US3180078A - Combined internal combustion and hot-air engine - Google Patents

Combined internal combustion and hot-air engine Download PDF

Info

Publication number
US3180078A
US3180078A US103044A US10304461A US3180078A US 3180078 A US3180078 A US 3180078A US 103044 A US103044 A US 103044A US 10304461 A US10304461 A US 10304461A US 3180078 A US3180078 A US 3180078A
Authority
US
United States
Prior art keywords
engine
cylinder
cylinders
stirling
stage
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Lifetime
Application number
US103044A
Inventor
Liston Joseph
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Individual
Original Assignee
Individual
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Individual filed Critical Individual
Priority to US103044A priority Critical patent/US3180078A/en
Application granted granted Critical
Publication of US3180078A publication Critical patent/US3180078A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B41/00Engines characterised by special means for improving conversion of heat or pressure energy into mechanical power
    • F02B41/02Engines with prolonged expansion
    • F02B41/06Engines with prolonged expansion in compound cylinders
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02GHOT GAS OR COMBUSTION-PRODUCT POSITIVE-DISPLACEMENT ENGINE PLANTS; USE OF WASTE HEAT OF COMBUSTION ENGINES; NOT OTHERWISE PROVIDED FOR
    • F02G3/00Combustion-product positive-displacement engine plants
    • F02G3/02Combustion-product positive-displacement engine plants with reciprocating-piston engines

