US1722425A - Internal-combustion engine - Google Patents

Internal-combustion engine Download PDF

Info

Publication number
US1722425A
US1722425A US142115A US14211526A US1722425A US 1722425 A US1722425 A US 1722425A US 142115 A US142115 A US 142115A US 14211526 A US14211526 A US 14211526A US 1722425 A US1722425 A US 1722425A
Authority
US
United States
Prior art keywords
pistons
cylinder
engine
gear
opposite directions
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
US142115A
Inventor
Junkers Hugo
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
Application granted granted Critical
Publication of US1722425A publication Critical patent/US1722425A/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
    • F02B71/00Free-piston engines; Engines without rotary main shaft

Definitions

  • 'My invention refers to internal combustion engines and more especially to engines of the type in which two pistons are freely arranged for reciprocation in a cylinder, these pistons being designed to move in opposite directions, and in my invention quite especially concerns the means whereby the two pistons are coupled for positive cooperation.
  • the term free piston is herein used to refer to an arrangement Where the pistons do not function to transmit power to a crank shaft by connecting rods, the construction in reality being crankless.
  • the arrangements involve the disadvantage that besides thepiston also the comparatively large masses of rock levers or rods must reciprocate, whereby the number of strokes per unit of time is reduced.
  • a further disadvantage consists therein that crossheads must be provided for the connection of the rods, su'ch cross-heads bein guided in longitudinal slots provided in the cylinder, whereby part of the cylinder cannot be utilized in the production of power, so that the length of the cylinder is greatly increased.
  • Another disadvantage is created by the fact that the rock levers, rods and the like must be provided on both sides of the engine, whereby this latter, and more especially the controlling means are rendered less readily accessible.
  • the present invention obviates this drawback inasmuch as the masses which reciprocate in opposite directions are substantially coupled only by means of rotary members.
  • the rotary members have comparative ly small masses and therefore permit obtaining a larger number of strokes. They can be arranged on one side only and substantially at any desired distance from the other parts of the engine, so as not to reduce the accessibility.
  • the long slits previously provided in the cylinders can be greatly reduced, whereby a considerable saving in weight, space and cost is obtained.
  • the fact that the pistons can be made shorter and lighter results in a further increase of the number of strokes per unit of time, which in turn results ends bevelled the engine.
  • the rotary coupling members preferably have the form of-toothed gear wheels or helical gear wheels cooperating with correspond ing racks and coupled by suitable shafts, the racks or the like being formed on or forming part of the pistons themselves.
  • Fig. 1 is an axial section
  • Fig. 2 is a. cross-section on the line II-II in Fig. 1
  • i Fig. 3 is a plan view of the movable parts of one modification
  • Figs. 4, 5 and 6 are similar views of the second modification.
  • 1 is a cylinderthe inner, and outer ends and are provided at the bottom each with teeth 10, 11, respectively,mesh1ng with toothed wheels 12, 13, keyed onto shafts 14, 15, respectively. These shafts project sideways and have mounted on their ear wheels .16, 17, meshing with similar w eels 18,19, which latter are keyed onto a common shaft 20. Obviously the two pistons 2 and 3 are coupled for absolutely uniform motion in opposite directions.
