during operation of the engines of the present invention.
  • auxiliary oil pump piston could be attached to and moved with the walls 73, 74 of the synchronizer-balancer assembly 62, in the opposite direction to the main pistons, or the same oil pump piston could be attached to and moved with power assembly 43, in the same direction as the main pistons.
  • the weight of such an auxiliary piston must be considered as a part of the weight of the balancing and synchronizing assembly or the power assembly, as the case may be, in order to balance the engine.
  • main pistons as used herein should be distinguished from the term power assembly.
  • power assembly includes the main pistons, the movable member of the energy absorbing device, and the means for connecting the main pistons together and for interconnecting the main pistons with the movable member of the energy absorbing device.
  • the main pistons and the movable member of the energy absorbing device form parts of the power assembly and always move together as a unit within the engine of the present invention.
  • cam 131 of pump 104 shown in FIG. 3 may be designed to cause more than one pump stroke per power stroke of the free piston engine.
  • Cam 131 may also include more than two cam surfaces which may be arranged in such a phase relationship as to require a minimum accumulator size.
  • Many other pump configurations may be used in place of the preferred arrangement shown in FIG. 3.
  • power sections and 200 may both be double acting if the synchronizer-balancer is designed to have substantially twice the strength.
  • An unsymmetrical, synchronized, balanced, free piston engine adapted to drive a reciprocally movable member of an energy absorbing device comprising, in combination: an engine housing; means for defining a first power cylinder in the engine housing; means for defining a second power cylinder in the engine housing, with the second power cylinder being substantially coaxial to the first power cylinder; main piston means including a first power piston mounted in the first power cylinder for reciprocal movement therein along an axis substantially parallel to the central longitudinal axis of the first power cylinder, the first power piston defining a first combustion chamber with the first power cylinder, and including a second power piston mounted in the second power cylinder for reciprocal movement therein along an axis substantially parallel to the central longitudinal axis of the second power cylinder, the second power piston defining a second combustion chamber with the second power cylinder, the second combustion chamber being arranged to be alternately acting with the first combustion chamber; connection means, including shaft means, for connecting the main piston means, including the first power piston and the second power piston, to the
  • the pump includes at least one pumping chamber
  • the movable member includes at least one pumping plunger associated with the pumping chamber and a cam which causes the pumping plunger to move reciprocally within the pumping chamber in response to movement of the cam.
  • the energy absorbing device is a double-acting reciprocal compressor having a compressor housing with a compressor cylinder formed therein
  • the movable member is a compressor piston which is mounted in the compressor cylinder for reciprocal movement therein in a direction substantially parallel to the longitudinal axis of the compressor cylinder, the compressor piston defining at least first and second compressor chambers with the compressor housing and the compressor cylinder.
  • the means for defining the second power cylinder in the housing defines the second power cylinder to be adjacent to, coaxial with, and interconnected with the first power cylinder to form a doubleacting power cylinder, wherein the connection means interconnects the first power piston and the second power piston to form a double-acting power piston, and wherein the combination of the double-acting power cylinder and the double-acting power piston comprises a double-acting power section.
  • first power piston and the first power cylinder comprise a first single-acting power section, wherein the first single-acting power section is positioned adjacent an end of the engine, and wherein the second power piston and the second power cylinder comprise a second single-acting power section.
  • the improved free piston engine of claim 10 wherein the first combustion chamber is defined in the first power cylinder between the outer face of the first power piston and the closed outer end of the first power cylinder, and wherein the second combustion chamber is defined in the second power cylinder between the outer face of the second power piston and the closed outer end of the second power cylinder.
  • connection means being adapted for connecting to the movable member of an energy absorbing device located along said axis at one end of the engine beyond said power pistons and synchronizer-balancer assembly.

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Compressors, Vaccum Pumps And Other Relevant Systems (AREA)
US868008A 1969-10-21 1969-10-21 Balanced-free piston engine Expired - Lifetime US3610217A (en)

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US86800869A 1969-10-21 1969-10-21

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US (1) US3610217A (enrdf_load_stackoverflow)
JP (2) JPS5118566B1 (enrdf_load_stackoverflow)
CA (1) CA922998A (enrdf_load_stackoverflow)

Cited By (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3859966A (en) * 1973-02-16 1975-01-14 Anton Braun Linear balanced free piston machines
US4332219A (en) * 1980-11-18 1982-06-01 Ernesto Gonzalez Electrocombustion engine
US4763478A (en) * 1986-06-25 1988-08-16 Brown, Boveri & Cie Ag Method and device for driving a linearly movable component, especially the movable switch contact of an electric high-voltage circuit breaker
US4917335A (en) * 1988-03-31 1990-04-17 Gt-Devices Apparatus and method for facilitating supersonic motion of bodies through the atmosphere
US5540194A (en) * 1994-07-28 1996-07-30 Adams; Joseph S. Reciprocating system
US6105541A (en) * 1999-02-22 2000-08-22 Caterpillar, Inc. Free piston internal combustion engine with rotating piston
US6244226B1 (en) * 1999-08-06 2001-06-12 Caterpillar Inc. Free piston internal combustion engine with rotating piston
US6966281B1 (en) * 2004-05-05 2005-11-22 Hale James R Internal combustion device and methods of use
US20110203548A1 (en) * 2010-02-24 2011-08-25 Fillios Thomas L Plunger Motor
US8485146B2 (en) 2010-11-24 2013-07-16 Industrial Technology Research Institute Engine device
US9366199B2 (en) * 2014-05-09 2016-06-14 Ali Farzad Farzaneh Sliding engine with shaft on one or both ends for double or single ended combustion
US10641166B1 (en) 2018-12-03 2020-05-05 Aquarius Engines (A.M.) Ltd. Piston rod and free piston engine
US10968742B2 (en) 2014-04-24 2021-04-06 Aquarius Engines (A.M.) Ltd. Engine with work stroke and gas exchange through piston rod
US11008959B2 (en) 2019-06-28 2021-05-18 Aquarius Engines Central Europe Sp. z o.o. System and method for controlling engine using reference point
US11008864B2 (en) 2014-04-24 2021-05-18 Aquarius Engines (A.M.) Ltd. Engine with work stroke and gas exchange through piston rod
US11255405B2 (en) 2015-10-20 2022-02-22 Aquarius Engines (A.M.) Ltd. Vibration prevention in a linear actuator
US11346219B2 (en) 2014-04-24 2022-05-31 Aquarius Engines (A.M.) Ltd. Engine with work stroke and gas exchange through piston rod