Definitions

  • the pistons and cylinders of the two stages are independent of each other, although the pistons are preferably operatively interconnected, most desirably by being associated with a common crankshaft. Operatively interconnecting the pistons of the two stages makes possible a predetermined distribution of torque impulses; and by properly arranging the cylinders of the two engines, the distribution of torque impulses can be made substantially uniform.
  • I provide, in the conduit through which exhaust gases from the first stage flow to the second stage, means for burning any fuel unburned in the first stage.
  • FIG. l is an isometric view, largely diagrammatic in Character, of a two-stage power plant wherein the Stirling engine is a two-cylinder, V-type engine disposed in the re ⁇ gion between the cylinders of a two-cylinder, in-line internal combustion engine of the four-stroke cycle type;
  • FIG. 2 is a section through the two cylinders of the Stirling engine incorporated in the power plant of FIG. l;
  • FIG. 3 is a longitudinal section through the same power plant in the plane of the cylinders of the internalcombustion engine
  • FIG. 4 is a diagrammatic view illustrating means for burning fuel unburned in the internal-combustion engine
  • FIG. 5 is an isometric view somewhat diagrammatic in Character, of a power plant embodying the invention and employing a single-cylinder, two-stroke cycle internal combustion engine as a first stage;
  • FIG. 6 is a diagrammatic view illustrating the form of a crankshaft for the power plant of FIG. 5.
  • the engine shown in FIGS. 1-3 comprises a crankcase 10 within which a crankshaft 11 is rotatably supported.
  • Two cylinders 12 and 13 of an internal combustion engine are mounted on the crankcase near the ends thereof and in a common plane. Between the two cylinders 12 and 13, the crankcase supports two cylinders 15 and 16 of a Stirling engine, such two cylinders being disposed at an angle to each other and symmetrically with respect to the common plane of the cylinders 12 and 13.
  • the cylinders 12 and 13 contain pistons 18 connected by connecting rods 19 to cranks 20 of the crankshaft 11, such cranks being coaxial with each other.
  • the cylinders 15 and 16 contain pistons 22 connected by connecting rods 23 with a common crank 24 coplanar with but diametrically opposite the cranks 20.
  • the head ends of the two cylinders 15 and 16 are interconnected by a transfer conduit 25 through which the gas trapped above the pistons 22, which gas constitutcs the working medium of the Stirling engine, is transferred back and forth between the cylinders as the crankshaft rotates.
  • the cylinder 15 constitutcs the hot space of the Stirling engine, and it, together with the adjacent end of the conduit 25, is provided with a jacket 26 connected through conduits 27 with the exhaust ports (not shown) of the cylinders 12 and 13.
  • the jacket 26 has an outlet opening communicating with an exhaust pipe 27.
  • the cylinder 16, which constitutcs the cold space of the Stirling engine shown, is provided with a coolant jacket 28, which desirably surrounds the adjacent end of the conduit 25 as well as the cylinder 16.
  • the jacket 28 may be embodied in the same coolant circulating system as that used to cool the first-stage cylinders 12 and 13; but if so, the jacket 28 should desirably receive cold coolant directly from the radiator so as to maintain the cylinder 16 as cool as possible.
  • a Stirling engine operates on a cycle in which the working medium is successively compressed isotherrr lly to minimum volume, heated at the minimum volufne, permitted to expand isothermally to maximum volume while doing work, and then cooled at the maximum volume.
  • the working medium is successively compressed isotherrr lly to minimum volume, heated at the minimum volufne, permitted to expand isothermally to maximum volume while doing work, and then cooled at the maximum volume.
  • there is more or less overlapping of successive steps of the cycle the extent of such overlapping depending on the particular design of the engine.
  • the Stirling engine shown by Way of example in the drawings provides considerable overlapping of successive cycle-Steps, but it possesses several advantages which tend to compensate for such loss in efficiency as results from the overlapping.
  • the crank 24 is at the lowermost point of its path of travel, the working medium trapped above the pistons 22 has its maximum volume, and the engine has therefore just completed its Working stroke.
  • the efficiency of a Stirling engine can be increased by providing a regenerator or heat sink in the passage through which the working medium flows between the hot and cold spaces of the engine.
  • a regenerator indicated by the reference numeral 30, is shown in FIG. 2 in the transfer conduit 25.
  • the regenerator may be any means which possesses adequate thermal capacity and a relatively large surface area and which offers little obstruction to the flow of gas through the conduit 25.
  • a mass of metal wool or a series of juxtaposed disks of fine- Wire mesh constitutes a suitable regenerator.
  • the specific power plant illustrated in the drawngs has several advantages, especially where the internal combustion engine is of the four-stroke cycle type and has two cylinders. Locating the Stirling engine, or at least the hot-space thereof, between two cylinders of the internal combustion engine facilitates the ducting through which the exhaust from the internal-combustion engine is conducted to such hot space. If, the two four-cycle cylinders 12 and 13 are arranged to fire alternately, the power plant provides a substantially uniform distribution of the torque impulses, the torque impulses of the Stirling engine, which occur at one-revolution intervals, alternating with the torque impulses of the two-cylinder internalcombustion engine, which in combination likewise occur at one-revolution intervals.
  • the exhaust strokes of the internal-combustion cylinders coincide approximately with the intervals in which the working medium of the Stirling engine is to be heated.
  • the primary inertia forces of the reciprocating parts produce no substantial rocking couples and can be effectively suppressed by the employment of appropriate counterweights on the crankshaft.
