US2876751A - Synchronizing device for free piston engines - Google Patents

Synchronizing device for free piston engines Download PDF

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Publication number
US2876751A
US2876751A US653815A US65381557A US2876751A US 2876751 A US2876751 A US 2876751A US 653815 A US653815 A US 653815A US 65381557 A US65381557 A US 65381557A US 2876751 A US2876751 A US 2876751A
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rack
pistons
compressor
flexible
free piston
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US653815A
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Jr C Paul Kolthoff
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Navistar Inc
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International Harverster Corp
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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01BMACHINES OR ENGINES, IN GENERAL OR OF POSITIVE-DISPLACEMENT TYPE, e.g. STEAM ENGINES
    • F01B11/00Reciprocating-piston machines or engines without rotary main shaft, e.g. of free-piston type
    • F01B11/004Reciprocating-piston machines or engines without rotary main shaft, e.g. of free-piston type in which the movement in the two directions is obtained by two single acting piston motors, each acting in one direction
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01BMACHINES OR ENGINES, IN GENERAL OR OF POSITIVE-DISPLACEMENT TYPE, e.g. STEAM ENGINES
    • F01B9/00Reciprocating-piston machines or engines characterised by connections between pistons and main shafts and not specific to preceding groups
    • F01B9/04Reciprocating-piston machines or engines characterised by connections between pistons and main shafts and not specific to preceding groups with rotary main shaft other than crankshaft
    • F01B9/047Reciprocating-piston machines or engines characterised by connections between pistons and main shafts and not specific to preceding groups with rotary main shaft other than crankshaft with rack and pinion