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5676709U (enrdf_load_stackoverflow) * 1979-11-19 1981-06-23
JPH0389212U (enrdf_load_stackoverflow) * 1989-12-27 1991-09-11
JP4779881B2 (ja) * 2006-08-28 2011-09-28 マツダ株式会社 フリーピストンエンジン
CA2946504C (en) * 2014-04-24 2021-06-22 Shaul Yaakoby Free piston engine

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CA640650A (en) * 1962-05-01 F. Hobbs Howard Internal combustion engines and power transmission therefor
US662631A (en) * 1897-01-18 1900-11-27 Atlantic Motor Company Counterbalance for explosion-engines.
US1741731A (en) * 1925-08-19 1929-12-31 Nordensson Tom Knut Arfved Compressor driven by internal-combustion engines
US2407790A (en) * 1944-02-03 1946-09-17 Letourneau Inc Reciprocating pressure generator
DE1108002B (de) * 1954-08-31 1961-05-31 Aake Elvir Anderberg Dipl Ing Freiflugkolbenmotor zur Erzeugung elektrischer Energie
US2991773A (en) * 1958-07-03 1961-07-11 Citroen Sa Andre Free-piston machines

Cited By (23)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3859966A (en) * 1973-02-16 1975-01-14 Anton Braun Linear balanced free piston machines
US4332219A (en) * 1980-11-18 1982-06-01 Ernesto Gonzalez Electrocombustion engine
US4763478A (en) * 1986-06-25 1988-08-16 Brown, Boveri & Cie Ag Method and device for driving a linearly movable component, especially the movable switch contact of an electric high-voltage circuit breaker
EP0251147A3 (de) * 1986-06-25 1990-01-03 Asea Brown Boveri Aktiengesellschaft Verfahren und Vorrichtung zum Antrieb eines linear bewegbaren Bauelemetes, insbesondere des beweglichen Schaltkontaktes eines elektrischen Hochspannungs-Leistungsschalters
US4917335A (en) * 1988-03-31 1990-04-17 Gt-Devices Apparatus and method for facilitating supersonic motion of bodies through the atmosphere
US5540194A (en) * 1994-07-28 1996-07-30 Adams; Joseph S. Reciprocating system
US6105541A (en) * 1999-02-22 2000-08-22 Caterpillar, Inc. Free piston internal combustion engine with rotating piston
US6244226B1 (en) * 1999-08-06 2001-06-12 Caterpillar Inc. Free piston internal combustion engine with rotating piston
US6966281B1 (en) * 2004-05-05 2005-11-22 Hale James R Internal combustion device and methods of use
US20110203548A1 (en) * 2010-02-24 2011-08-25 Fillios Thomas L Plunger Motor
US8485146B2 (en) 2010-11-24 2013-07-16 Industrial Technology Research Institute Engine device
US10968742B2 (en) 2014-04-24 2021-04-06 Aquarius Engines (A.M.) Ltd. Engine with work stroke and gas exchange through piston rod
US11008864B2 (en) 2014-04-24 2021-05-18 Aquarius Engines (A.M.) Ltd. Engine with work stroke and gas exchange through piston rod
US11346219B2 (en) 2014-04-24 2022-05-31 Aquarius Engines (A.M.) Ltd. Engine with work stroke and gas exchange through piston rod
US11686199B2 (en) 2014-04-24 2023-06-27 Aquarius Engines (A.M.) Ltd. Engine with gas exchange through piston rod
US9366199B2 (en) * 2014-05-09 2016-06-14 Ali Farzad Farzaneh Sliding engine with shaft on one or both ends for double or single ended combustion
US11255405B2 (en) 2015-10-20 2022-02-22 Aquarius Engines (A.M.) Ltd. Vibration prevention in a linear actuator
US10641166B1 (en) 2018-12-03 2020-05-05 Aquarius Engines (A.M.) Ltd. Piston rod and free piston engine
US10968821B2 (en) 2018-12-03 2021-04-06 Aquarius Engines (A.M.) Ltd. Piston rod and free piston engine
US11346279B2 (en) 2018-12-03 2022-05-31 Aquarius Engines (A.M.) Ltd. Piston rod and free piston engine
US11655756B2 (en) 2018-12-03 2023-05-23 Aquarius Engines (A.M.) Ltd. Single air supply using hollow piston rod
US11008959B2 (en) 2019-06-28 2021-05-18 Aquarius Engines Central Europe Sp. z o.o. System and method for controlling engine using reference point
US11846241B2 (en) 2019-06-28 2023-12-19 Aquarius Engines Central Europe Sp. z o.o. System and method for controlling engine

Also Published As

Publication number Publication date
CA922998A (en) 1973-03-20
JPS5224163B1 (enrdf_load_stackoverflow) 1977-06-29
JPS5118566B1 (enrdf_load_stackoverflow) 1976-06-10

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