  • Flap valves 39 and 39' located at the junctions of the two branches 37 and 38 are employed to open one branch and close the other. Such flap valves may be operated automatically by means 40 responsive to the temperature of the exhaust gases leaving the internal combustion engine 35. When the temperature of the exhaust gases is relatively low, the valves 39 and 39' are positoned as shown to direct flow through the branch 38 which contains means for burning any unburned components in the exhaust gases. As shown, the branch 38 has an opening 42 for admitting the auxiliary air necessary to combustion and is also provided with an igniter 43, which may be a simple glow plug. In addition to the auxiliary air opening and igniter, or as an alternative for the igniter, the branch 38 contains a mass 44 of an oxidation catalyst.
  • the temperature-responsive means 40 will swing the valves 39 and 39' to close the branch 38 and open the branch 37, which provides free passage of the exhaust to the hotspace jacket 36 of the Stirling engine.
  • By-passing of hightemperature gases around the auxiliary air-opening 42 and the Catalyst 44 avoids their diluton and Cooling by air which would enter through the opening 42.
  • FIGS. 5 and 6 illustrate a power plant embodying the invention and suitable for incorporation of a single-cylinder two-stroke cycle internal combustion engine.
  • Such power plant comprises a crankcase supporting in coplanar relationship an intemal combustion cylinder 51 and the two cylinders 52 and 53 of a Stirling-cycle engine.
  • the cylinders 51 and 52 are provided respectively with coolant jackets 54 and 54', while the cylinder 53 is provided with a jacket 55 to which the exhaust from the cylinder 51 is conveyed through the branched conduit 37-38 of FIG. 4.
  • the two Stirling-cycle cylinders are interconnected at their head-ends by a transfer conduit
  • the power plant shown in FIG. 5 conveniently embodies a crankshaft 57 of the form shown diagrammatically in FIG. 6.
  • crankshaft has cranks 58, 59, and connected respectively through connecting rods to the pistons 61, 62, and 63 in the cylinders 51, 52, and 53.
  • the cranks are arranged at equal angular intervals about the axis of the crankshaft 57, with the Crank 59 leading and the crank 60 trailing the Crank 58 in rotation in the contemplated direction, which is the counterclockwise direction as indicated by the arrow in FIG. 6.
  • crankcase 50 of FIG. 5 may be divided intemally by partition means to provide a pressurized chamber with which the inner ends of the cylinders 52 and 53 communicate.
  • the invention of this application is not limited to any particular form or type for the internal combustion engine or the Stirling engine.
  • the two arrangements shown for purposes of illustrating the invention have certain advantages is respect to simplicity of construction, economy of manufacture, and dynamic balance, as well as other advantages.
  • the arrangements of the cylinders of a two-cylinder Stirling engine in a common plane, as in FIGS. 5 and 6, or perpendicularly to each other, as shown in FIGS. 1-3, may not be the Optimum arrangement from the standpoint of Stirling-engine efficiency; and if so, it would be possible to improve the eficiency of the Stirling engine by altering the effective angle between its two cylinders. Any such improvement, however, would be obtained at the expense of complicatng the problem of balancng inertia forces.
  • a two-stage power plant comprising an internalcombustion engine as a first stage and a Stirling-cycle engine as a second stage, said two engines having a common crankshaft, said Stirling engine having means providing intercommunicating heated and cooled chambers and including a cylinder and a piston reciprocable in the cylinder for confining a body of gaseous working medium, said internal-combustion engine including at least one cylinder and a piston reciprocable therein, said crankshaft having a separate crank for each of said cylinders, connecting rods operatively interconnecting said cranks respectively with said pistons, ducting for conveying exhaust gases from the intemal-combustion engine into heat transferring relation to said heated chamber, and means located in said ducting for burning unburned components of said exhaust gases.
  • a two stage power plant comprising an internalcombustion engine as a first stage and a Stirling-cycle engine as a second stage, said intemal-combustion engine being of the four-stroke cycle type and including two coplanar cylinders, said Stirling-cycle engine having a pair of cylinders disposed between the two intemal-combustion engine cylinders and arranged at an angle to each other generally symmetrically relative to the common plane of the intemal-combustion engine cylinders, a piston in each of said cylinders, a common crankshaft for the two engines, said crankshaft having two coaxial end cranks connected by connecting rods to the pistons in the internal-combustion engine cylinders and an intermediate Crank spaced substantially l from said end cranks and connected by connecting rods to the pistons in the cylinders of the Stirling-cycle engine, a transfer conduit nterconnecting the head ends of the latter cylinders, a jacket for one of the cylinders of the Stirling-cycle engine, ducting for
  • a two stage power plant comprising an intemalcombustion engine as a first stage and a Stirling-cycle engine as a second stage, said Stirling-cycle engine comprising two cylinders and a transfer conduit interconnecting their head ends, pistons in said cylinders, said internalcombustion engine being of the two-stroke cycle type and having a single cylinder containing a piston, all three of said cylinders being at least approximately coplanar, a common crankshaft for said engines, said crankshaft having three cranks spaced at substantially equal angular intervals about the crankshaft axis and connected by connecting rods to the three pistons respectively, one of said Stirling-engine cylinders being provided with a jacket, ducting for conveying exhaust gases from the intemaloombustion engine to said jacket, and means located in said ducting for burning unbumed components of said exhaust gases.