Description

March 10, 1959 c@ P. KOLTHOFF, JR
SYNCHRONIZING DEVICE FOR FREE PISTON ENGINES Filed April 19, 1957 INVENTOR. C'Paa/K BYP *SYNCHRONIZING DEVICE FORFREE PISTON ENGINES C. lanl Koltholf, Jr., Naperville, 11]., assignor to Interim-- honal Harvester Company, Chicago, llli, a corporation ofNew Jersey Application April 19, 1957, Serial No. 653,815
Claims. (Cl. 123-46):
This invention relates to a synchronizing device for free piston engines. More particularly the invention relates to a free piston synchronizing device with flexiblesynchronizing rack elements.
In a conventional free piston engine, power pistons are freely mounted for reciprocation within a cylinder. The cylinder includes a combustion chamber. and during the power stroke the pistonsare moved in an outward direction. The power pistons are connected to compressor pistons which operate in compression chambers to bring the pistons back to their. original starting position. Thus, the pistons are freely mounted in the cylinder and generally in devices of this type power is derived from the exhaust gases rather than from the direct'mechanical connection to the freely moving pistons. It is, of, course, necessary to properly synchronize the movement of the free pistons and that is generally accomplished by a rack and pinion arrangementwhich positively synchronizes the movement of the free pistons. so
that they are constantly in phase. Under: certain conditions, power also may. be'derived from the racks where such power delivery is desired. The. conventional: free piston engine has the racks connectedto the compressor piston and the pinionv which engages the. racks is. ar ranged so that a movement of one pistoncauses. a cor= responding movement of the other piston relative to the center line of the engine. It' is, of course, readily apparent that during the operation of the engine the racks are constantly in motion. Generally fine tolerances must be held in the manufacture of the engine; to; assure that;
the synchronizing racks are in precision sliding contact withthe guides on which they are supported, so that" whipping or blending of the racks is eliminated-during the constant reciprocation which takes place; Duev totolerance build-ups, it is extremely difficult toah'old the close tolerances normally necessarywith the usual rigid type of rack element. As a result, malfunction canreadily occur. in the synchronizing mechanism of a free piston engine. It is a prime object ofthis invention therefore to eliminate the service problems usually occurring with conventional;
synchronizing mechanisms by the utilizationv of flexible racks which can, readily accommodate slight misalignments between the racks, guide elements, andmoving pistons so that the deleterious effects. of such misalignments are avoided.
Still another object is to providev a pair of. flexible rack elements for the synchronizer ofafree piston engine, the rack elements having flexible portions adjacent the compressor pistons arranged toaccommodatemisalign ment which may occur during construction. or the nor-- mal operation of the engine.
A more specific object is the provision. of improved rack elements for free piston engine synchronizers, the rack elements including reduced diameter portions permitting flexible movement oftheraclrelements with respect to the rack guides and the compressorv pistons to which the rack elements are attached.
.These'and further objects will. become. morereadily 2% apparent from. a reading of the: specification when ex= emitted in. connection with the accompanying sheet ofdrawings;
In the drawings:
Figure 1 is a cross-sectional view showing the upper half of a free piston engine embodying the invention;
Figure 2 is a cross-sectional view taken. particularly along the line. 22 of Figurev 1;
Figure 3 is a; cross-sectional view through an improved. rack element: ofa synchronizer mechanism, the said view being taken substantially alongthe line 3-3 of Figure 1;
Figure 4" is a cross-sectional view of a portion of: a fiexible rack elementrfor free piston engine synchronizers. showing a modified form of theinvention;
Figure 5- is a view similar to Figure 4 showing another modification of a" flexible construction for free piston" synchronizer. rack elements;
Figure 6 is a detailed sectional view taken along the line 6-6 of Figure 3;
Figure 7 is a cross-sectional view taken substantially along the line 7-7 of'Figure 4; and
Figure 8 is a cross-sectionalview taken along the line 8-8 of Figure 5.
Referring now particularlyto Figures 1', Ziand 3', a free piston engine is generally designated by the reference character 10. The free piston engine 10 is generally of conventionalconstruction and onlyportions thereof have. been schematically shown. The engine 10 comprises. a: cylindrical housing 11 havinganout'er: cylindrical wall 12. The cylindrical wall 12 includes. air: inlet openings 16 in communication with: the atmosphere; Thehousing also-includes oppositely;disposedend walls 14"an'd'a c'en trallydisposedirecess 15. Laterally: spaced and oppositely: disposed intermediate walls 16. are: provided on the. housing 11. The: cylindrical walls form-compression chambers as designated at. 17. oppositely-disposed. com; pressor pistons 18 are suitably mounted for: reciprocation: within the compressor. chambers 17.. Each. cylindrical wall- 16 also includes one or. more air inlet valvesxlflposi tioned immediately adjacent to an inwardly" extending: inclined wall 20. The inclined walls'20 define. therop=- posite ends of a compressed air'chamber 21 and aiifltO- said chamber may he delivered. through one or: more: valves-22 positioned on each of therwalls zll.
An inner cylindrical. wall is designated at 23. and this; wall includes acombustion chamber: 24centrally" posi tioned. The cylindricalwall 23 also includes'a scavenging: opening 25, adapted during-a certain stageof operationof the engine, to scavenge the combnstionschamber: 24; A pair of oppositely-disposed.freely'sliding powerpistons,
are positioned within the combustion chamber. 24; The:.
power pistons 26' are suitably connected by; means: of screws 27 to the compressor. pistons: 18 so' that they reciprocate with; the; power pistons 26..