  • scavenging air blower 30 which is driven by any suitable means and supplies scavenging air through the conduit 31 into the container 32, from whichthe air passes through the ports 33 into the working chamber 1 when the .pistons have reached their outer dead centre positions, while the exhaust gases escape on the other side throu h port 34 into the exhaust conduit 35.
  • the rotary parts of the couphng gear are furtheradapted for driving auxiliary devices, such I combustion of a gas mixture to have taken place in the space 1' enclosed betweenthe pistons 4 and 5, while these pistons were In their inner dead centre position, the. expansion of y the combustion gases will force the pistons still remained in the cylinder. 'Durin 2, 3 asunder.
  • the piston 4 will uncover the port 33 of the scavenging air container 32 and a current of scavenging air will now flow through the cylinderlinthe direction from 33 to 34, carrying along with it the rest of exhaust gases whif1 1 t e outward, stroke of the pistons the kinetic en- .ergy imparted to them by the combustion ases' is converted into compressive energy in the cylinders 8, 9 and the pistons will come to a stillstand directlyafter having uncovered the ports 33 and 34. They are now acted upon'by the compressed air which remained over in the dead spaces of the coinpress'or cylinders 8, 9 and this air now forces the pistons back.
  • the pistons On their inward stroke the pistons will compress the scavenging air enclosed between them to such an extent that the fuel which is injected by means of pump 22 through pipe 25 and nozzle 26 into the cylinder space 1 towards the end of the inward stroke, is ignited, thereby forcing the pistons asunder again.
  • the pressure in the dead spaces of the compressor cylinders 8, 9 is graduall diminished until it has become as low as t 1e pressure in the suction pipes 55, 56.
  • the teeth forming part of the pistons are arranged as shown in Figs. 2 and 5, where the end faces of the teeth are shown to be formed in accordance with the circumference of the cylinder 1.
  • the teeth also contribute to packing the pistons relative to the cylinder and can also be made to extend across ports and the like in the cylinder wall without causing any considerable losses.
  • An engine comprising a cylinder, apair of free pistons arranged in said cylinder for simultaneous reciprocation in opposite directions and oscillatory pistons.
  • An engine comprising a cylinder, a pair of free pistons arranged in said cylinder for simultaneous reciprocation in opposite directions, a rack formed in the body of each piston, a gear wheel meshing with each rack and oscillatory means coupling said wheels.
  • An engine comprising a cylinder, a pair means for coupling said of free pistons arranged in said cylinder forsimultaneous reclprocatlon in opposite dlrections, a rack formed in the body of each. piston, a gear .Wheel meshing with each rack and oscillatory means including an inter- .mediate shaft coupling said wheels.
  • An engine comprising a cylinder, a pair of free pistons arranged in said cylinder for simultaneous reciprocation in opposite directions, rack teeth formed in the body of each piston, a gear wheel meshing-with each rackand an intermediate shaft coupling said tons and'an auxiliary device operatively connected with said oscillatory means.
  • An engine comprising a cylinder, a pair of free pistons arranged in said cylinder for simultaneous reciprocation in opposite directions, oscillatory means for coupling said pistons and a pump operatively connected with said oscillatory means.
  • An engine comprising a cylinder, a pair of free pistons arranged in said cylinder for simultaneous reciprocation in opposite directions and oscillatory means including racks and gears for coupling said pistons,.both ends of each piston being equal in diameter.
  • a cylinder of uniform diameter throughout its length a pair of free pistons arranged in said cylinder, a rack on each piston substantially spaced from the ends thereof, the tip faces of the rack teethconforming to the circumferential face of the piston, and