Description

DLAHUH ROOM-- 0-280. OR 3.180.078 SR ,April 27, 1965 J. LlsToN 3.180,078
COMBINED INTERNAL COMBUSTION AND HOT AIR ENGINE Filed April 14, 1961 'lasera /s ro/v,
'I mmvmn.
,April 27, 1965 J. Lls'roN 3,180073 COMBINED INTERNAL COMBUSTION AND HOT-AIR ENGINE Filed April 14. 1981 5 Sheets-Sheet 2 A rromvef's.
April 27, 1965 J. LlsToN 3,180,078
COMBINED INTERNAL COMBUSTION AND HOT-AIR ENGINE Filed April 14. 1961 3 Sheets-Sheet S Arroemsrs.
United States Patent O 3.180,078 COMBINED INTERNAL COMBUSTION AND HOT-AIR ENGINE Joseph Liston, Lafayette, Ind. (900 Robinson St., West Lafayette, Ind.) Filed Apr. 14, 1961, Ser. No. 103,044 4 Claims. (Cl. 60-14) The subject matter of this invention is a two-stage power plant or prime mover, the first stage of which is an internal combustion engine and the second stage of which is a hot-air or Stirling-cycle engine operated by heat derived from the gases exhausted by the first stage. An arrangement heretofore proposed for utilizing in a Stirling engine heat contained in the exhaust gases from an internal combustion engine employed a cylinder and piston combination in which the head-end of the cylinder functioned as a combustion space, as in an ordinary internal combustion engine, and the crank-end of the cylinder functioned as the cold space of a Stirling engine. In that arrangement, inward movement of the piston under pressure generated by combustion compressed the gaseous working medium of the Stirling engine and displaced it into a heat-exchanger where it absorbed heat from the gases exhausted from the head-end of the cylinder. After bottom dead-center, the compressed and heated working medium expanded into the crank-end of the cylinder impelling the piston outwardly. Such an arrangement has several disadvantages. In the first place, there is an inevitable and undesirable transfer of heat from the combustion space to the Stirling-engine cold space by conduction through the piston and cylinder wall. In the second place, it is desirable that the fixed quantity of working medium employed in the Stirlng engine be maintained under substantial pressure, and the low fluid pressures which would exist in the combustion space just before compression and during the initial stages thereof would contribute to the escape of the working medium past the piston. Again, since a single piston is used, Variation in the displacements of the two engines could be obtained only by employing a piston and cylinder each having portions of different diameter, which would result in complicating the construction, increasing cost, and increasing the weight of the piston. Still further, a reasonably uniform distribution of torque impulses would be obtained only if the head-end of the cylinder operated on a two-stroke cycle, for a Stirling engine delivers a torque impulse for each revolution of the crankshaft.
It is an object of this invention to produce a prime mover having an internal-combustion engine as a first stage and a Stirling engine as a second stage and to utilize in the Stirling engine the heat contained in or derivable from the exhaust gases of the internal-combustion engine. Another object of the invention is to make available for use in the Stirling engine heat derived from the combustion of unburned fuel contained in the exhaust from the internal-combustion engine.
According to one feature of the present invention, the pistons and cylinders of the two stages are independent of each other, although the pistons are preferably operatively interconnected, most desirably by being associated with a common crankshaft. Operatively interconnecting the pistons of the two stages makes possible a predetermined distribution of torque impulses; and by properly arranging the cylinders of the two engines, the distribution of torque impulses can be made substantially uniform.
In accordance with another feature of my invention, I provide, in the conduit through which exhaust gases from the first stage flow to the second stage, means for burning any fuel unburned in the first stage.
Other objects and features of my invention will become 3,l80,078 Patented Apr. 27, 1965 ICC apparent from the following more detailed description and from the accompanying drawings in which:
FIG. l is an isometric view, largely diagrammatic in Character, of a two-stage power plant wherein the Stirling engine is a two-cylinder, V-type engine disposed in the re` gion between the cylinders of a two-cylinder, in-line internal combustion engine of the four-stroke cycle type;
FIG. 2 is a section through the two cylinders of the Stirling engine incorporated in the power plant of FIG. l;
FIG. 3 is a longitudinal section through the same power plant in the plane of the cylinders of the internalcombustion engine;
FIG. 4 is a diagrammatic view illustrating means for burning fuel unburned in the internal-combustion engine;
FIG. 5 is an isometric view somewhat diagrammatic in Character, of a power plant embodying the invention and employing a single-cylinder, two-stroke cycle internal combustion engine as a first stage; and
FIG. 6 is a diagrammatic view illustrating the form of a crankshaft for the power plant of FIG. 5.
The engine shown in FIGS. 1-3 comprises a crankcase 10 within which a crankshaft 11 is rotatably supported. Two cylinders 12 and 13 of an internal combustion engine are mounted on the crankcase near the ends thereof and in a common plane. Between the two cylinders 12 and 13, the crankcase supports two cylinders 15 and 16 of a Stirling engine, such two cylinders being disposed at an angle to each other and symmetrically with respect to the common plane of the cylinders 12 and 13. The cylinders 12 and 13 contain pistons 18 connected by connecting rods 19 to cranks 20 of the crankshaft 11, such cranks being coaxial with each other. The cylinders 15 and 16 contain pistons 22 connected by connecting rods 23 with a common crank 24 coplanar with but diametrically opposite the cranks 20.
The head ends of the two cylinders 15 and 16 are interconnected by a transfer conduit 25 through which the gas trapped above the pistons 22, which gas constitutcs the working medium of the Stirling engine, is transferred back and forth between the cylinders as the crankshaft rotates. As shown, the cylinder 15 constitutcs the hot space of the Stirling engine, and it, together with the adjacent end of the conduit 25, is provided with a jacket 26 connected through conduits 27 with the exhaust ports (not shown) of the cylinders 12 and 13. The jacket 26 has an outlet opening communicating with an exhaust pipe 27.
The cylinder 16, which constitutcs the cold space of the Stirling engine shown, is provided With a coolant jacket 28, which desirably surrounds the adjacent end of the conduit 25 as well as the cylinder 16. The jacket 28 may be embodied in the same coolant circulating system as that used to cool the first- stage cylinders 12 and 13; but if so, the jacket 28 should desirably receive cold coolant directly from the radiator so as to maintain the cylinder 16 as cool as possible.