The cylindrical wall 23 is-provided with*.a1boss 2'8- projecting upwardlyginto therrecess'15. The bossr28 has connected thereto a shaft 29" on which a' gear: or pinion. 30 is freely rotatable. The gear 30 forms part of a syn-- chronizing mechanism generally. designated at 31.. The synchronizing mechanism 31 comprises a pair of cylindrical guide members 32' which are laterally spaced-on opposite sides of the gear 30-andwhich may beformed as anintegral part ofthe housing 11; Eachguide merrrber 31 includes a centrally disposedopening oraccess. 33: so disposed that the. gear 30'may project through. said openings. A pair of laterally spaced substantially parallel. rack elements 34 are reciprocally positioned within the guide members 32. Each rack element comprises aplu: rality of rack teethSS in meshingengagementwith.- the gear 30. Eachrack'element 34 also includes afirstacyline' dricalportion. 36 havingsuitable-seals. 37. mounted. therea on, the said seals 37 being in sliding engagement with the inner surface of each cylindrical guide member 32.
The first cylindrical portion 36 is integrally connected to a flexible strap or reduced portion 38 which, in turn, is integral with a second cylindrical portion 39 which is provided at its end with a threaded projection 40. The threaded projection 40 of each rack element 34 is suitably connected to each of the compressor pistons 18 as indicated by means of nuts 41.
Referring now particularly to Figure 3 and 6, it should be pointed out that the flexible reduced portion 38 is positioned immediately adjacent the connecting end of the rack element 34. The reduced portion 38 permits a limited amount of flexing immediately adjacent the first and second cylindrical portions 36 and 39, respectively, and to prevent buckling of the strap 38 a pair of metal strip stifieners 42 are connected. The stitfeners may be of light metal material and are of semi-cylindrical construction, the same being disposed on opposite sides of the reduced portion 38 and being suitably connected thereto by means of screws 43. Thus, a major portion of the reduced portion 38 is supported against possible buckling through suflicient flexibility of the rack is obtained by virtue of the flexibility achieved at opposite ends of the said flexible portion 38. This design provides flexibility in a plane perpendicular to the reduced section 38, but is stiff in the plane of the section 38.
Figures 4, 5, 7 and 8 show modified forms of the invention, the rack elements being substantially identical with the exception that diflerent flexible portions are provided. These variations provide flexibility in all directions.
Referring now particularly to Figures 4 and 7, the reduced portion is designated at 44, the said portion being of cylindrical shape. A cylindrical stiffener 45 of a light metal encloses the reduced portion 44 by means of half portions 46 which are suitably connected together by screws 46. Here again, flexibility of the portion 44 is apparent at its opposite ends, the main portion of the reduced portion being, of course, supported against buckling by means of the cylindrical stiflener 45.
In the modification shown in Figures and 8, the flexible portion of the rack element shown here comprises essentially a pair of longitudinally spaced spool-shaped necks 47. The necks 47 provide for flexibility and are suitably connected together by means of a cylindrical connector 48 also integrally formed.
During the operation of a free piston engine, the power pistons 26, during the power stroke, are forced outwardly whereupon simultaneously the compressor pistons 18 compress air in the chamber 17. The opening 25 is now exposed and compressed air in the chamber 21 scavenges the combustion chamber 24 and discharges the gas through an exhaust outlet 49. The air which is compressed in the chamber 17 now forces the pistons 18 to return to the original position whereupon the valves 22 open to permit the inlet of air into the compressed air chamber 21. Thus, the operation has been briefly described and, of course, in this respect the engine disclosed is conventional.
As the pistons 26 and 28 reciprocate, it is, of course, desired that they are synchronized during the operation. This is achieved by the synchronizing mechanism 31. Since the rack elements are rigidly connected to the pistons 18, they are reciprocated with the said pistons. The rack teeth 35 engage the gear 30 and it is thus obvious that movement of one rack element is identical to the movement of the other rack element whereby synchronization is obtained. As indicated above, the rack elements, guides, and compressor pistons normally are required to maintain very close tolerances so that the racks will not bind, permanently bend or vibrate and will have a sulficiently satisfactory service life. In view of tolerance build-ups, during the engine assembly, and deflections occuring during operation, it is extremely diflicult to hold close tolerances or to obtain satisfactory service. How
ever, in the present invention, provisions are made for flexing of portions of the rack elements by means of the flexible reduced portions 38, 44 and 47. Thus, the rack elements will reciprocate in the guides without binding and the seals 37 are effective to seal lubricating oil, which may be contained within the guides, from the compressor chambers 17. In the embodiment shown in Figures 1, 2 and 3, the flexible element 38 is eflective at itsopposite ends to flex or bend during operation to accommodate any misalignment which might occur between the connecting portions 40 and the piston 18 with respect to the guide members 32. Yet by the inclusion of the stitfeners 42, buckling of the flexible element 38 is prevented. The stifleners, being of light metal, reduce the reciprocating mass of the system, and also reduce the compressor clearance volume. It is apparent that flexibility to accommodate misalignment has been achieved with no moving joints which could result in axial clearance and wear.