Description

Patented July 30, 1929.
UNITED STATES HUGO JUNKERS, OF DESS AU, GERMANY.
INlLERNAL-COMBU STION Enema.
Application filed October 16, 1926, Serial No. 142,115, and in Germany October 19, 1925. 4
'My invention refers to internal combustion engines and more especially to engines of the type in which two pistons are freely arranged for reciprocation in a cylinder, these pistons being designed to move in opposite directions, and in my invention quite especially concerns the means whereby the two pistons are coupled for positive cooperation. The term free piston is herein used to refer to an arrangement Where the pistons do not function to transmit power to a crank shaft by connecting rods, the construction in reality being crankless.
In similar free piston engines such coupling of the pistons has hitherto been effected by means of rocking levers or rods arranged for parallel motion relative to the pistons,
reversing gear being inserted between these rods. 1
The arrangements involve the disadvantage that besides thepiston also the comparatively large masses of rock levers or rods must reciprocate, whereby the number of strokes per unit of time is reduced. A further disadvantage consists therein that crossheads must be provided for the connection of the rods, su'ch cross-heads bein guided in longitudinal slots provided in the cylinder, whereby part of the cylinder cannot be utilized in the production of power, so that the length of the cylinder is greatly increased. Another disadvantage is created by the fact that the rock levers, rods and the like must be provided on both sides of the engine, whereby this latter, and more especially the controlling means are rendered less readily accessible.
The present invention obviates this drawback inasmuch as the masses which reciprocate in opposite directions are substantially coupled only by means of rotary members. As compared with reciprocating coupling means the rotary members have comparative ly small masses and therefore permit obtaining a larger number of strokes. They can be arranged on one side only and substantially at any desired distance from the other parts of the engine, so as not to reduce the accessibility. The long slits previously provided in the cylinders, can be greatly reduced, whereby a considerable saving in weight, space and cost is obtained. The fact that the pistons can be made shorter and lighter results in a further increase of the number of strokes per unit of time, which in turn results ends bevelled the engine.
The rotary coupling members preferably have the form of-toothed gear wheels or helical gear wheels cooperating with correspond ing racks and coupled by suitable shafts, the racks or the like being formed on or forming part of the pistons themselves.
In the drawings afiixed to this specification and forming part thereof two modifications of an engine embodying my invention are illustrated diagrammatically by way of example.
In the drawings- Fig. 1 is an axial section,
Fig. 2 is a. cross-section on the line II-II in Fig. 1, and i Fig. 3 is a plan view of the movable parts of one modification, while Figs. 4, 5 and 6 are similar views of the second modification.
in a corresponding increase inthe efliciency of Referring first to Figs. 1-3, 1 is a cylinderthe inner, and outer ends and are provided at the bottom each with teeth 10, 11, respectively,mesh1ng with toothed wheels 12, 13, keyed onto shafts 14, 15, respectively. These shafts project sideways and have mounted on their ear wheels .16, 17, meshing with similar w eels 18,19, which latter are keyed onto a common shaft 20. Obviously the two pistons 2 and 3 are coupled for absolutely uniform motion in opposite directions.
By using pistons having end faces of equal size for the working and for the compressor cylinders I obtain the advantage that the working chambers 1 and 8, 9 of the cylinders can extend closev to the toothed wheels. 12 and 13, gearing with the pistons 2 and 3,
so that sideways of these gear wheels only the space for the packing of the pistons is re quired. It is true that in thecase'of twostroke engines separate means for feeding scavenging air are required. In the present instance a scavenging air blower 30 is shown, which is driven by any suitable means and supplies scavenging air through the conduit 31 into the container 32, from whichthe air passes through the ports 33 into the working chamber 1 when the .pistons have reached their outer dead centre positions, while the exhaust gases escape on the other side throu h port 34 into the exhaust conduit 35. The rotary parts of the couphng gear are furtheradapted for driving auxiliary devices, such I combustion of a gas mixture to have taken place in the space 1' enclosed betweenthe pistons 4 and 5, while these pistons were In their inner dead centre position, the. expansion of y the combustion gases will force the pistons still remained in the cylinder. 'Durin 2, 3 asunder. The outer end faces 6, 7 of the pistons will now compress the air or other gases enclosed in the compressor cylinders8, 9 and will force them through the pressure valves 51, 52 into'the pressure pipes 53, 54 which lead to some place of consumption of the compressed gas or air thus produced; While the pistons 2, 3 are moving outwards, the pressure in 1 diminishes and the inner edge of piston 3 will uncoverthe exhaust port 34, allowing the gases of combustion to escape through pipe 35. Directly thereafter the piston 4 will uncover the port 33 of the scavenging air container 32 and a current of scavenging air will now flow through the cylinderlinthe direction from 33 to 34, carrying along with it the rest of exhaust gases whif1 1 t e outward, stroke of the pistons the kinetic en- .ergy imparted to them by the combustion ases' is converted into compressive energy in the cylinders 8, 9 and the pistons will come to a stillstand directlyafter having uncovered the ports 33 and 34. They are now acted upon'by the compressed air which remained over in the dead spaces of the coinpress'or cylinders 8, 9 and this air now forces the pistons back. On their inward stroke the pistons will compress the scavenging air enclosed between them to such an extent that the fuel which is injected by