Ideally, a Stirling engine operates on a cycle in which the working medium is successively compressed isotherrr lly to minimum volume, heated at the minimum volufne, permitted to expand isothermally to maximum volume while doing work, and then cooled at the maximum volume. In an actual engine, there is more or less overlapping of successive steps of the cycle, the extent of such overlapping depending on the particular design of the engine. The Stirling engine shown by Way of example in the drawings, provides considerable overlapping of successive cycle-Steps, but it possesses several advantages which tend to compensate for such loss in efficiency as results from the overlapping. As shown in FIG. 2, the crank 24 is at the lowermost point of its path of travel, the working medium trapped above the pistons 22 has its maximum volume, and the engine has therefore just completed its Working stroke. Compression of the working medium will occur as the crank 24 moves from its lowermost position to its uppermost position, when the working stroke and expansion of the working medium will begin. As will be clear from FIG. 2, where the crankshaft is indicated as rotating in a clockwise direction, movement of the Crank 24 from its lowermost position will be accompanied by outward movement (relative to the crankshaft) of the piston in cylinder and inward movement of the piston in cylinder 16, and a displacement of the working medium toward the cooled cylinder will therefore result. Such displacement will continue for approximately onefourth of a revolution, or until the time when the piston in cylinder 16 will have reversed its direction and accelerated to an outward Velocity which equals and begins to exceed that of the decelerating piston in cylinder 15. Thereafter, the displacement of the working medium will be in the general direction of the heated space of the engine, and such displacement will continue for about one-half a revolution, when both pistons will be moving inwardly and the piston in cylinder 16 attains an inward Velocity which equals and begins to exceeds that of the piston in cylinder 15, whereupon the displacement of the working medium will be reversed. It is thus apparent that in the Stirling engine shown the working medium will be heated during the last stage of its compression and the first stage of its expansion and cooled during the final stage of its expansion and the initial stage of its compression.
The efficiency of a Stirling engine can be increased by providing a regenerator or heat sink in the passage through which the working medium flows between the hot and cold spaces of the engine. Such a regenerator, indicated by the reference numeral 30, is shown in FIG. 2 in the transfer conduit 25. The regenerator may be any means which possesses adequate thermal capacity and a relatively large surface area and which offers little obstruction to the flow of gas through the conduit 25. A mass of metal wool or a series of juxtaposed disks of fine- Wire mesh constitutes a suitable regenerator.
The specific power plant illustrated in the drawngs has several advantages, especially where the internal combustion engine is of the four-stroke cycle type and has two cylinders. Locating the Stirling engine, or at least the hot-space thereof, between two cylinders of the internal combustion engine facilitates the ducting through which the exhaust from the internal-combustion engine is conducted to such hot space. If, the two four- cycle cylinders 12 and 13 are arranged to fire alternately, the power plant provides a substantially uniform distribution of the torque impulses, the torque impulses of the Stirling engine, which occur at one-revolution intervals, alternating with the torque impulses of the two-cylinder internalcombustion engine, which in combination likewise occur at one-revolution intervals. Further, the exhaust strokes of the internal-combustion cylinders coincide approximately with the intervals in which the working medium of the Stirling engine is to be heated. The primary inertia forces of the reciprocating parts produce no substantial rocking couples and can be effectively suppressed by the employment of appropriate counterweights on the crankshaft.
For known reasons, it is desirable that the gaseous working medium of a Stirling engine be maintained under a substantial pressure, and to lessen the possibility of the escape of the working medium past the pistons, as well as for other reasons, it is desirable to maintan the inner faces of the pistons under fluid pressure comparable to the average pressure of the working medium. I have therefore shown (FIG. 3) the crankcase 10 as provided with spaced partitons 32 which are located on opposite sides of the crank 24 and which cooperate with the pistons and the walls of the crankcase to define an enclosed space the gas n which may be maintained under appropriate pressure in any convenient manner.
In an internal-combustion engine operating under varying speeds and loads, wide variations occur in the temperature of the exhaust gases; and when the exhaust gases are used to heat the hot space of a Stirling engine, the output of the latter engine will vary with the temperature of the exhaust gases. Low-temperature exhaust gases from an internal combustion engine normally contain a substantial amount of unbumed fuel which, in accordance with my invention. I employ to raise the temperature that otherwise would exist in the hot space of the Stirling engine. One arrangement for accomplishing that purpose is indicated diagrammatically in FIG. 4, where the exhaust gases from an internal combustion engine are shown as being conducted to the hot-space jacket 36 of a Stirling engine through a conduit having two branches 37 and 38. Flap valves 39 and 39' located at the junctions of the two branches 37 and 38 are employed to open one branch and close the other. Such flap valves may be operated automatically by means 40 responsive to the temperature of the exhaust gases leaving the internal combustion engine 35. When the temperature of the exhaust gases is relatively low, the valves 39 and 39' are positoned as shown to direct flow through the branch 38 which contains means for burning any unburned components in the exhaust gases. As shown, the branch 38 has an opening 42 for admitting the auxiliary air necessary to combustion and is also provided with an igniter 43, which may be a simple glow plug. In addition to the auxiliary air opening and igniter, or as an alternative for the igniter, the branch 38 contains a mass 44 of an oxidation catalyst. Most oxidation catalysts which have been used to promote the combustion of unburned components in exhaust gases operate most effectively at relatively high temperatures; and while such a Catalyst may eventually attain an effective temperature as a result of the combustion it induces, the use of an igniter 43 to initiate combustion and promote rapid rise in the temperature-of the Catalyst 44 is usually desirable.
If the internal combustion engine 35 of FIG. 4 is operating under conditions which result in high exhaust-gas temperature and substantially complete fuel consumption, the temperature-responsive means 40 will swing the valves 39 and 39' to close the branch 38 and open the branch 37, which provides free passage of the exhaust to the hotspace jacket 36 of the Stirling engine. By-passing of hightemperature gases around the auxiliary air-opening 42 and the Catalyst 44 avoids their diluton and Cooling by air which would enter through the opening 42.