Likewise, in the modified embodiment shown in Figures 4 and 5, the flexible reduced portions 44 and 47 permit flexing of the portion of the rack adjacent thecompressor pistons to properly compensate for any slight misalignment which might occur. In the modified form shown in Figure 4, again the reduced portion 44 is reinforced against buckling by means of the casing or stiifener 45. The modification shown in Figures 5 and 8, of course, provide for flexing in the reduced portions 47 which are of spool shape and the intermediate portion 48.
prevents buckling during operation.
It is now apparent that improved rack designs for free piston engines has been provided, the same fully achieving the stated objects. It must be understood, of
course, that changes and modifications may be made associated with said housing, a gear mounted for rota-- tion on said housing between said guides, a rack element reciprocally positioned on each guide, each of said rack elements having a rack portion in meshing engagement with said gear, means connecting one end of each rack element to one of said compressor pistons for reciprocation therewith, each rack element including an elongated flexible portion of reduced cross sectional dimension permitting flexing of said rack elements relative to said guides during reciprocation, and stiffening means connected to said reduced flexible portion on opposite sides thereof, said stififening means including stifleners havinga length shorter than said flexible portion to permit flexing at longitudinally spaced points along said flexible portion. 6
2. In a free piston engine comprising a housing having a combustion chamber, opposed power pistons reciprocally positioned Within said combustion chamber, a compressor chamber associated with each power piston, and
compressor pistons within said compressor chambers, said compressor pistons being connected to said power pistons for movement therewith; a piston synchronizing .mechanism comprising a pair of laterally spaced guides associated with said housing, a gear mounted for rotation on said housing between said guides, a rack element reciprocally positioned on each guide, each of said rack elements having a rack portion in meshing engagement with said gear, and means connecting one end of each rack element to one of said compressor pistons for reciprocation therewith; each rack element including an elongated flat flexible strip portion of reduced cross sectional dimension permitting flexing of said rack elements relative to said guides during reciprocation.
3. In a free piston engine comprising a housing having a combustion chamber, opposed power pistons reciprocally positioned within said combustion chamber, a compressor chamber associated with each power piston, and compressor pistons within said compressor chamhers, said compressor pistons being connected to said power pistons for movement therewith; a piston syncronizing mechanism comprising a pair of laterally spaced guides associated with said housing, a gear mounted for rotation on said housing between said guides, a rack element reciprocally positioned on each guide, each of said rack elements having a rack portion in meshing engagement with said gear, means connecting one end of each rack element to one of said compressor pistons for reciprocation therewith, each rack element including an elongated flat flexible strip permitting flexing of said rack elements relative to said guides during reciprocation, and metal stifleners connected to said flat strip on opposite sides thereof, said stiffeners being shorter than said strip to permit flexing of longitudinally spaced portions of said strips.
4. In a free piston engine comprising a housing having a combustion chamber, opposed power pistons reciprocally positioned within said combustion chamber, a compressor chamber associated with each power piston, and compressor pistons within said compressor chambers, said compressor pistons being connected to said power pitons for movement therewith; a piston synchronism mechanism comprising a pair of laterally spaced guides associated with said housing, a gear mounted for rotation on said housing between said guides, a rack element reciprocally positioned on each guide, each of said rack elements having a rack portion in meshing engagement with said gear, means connecting one end of each rack element to one of said compressor pistons for reciprocation therewith, said means comprising a cylindrical flexible portion of less cross sectional dimension disposed between said rack portion and said connecting means to provide for flexing of said rack elements relative to said guides during reciprocation, and a stiffener member of lesser length than said flexible portion and connected to said flexible portion with its opposite ends disposed inwardly from the ends of the flexible member to localize the flexibility of said flexible portion.
5. In a free piston engine comprising a housing having a combustion chamber, opposed power pistons reciprocally positioned within said combustion chamber, a compressor chamber associated with each power piston, and compressor pistons within said compressor chambers, said compressor pistons being connected to said power pistons for movement therewith; a piston synchronism mechanism comprising a pair of laterally spaced guides associated with said housing, a gear mounted for rotation on said housing between said guides, a rack element reciprocally positioned on each guide, each of said rack elements having a rack portion in meshing engagement with said gear, means connecting one end of each rack element to one of said compressor pistons for reciprocation therewith, a cylindrical flexible portion of less cross sectional dimension disposed between said rack portion and saidconnecting means to provide for flexing of said rack elements relative to said guides during reciprocation, and a tubular stiflener member of lesser length than said flexible member and connected around said flexible portion with its opposite ends disposed inwardly from the opposite ends of the flexible member to localize the flexibility of said flexible portion.
References Cited in the file of this patent UNITED STATES PATENTS 2,461,224 Meitzler Feb. 8, 1949 2,811,148 Bobrowsky Oct. 29, 1957 FOREIGN PATENTS 754,169 Germany Aug. 14, 1952
US653815A 1957-04-19 1957-04-19 Synchronizing device for free piston engines Expired - Lifetime US2876751A (en)