means of pump 22 through pipe 25 and nozzle 26 into the cylinder space 1 towards the end of the inward stroke, is ignited, thereby forcing the pistons asunder again. During the inward stroke of the pistons the pressure in the dead spaces of the compressor cylinders 8, 9 is graduall diminished until it has become as low as t 1e pressure in the suction pipes 55, 56. From this point on owing to their momentum the pistons on their inward s roke' generate a vacuum in the compressor c linders, whereby the suction valves 57, 58am opened and the compressor cylinders 8, 9 are filled with fresh air or other gas to be compressed during the outward stroke of the pis ton which nowfollows. The pistons during their movements in opposite directions are continuously coupled by the gearing 1420 in such manner that they are compelled to always move in unison, so that small inequalities in the friction arisin between the pistons and the cylinder walls or in the operation of the compressor cylinders cannot bring forth any irregularit pistons. However, t is gearing does not serve for transmitting the full energy of combustion acting on the pistons to the outside,
of movement of the thistransmission' of ener y being effected by means of the compresse gas through pipes 53, 54.
It will be obvious that in the operation of air or compressed the gearing coupling the pistons, said gears partake of the reciprocatory motion of the pistons, converting the same into what I term osclllatory movement 1n that the gears may rotate in one direction one or morerevo-' lut-ions followed by a rotation of one or more tinguished from a continuous rotation in one revolutions in the opposite direction, as disdirection. It is in thissense that the term oscillatory is employed in the appended have opposite pitches, so that in this case also the pistons 2 and 3 are coupled for exact motion in opposite directions.
Preferably the teeth forming part of the pistons are arranged as shown in Figs. 2 and 5, where the end faces of the teeth are shown to be formed in accordance with the circumference of the cylinder 1. For in this case the teeth also contribute to packing the pistons relative to the cylinder and can also be made to extend across ports and the like in the cylinder wall without causing any considerable losses.
By correspondingly choosing the ratio of transmission and of the screw pitch-I am enabled also to utilize the new coupling of the pistons in'such cases, where the two masses shall have strokes of different length.
I wish it to be understood that I do not desire to be limited to the exact details'of construction shown and described for obvious modification willoccur to a person skilled in the art. I i
I claim 1. An engine comprisinga cylinder, apair of free pistons arranged in said cylinder for simultaneous reciprocation in opposite directions and oscillatory pistons.
2.; An engine comprising a cylinder, a pair of free pistons arranged in said cylinder for simultaneous reciprocation in opposite directions, a rack formed in the body of each piston, a gear wheel meshing with each rack and oscillatory means coupling said wheels.
3. An engine comprising a cylinder, a pair means for coupling said of free pistons arranged in said cylinder forsimultaneous reclprocatlon in opposite dlrections, a rack formed in the body of each. piston, a gear .Wheel meshing with each rack and oscillatory means including an inter- .mediate shaft coupling said wheels.
4. An engine comprising a cylinder, a pair of free pistons arranged in said cylinder for simultaneous reciprocation in opposite directions, rack teeth formed in the body of each piston, a gear wheel meshing-with each rackand an intermediate shaft coupling said tons and'an auxiliary device operatively connected with said oscillatory means.
7. An engine comprising a cylinder, a pair of free pistons arranged in said cylinder for simultaneous reciprocation in opposite directions, oscillatory means for coupling said pistons and a pump operatively connected with said oscillatory means.
8. An engine comprising a cylinder, a pair of free pistons arranged in said cylinder for simultaneous reciprocation in opposite directions and oscillatory means including racks and gears for coupling said pistons,.both ends of each piston being equal in diameter.
9. In an engine of thetype described, a cylinder of uniform diameter throughout its length and formed with pockets intermediate the ends thereof, a pair of free pistons disposed in said cylinder and provided with racks intermediate their ends, gear members disposed in the pockets and projecting through openings in the wall of the cylinder into coacting relation with the racks aforesaid, and connections between the gear members to effect simultaneous rotation of the gear membersalternately in opposite directions incident to the movement of the pistons.
10. In an engine construction of the class described, a cylinder of uniform diameter throughout its length, a pair of free pistons arranged in said cylinder, a rack on each piston substantially spaced from the ends thereof, the tip faces of the rack teethconforming to the circumferential face of the piston, and
gear connections between the racks of the pistons to insure simultaneous travel of the same during reciprocation.
11. In an engine construction of the class described, a cylinder of uniform diameter throughout its length. and having spaced pockets in the wall thereof, a pair of free pistons arranged in the cylinder, a rack on each piston intermediate the ends thereof,' the tip faces of the teeth of the racks conforming with the circumferential face of the pistons, gear members disposed in. the pockets aforesaid adjacent the walls of the cylinder and projecting through openings in the latter into engagement with the racks of the pistons, and
a driving connection between the gear members for causing simultaneous rotation of the gear members alternately in opposite direc tionandcorrespondin'g movement of the pistons in opposite directions.
' In testimony whereof I aflix my signature.
HUGO JUN
US142115A 1925-10-19 1926-10-16 Internal-combustion engine Expired - Lifetime US1722425A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE1722425X 1925-10-19