FIGS. 5 and 6 illustrate a power plant embodying the invention and suitable for incorporation of a single-cylinder two-stroke cycle internal combustion engine. Such power plant comprises a crankcase supporting in coplanar relationship an intemal combustion cylinder 51 and the two cylinders 52 and 53 of a Stirling-cycle engine. The cylinders 51 and 52 are provided respectively with coolant jackets 54 and 54', while the cylinder 53 is provided with a jacket 55 to which the exhaust from the cylinder 51 is conveyed through the branched conduit 37-38 of FIG. 4. The two Stirling-cycle cylinders are interconnected at their head-ends by a transfer conduit The power plant shown in FIG. 5 conveniently embodies a crankshaft 57 of the form shown diagrammatically in FIG. 6. Such crankshaft has cranks 58, 59, and connected respectively through connecting rods to the pistons 61, 62, and 63 in the cylinders 51, 52, and 53. The cranks are arranged at equal angular intervals about the axis of the crankshaft 57, with the Crank 59 leading and the crank 60 trailing the Crank 58 in rotation in the contemplated direction, which is the counterclockwise direction as indicated by the arrow in FIG. 6.
Like the crankcase 10 of FIGS. l-4, and for the same purpose, the crankcase 50 of FIG. 5 may be divided intemally by partition means to provide a pressurized chamber with which the inner ends of the cylinders 52 and 53 communicate.
In the crankshaft position shown in FIG. 6, the piston 61 in the cylinder 51 has just completed its power stroke and the working medium of the Stirling engine is at minimum volume. During the approximately 90 of crankshaft rotation prior to attainment of the crankshaft position indicated in FIG. 6, the working medium of the Stirling engine was being displaced from the cold cylinder 52 to the hot cylinder 53, and displacement in that sense will Continue for approximately an additional 90 of crankshaft rotation, whereupon the ow of the working medium will be reversed and displacement from the hot cylinder to the cold cylinder will occur. As the heated working medium begins to expand following attainment of the crankshaft position shown in FIG. 6, it will perform work on the piston 63 with the result that a torque impulse will be imposed on the crank 60. During the working stroke of the piston 63 the piston 61 will be compressing the charge in the cylinder 51. Charge-compression will be completed after 180 of crankshaft revolution from the position shown in FIG. 6 at which time the working medium of the Stirling engine will have attained its maximum volume.
It will thus be obvious that in the power plant of FIGS. 5 and 6 the respective torque impulses of the two-stroke cycle internal combustion engine 51 and of the Stirling engine will be substantially equally spaced. By suitable coordination of the throws of the cranks 58, 59, and 60 and the masses of the pistons 61, 62, and 63, primary and secondary inertia forces can be balanced.
It may be noted that in its broad aspect the invention of this application is not limited to any particular form or type for the internal combustion engine or the Stirling engine. The two arrangements shown for purposes of illustrating the invention have certain advantages is respect to simplicity of construction, economy of manufacture, and dynamic balance, as well as other advantages. The arrangements of the cylinders of a two-cylinder Stirling engine in a common plane, as in FIGS. 5 and 6, or perpendicularly to each other, as shown in FIGS. 1-3, may not be the Optimum arrangement from the standpoint of Stirling-engine efficiency; and if so, it would be possible to improve the eficiency of the Stirling engine by altering the effective angle between its two cylinders. Any such improvement, however, would be obtained at the expense of complicatng the problem of balancng inertia forces.
I claim as my invention:
1. A two-stage power plant comprising an internalcombustion engine as a first stage and a Stirling-cycle engine as a second stage, said two engines having a common crankshaft, said Stirling engine having means providing intercommunicating heated and cooled chambers and including a cylinder and a piston reciprocable in the cylinder for confining a body of gaseous working medium, said internal-combustion engine including at least one cylinder and a piston reciprocable therein, said crankshaft having a separate crank for each of said cylinders, connecting rods operatively interconnecting said cranks respectively with said pistons, ducting for conveying exhaust gases from the intemal-combustion engine into heat transferring relation to said heated chamber, and means located in said ducting for burning unburned components of said exhaust gases.
2. A two stage power plant, comprising an internalcombustion engine as a first stage and a Stirling-cycle engine as a second stage, said intemal-combustion engine being of the four-stroke cycle type and including two coplanar cylinders, said Stirling-cycle engine having a pair of cylinders disposed between the two intemal-combustion engine cylinders and arranged at an angle to each other generally symmetrically relative to the common plane of the intemal-combustion engine cylinders, a piston in each of said cylinders, a common crankshaft for the two engines, said crankshaft having two coaxial end cranks connected by connecting rods to the pistons in the internal-combustion engine cylinders and an intermediate Crank spaced substantially l from said end cranks and connected by connecting rods to the pistons in the cylinders of the Stirling-cycle engine, a transfer conduit nterconnecting the head ends of the latter cylinders, a jacket for one of the cylinders of the Stirling-cycle engine, ducting for conveying exhaust gases to said jacket from the cylinders of the internal-combustion engine, means located in said ducting for burning unburned components of said exhaust gases and means for cooling the other cylinder of the Stirling-cycle engine.
3. A two stage power plant, comprising an intemalcombustion engine as a first stage and a Stirling-cycle engine as a second stage, said Stirling-cycle engine comprising two cylinders and a transfer conduit interconnecting their head ends, pistons in said cylinders, said internalcombustion engine being of the two-stroke cycle type and having a single cylinder containing a piston, all three of said cylinders being at least approximately coplanar, a common crankshaft for said engines, said crankshaft having three cranks spaced at substantially equal angular intervals about the crankshaft axis and connected by connecting rods to the three pistons respectively, one of said Stirling-engine cylinders being provided with a jacket, ducting for conveying exhaust gases from the intemaloombustion engine to said jacket, and means located in said ducting for burning unbumed components of said exhaust gases.
4. A power plant as set forth in claim 3 with the addition that said internal-combustion engine cylinder and said jacketed cylinder of the Stirling-engine are located on opposite sdes of the other Stirling-engine cylinder.
References Cited by the Examiner UNITED STATES PATENTS 2,196,979 4/40 Campbell 60-14 2,590,5l9 3/52 Du Pre 60-24 2,6l6,250 11/52 YZer 60-24 2,907,169 10/59 Newton 60-24 EDGAR W. GEOGHEGAN, Primary Examiner.
SAMUEL LEVINE, ROBERT R. BUNEVICH, I ULUS E. WEST, Examiners.