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Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3192972A (en) * 1961-06-29 1965-07-06 William L Tenney Opposed piston cutting apparatus
US3672260A (en) * 1970-12-14 1972-06-27 Jean Gachot Compressed-air actuator
US3859966A (en) * 1973-02-16 1975-01-14 Anton Braun Linear balanced free piston machines
WO1980001588A1 (en) * 1979-02-03 1980-08-07 B Fromson Opposed piston internal combustion engine with special scavenging means
US4221155A (en) * 1978-05-24 1980-09-09 Ongaro Dynamics, Ltd. Vibration-free hydraulic power system
US4415110A (en) * 1981-08-17 1983-11-15 Hunter C Lamont LP Gas-operated impact tool
US4924956A (en) * 1986-10-24 1990-05-15 Rdg Inventions Corporation Free-piston engine without compressor
US4986394A (en) * 1986-06-26 1991-01-22 Lucas Industries Brake actuator
US5353690A (en) * 1993-03-04 1994-10-11 Shin Guo S Actuator type reciprocating mechanism

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2461224A (en) * 1944-08-23 1949-02-08 United Aircraft Corp Overstroke control for free-piston units
DE754169C (en) * 1941-07-12 1952-08-14 Forschungsanstalt Prof Junkers Gear to force the synchronism of the opposing flying masses of a free-flight piston machine
US2811148A (en) * 1955-11-28 1957-10-29 Ford Motor Co Coupling means

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE754169C (en) * 1941-07-12 1952-08-14 Forschungsanstalt Prof Junkers Gear to force the synchronism of the opposing flying masses of a free-flight piston machine
US2461224A (en) * 1944-08-23 1949-02-08 United Aircraft Corp Overstroke control for free-piston units
US2811148A (en) * 1955-11-28 1957-10-29 Ford Motor Co Coupling means

Cited By (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3192972A (en) * 1961-06-29 1965-07-06 William L Tenney Opposed piston cutting apparatus
US3672260A (en) * 1970-12-14 1972-06-27 Jean Gachot Compressed-air actuator
US3859966A (en) * 1973-02-16 1975-01-14 Anton Braun Linear balanced free piston machines
US4221155A (en) * 1978-05-24 1980-09-09 Ongaro Dynamics, Ltd. Vibration-free hydraulic power system
WO1980001588A1 (en) * 1979-02-03 1980-08-07 B Fromson Opposed piston internal combustion engine with special scavenging means
EP0014551A1 (en) * 1979-02-03 1980-08-20 Bertram William Fromson Opposed piston internal-combustion engine with special scavenging means
US4415110A (en) * 1981-08-17 1983-11-15 Hunter C Lamont LP Gas-operated impact tool
US4986394A (en) * 1986-06-26 1991-01-22 Lucas Industries Brake actuator
US4924956A (en) * 1986-10-24 1990-05-15 Rdg Inventions Corporation Free-piston engine without compressor
US5353690A (en) * 1993-03-04 1994-10-11 Shin Guo S Actuator type reciprocating mechanism

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