Publications (1)

Publication Number Publication Date
US1722425A true US1722425A (en) 1929-07-30

Family

ID=7740632

Family Applications (1)

Application Number Title Priority Date Filing Date
US142115A Expired - Lifetime US1722425A (en) 1925-10-19 1926-10-16 Internal-combustion engine

Country Status (1)

Country Link
US (1) US1722425A (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2453515A (en) * 1944-11-06 1948-11-09 United Aircraft Corp Restraining mechanism for freepiston units
US2581191A (en) * 1946-06-27 1952-01-01 United Aircraft Corp Free-piston compressor
US4382748A (en) * 1980-11-03 1983-05-10 Pneumo Corporation Opposed piston type free piston engine pump unit
US20070261677A1 (en) * 2006-05-12 2007-11-15 Bennion Robert F Paired-piston linear engine

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2453515A (en) * 1944-11-06 1948-11-09 United Aircraft Corp Restraining mechanism for freepiston units
US2581191A (en) * 1946-06-27 1952-01-01 United Aircraft Corp Free-piston compressor
US4382748A (en) * 1980-11-03 1983-05-10 Pneumo Corporation Opposed piston type free piston engine pump unit
US20070261677A1 (en) * 2006-05-12 2007-11-15 Bennion Robert F Paired-piston linear engine
US8091519B2 (en) 2006-05-12 2012-01-10 Bennion Robert F Paired-piston linear engine

Similar Documents

Publication Publication Date Title
US2199625A (en) Double-piston internal combustion engine
US3398643A (en) Rotary piston engine, pump or other machine
US3144007A (en) Rotary radial-piston machine
US2407859A (en) Mechanical movement
DE102008050014B4 (en) A rotary internal combustion engine
US3786790A (en) Double-chambered reciprocatable double-action-piston internal combustion engine
US3396709A (en) Roto-piston engine
US1895206A (en) Swash plate internal combustion engine operating on the two-stroke cycle
SU466675A3 (en) Rotary piston machine
US4442758A (en) Piston machine
US1722425A (en) Internal-combustion engine
US3329134A (en) Internal combustion engine
US3356080A (en) Internal combustion engine with wobble plate shaft drive
EP0320171A1 (en) Power transmission apparatus
US3269321A (en) Combustion engine for conveying a hydraulic pressure medium
US1476309A (en) Internal-combustion engine
US2828906A (en) Engine
US3283752A (en) Free piston machine
US3974803A (en) Internal combustion engine with gyratory piston and cylinder movement
US2767589A (en) Cam and slide motion converting means for converting rotary motion to reciprocating motion
GB1450815A (en) Internal combustion devices
US1653925A (en) Internal-combustion engine
RU2009347C1 (en) Internal combustion engine
US1099860A (en) Internal-combustion engine.
US1777007A (en) Engine construction