Claims (1)

1. A TWO-STAGE POWER PLANT COMPRISING AN INTERNALCOMBUSTION ENGINE AS A FIRST STAGE AND A STIRLING-CYCLE ENGINE AS A SECOND STAGE, SAID TWO ENGINES HAVING A COMMON CRANKSHAFT, SAID STIRLING ENGINE HAVING MEANS PROVIDING INTERCOMMUNICATING HEATED AND COOLED CHAMBERS AND INCLUDING A CYLINDER AND A PISTON RECIPROCABLE IN THE CYLINDER FOR CONFINING A BODY OF GASEOUS WORKING MEDIUM, SAID INTERNAL-COMBUSTION ENGINE INCLUDING AT LEAST ONE CYLINDER AND A PISTON RECIPROCABLE THEREIN, SAID CRANKSHAFT HAVING A SEPARATE CRANK FOR EACH OF SAID CYLINDERS, CONNECTING RODS OPERATIVELY INTERCONNECTING SAID CRANKS RESPECTIVELY WITH SAID PISTONS, DUCTING FOR CONVEYING EXHAUST GASES FROM THE INTERNAL-COMBUSTION ENGINE INTO HEAT TRANSFERRING RELATION TO SAID HEATED CHAMBER, AND MEANS LOCATED IN SAID DUCTING FOR BURNING UNBURNED COMPONENTS OF SAID EXHAUST GASES.
US103044A 1961-04-14 1961-04-14 Combined internal combustion and hot-air engine Expired - Lifetime US3180078A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US103044A US3180078A (en) 1961-04-14 1961-04-14 Combined internal combustion and hot-air engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US103044A US3180078A (en) 1961-04-14 1961-04-14 Combined internal combustion and hot-air engine

Publications (1)

Publication Number Publication Date
US3180078A true US3180078A (en) 1965-04-27

Family

ID=22293058

Family Applications (1)

Application Number Title Priority Date Filing Date
US103044A Expired - Lifetime US3180078A (en) 1961-04-14 1961-04-14 Combined internal combustion and hot-air engine

Country Status (1)

Country Link
US (1) US3180078A (en)

Cited By (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3513659A (en) * 1968-02-02 1970-05-26 Mc Donnell Douglas Corp Stirling cycle amplifying machine
US3852961A (en) * 1972-02-19 1974-12-10 United Stirling Ab & Co Heat exchanger pre-heating combustion air in a stirling cycle engine
US3867816A (en) * 1970-11-04 1975-02-25 George M Barrett Low pollution reciprocating heat engine
US3961483A (en) * 1975-07-03 1976-06-08 The Boeing Company Composite cycle engine
US4057040A (en) * 1976-04-12 1977-11-08 Wax Archie E Internal combustion engine system
US4121423A (en) * 1977-05-31 1978-10-24 Automotive Propulsion Laboratories, Ltd. Compound internal-combustion hot-gas engines
US4382362A (en) * 1979-08-28 1983-05-10 Mortel Antonius M External combustion engine
US4638635A (en) * 1981-11-05 1987-01-27 Nam Chul W Internal combustion engine system
EP0239560A1 (en) * 1986-03-17 1987-09-30 Helmut G. Dr. Brücker Two-stroke internal-combustion engine with reciprocating pistons
US20050167173A1 (en) * 2003-11-20 2005-08-04 Michael Hoetger Vehicle with combustion engine and auxiliary power unit
FR2905728A1 (en) * 2006-09-11 2008-03-14 Frederic Thevenod HYBRID ENGINE WITH EXHAUST HEAT RECOVERY
US20090013686A1 (en) * 2006-02-02 2009-01-15 Hiroshi Yaguchi Exhaust heat recovery apparatus
WO2011154622A1 (en) 2010-06-11 2011-12-15 Bernard Macarez Heat-exchanging cylinder head

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2196979A (en) * 1936-05-09 1940-04-16 James F Campbell Apparatus for power generation
US2590519A (en) * 1948-01-21 1952-03-25 Hartford Nat Bank & Trust Co Hot-gas engine or refrigerator
US2616250A (en) * 1949-08-09 1952-11-04 Hartford Nat Bank & Trust Co Cylinder head for hot-gas reciprocating engines
US2907169A (en) * 1957-12-10 1959-10-06 Alwin B Newton Hot fluid engine with movable regenerator

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2196979A (en) * 1936-05-09 1940-04-16 James F Campbell Apparatus for power generation
US2590519A (en) * 1948-01-21 1952-03-25 Hartford Nat Bank & Trust Co Hot-gas engine or refrigerator
US2616250A (en) * 1949-08-09 1952-11-04 Hartford Nat Bank & Trust Co Cylinder head for hot-gas reciprocating engines
US2907169A (en) * 1957-12-10 1959-10-06 Alwin B Newton Hot fluid engine with movable regenerator

Cited By (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3513659A (en) * 1968-02-02 1970-05-26 Mc Donnell Douglas Corp Stirling cycle amplifying machine
US3867816A (en) * 1970-11-04 1975-02-25 George M Barrett Low pollution reciprocating heat engine
US3852961A (en) * 1972-02-19 1974-12-10 United Stirling Ab & Co Heat exchanger pre-heating combustion air in a stirling cycle engine
US3961483A (en) * 1975-07-03 1976-06-08 The Boeing Company Composite cycle engine
US4057040A (en) * 1976-04-12 1977-11-08 Wax Archie E Internal combustion engine system
US4121423A (en) * 1977-05-31 1978-10-24 Automotive Propulsion Laboratories, Ltd. Compound internal-combustion hot-gas engines
US4382362A (en) * 1979-08-28 1983-05-10 Mortel Antonius M External combustion engine
US4638635A (en) * 1981-11-05 1987-01-27 Nam Chul W Internal combustion engine system
EP0239560A1 (en) * 1986-03-17 1987-09-30 Helmut G. Dr. Brücker Two-stroke internal-combustion engine with reciprocating pistons
US20050167173A1 (en) * 2003-11-20 2005-08-04 Michael Hoetger Vehicle with combustion engine and auxiliary power unit
US7464550B2 (en) * 2003-11-20 2008-12-16 Amovis Gmbh Vehicle with combustion engine and auxiliary power unit
US20090013686A1 (en) * 2006-02-02 2009-01-15 Hiroshi Yaguchi Exhaust heat recovery apparatus
US8166759B2 (en) * 2006-02-02 2012-05-01 Toyota Jidosha Kabushiki Kaisha Exhaust heat recovery apparatus
FR2905728A1 (en) * 2006-09-11 2008-03-14 Frederic Thevenod HYBRID ENGINE WITH EXHAUST HEAT RECOVERY
WO2011154622A1 (en) 2010-06-11 2011-12-15 Bernard Macarez Heat-exchanging cylinder head

Similar Documents

Publication Publication Date Title
US3623463A (en) Internal combustion engine
US3180078A (en) Combined internal combustion and hot-air engine
US6722127B2 (en) Split four stroke engine
US4159700A (en) Internal combustion compound engines
US4022167A (en) Internal combustion engine and operating cycle
US4791787A (en) Regenerative thermal engine
US4535592A (en) Internal combustion engine having an exhaust gas turbine
US5894729A (en) Afterburning ericsson cycle engine
US3996745A (en) Stirling cycle type engine and method of operation
US4936262A (en) Regenerative thermal engine
WO2009066178A2 (en) Heat engines
US3895620A (en) Engine and gas generator
US4121423A (en) Compound internal-combustion hot-gas engines
US3527049A (en) Compound stirling cycle engines
US3786631A (en) Nitrogen vapor engine
US4069671A (en) Stirling engine combustion assembly
US3886734A (en) Continuous combustion engine
US4008574A (en) Power plant with air working fluid
Flynn Jr et al. GMR Stirling Thermal Engine part of the Stirling engine story—1960 chapter
US6314925B1 (en) Two-stroke internal combustion engine with recuperator in cylinder head
CA1209925A (en) Internal combustion engine and operating cycle
US4599863A (en) Compound internal combustion and external combustion engine
US3009315A (en) Heat engines operating on the stirling or ericsson heat cycles
US967828A (en) Compound internal-combustion engine.
US3220177A (en) Thermodynamic reciprocating machine of the displacer-piston type