US2031318A - Engine - Google Patents

Engine Download PDF

Info

Publication number
US2031318A
US2031318A US406090A US40609029A US2031318A US 2031318 A US2031318 A US 2031318A US 406090 A US406090 A US 406090A US 40609029 A US40609029 A US 40609029A US 2031318 A US2031318 A US 2031318A
Authority
US
United States
Prior art keywords
crank
power
shaft
shafts
engine
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
US406090A
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.)
Firm Junkers Motorenbau G M B
FIRM JUNKERS-MOTORENBAU GmbH
Original Assignee
Firm Junkers Motorenbau G M B
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 Firm Junkers Motorenbau G M B filed Critical Firm Junkers Motorenbau G M B
Application granted granted Critical
Publication of US2031318A publication Critical patent/US2031318A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • 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
    • F01B7/00Machines or engines with two or more pistons reciprocating within same cylinder or within essentially coaxial cylinders
    • F01B7/02Machines or engines with two or more pistons reciprocating within same cylinder or within essentially coaxial cylinders with oppositely reciprocating pistons
    • F01B7/14Machines or engines with two or more pistons reciprocating within same cylinder or within essentially coaxial cylinders with oppositely reciprocating pistons acting on different main shafts
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B75/00Other engines
    • F02B75/28Engines with two or more pistons reciprocating within same cylinder or within essentially coaxial cylinders

Definitions

  • ENGINE cHugo Junkers, Dessau, Germany, assigner toI My invention refersztoiengines and more especially to the kind of engines in which two pistons are arranged in'each cylinder for reciprocation in opposite directions, these pistons acting ontwo separate crank shafts, one at each endof the plston,fwhich are positively coupled with each other by means of suitable. gearing, such as toothed wheels, chains, crank gear, orthe like.
  • the present invention contemplates a considerable reduction of the percentage of power tobe transmitted from the intermediate gearing ltothe place ofconsumption, in order to effect a saving of space, weight, cost, and power4 losses.
  • I employ means well known per seY for making the percentage of work to be transmitted by each of the two crank shafts unequal and I cause the major portion of the engine output to be taken oif the more heavily loaded shaft, or if the intermediate gearing has the form of" a toothed wheel gearing with a plurality Vof intermediate wheels arranged 'in series, from the axle of the toothed wheel directly adjoiningthis shaft. I thereby obtain that the power to be transmitted by the intermediate gearing is less firm: Junkers-Motorenbau Germany G. m. b. H., Dessau,V
  • I may for instance use the following means: l
  • cranks of .those pistons which transmit the major amount of power, are made to lead the cranks of the pistons transmitting the minor amount of power.
  • That crank shaft receiving thel minor amount of power is ,utilizedl for operating the auxiliary, devices to be-driven by the engine, such as for instance the pumps for cooling water, combustion air, f fuel, ⁇ lubricant, etc., the electrical this speci-ca'tion and
  • Fig. 1 is a diagram which illustrates the unequal distribution of the output, which. results in an internal combustion engine with double pistons from the leading of the crank for the exhaust piston.
  • Figs. 2 and 3 are an axial longitudinal section ⁇ and an axial cross section, respectively, of the first,i and v Figs. 4 and 5 are similar views of the second modification.
  • Fig. l illustrates thev pressure-volume-diagrams corresponding to the ⁇ thrust of an internal combustion engine having two pistons operating in opposite directions, the cranks of these pistons u relative to their extreme positions.
  • the surface bordered by the curved line 2 corresponds to thg percentage of power transmitted by the piston controlling the scavenging ports, this latter percentage being considerably lower than the one transmitted by the iirst mentioned 25 piston.
  • the relation between the two characteristics and the angle of lead d can easily be guessed from the diagram. i n
  • I0 area plurality of juxtaposed cylinders, and II, I2 ⁇ are two ⁇ 30 pistons arranged in each cylinder for reciproca.- tion in opposite directions.
  • I3 are the intake ports for the scavenging air or mixture arranged f-at one end of the working chamber of each cylinder. opposite end. of the working chamber.
  • the pistons vI I controlling the scavenging ports I3 transmit power yto the crank shaft l5, the pistons I2 controlling the exhaust ports operate the crank shaft I6.
  • the two shafts are positively con- 40 nected with each other by bevel gearlngs I'I,y I8, and I9, 20, respectively, and an intermediate shaft 2l in such manner that each crank of shaft IB leads with regard to the crank, belongingi'to the same cylinder, of lshaft I5 by a predeter- 45 mined angle a (Fig. 3).
  • 'Ihe power generatedV by the engine is transmitted for instance to a water or air propeller 23 driven by the engine by means of an extension 22 of the crank shaft I6 arranged on the exhaust side.
  • crank shafts are positively coupled by toothed wheels I1', I8', I9', 20', arranged in series, in such manner that the crank l shaft rI6' leads with respect to the shaft ISby an angle a, whereby also an increased transmission of power to shaft I6' is obtained.
  • the radius of the cranks oi shaft I6 is made longer than theI radius of the cranks of shaft I5.
  • power is transmitted by means of the extension 25 of the axle of the intermediate wheel 20' directly adjoining crank shaft I 6', so that only this intermediate wheel is more heavily strained, while the other intermediate wheels Il' to I 9' are much less loaded.
  • the most advantageous embodiment of my invention comprises a twin-shaft, two-cycle internal combustion 'aeroplane engine, a plurality of juxtaposed cylinders having intake and exhaust ports, a pair of crank-shafts one mounted at each end of-said cylinders rotating at the same speed, a pair of pistons mounted to reciprocate in each of said cylinders in opposite directions and operatively connected by means of crank arms to transmit power to said crank-shafts, one of said pistons being adapted to control said intake ports and the other being adapted to control said exhaust ports, means including crank arms of unequal crank throw producing an unequal distribution of power to said crank-shafts; the crank arms having the greater crank throw transmitting the major amount of power; a driven part ⁇ coupled to both crank-shafts, and means for synchronizing the operation of said crank-shafts and for transmitting power from the crank-shaft receiving the minor amount of power to said driven part, said synchronizing means being of such weight and strength as to be adapted to transmit less thanvhalf
  • a twin-shaft', two-cycle, internal combustion engine a plurality of juxtaposed cylinders having intake and exhaust ports, a pair of crankshafts one mounted at each end of said cylinders rotating at the same speed, a pair of pistons mounted to reciprocate in each of said cylinders in opposite directions and operatively connected by means of cranks and crank arms to transmit power to said crank-shafts.
  • one of said pistons being adapted to controlA said intake ports and the ⁇ other being adapted to control said exhaust ports, means 'including leading and lagging cranks producing an unequal distribution of power to said crank-shafts, said leading cranks, beingconnected to the crank-shaft receiving the major amount of power.
  • a driven part coupled to both crank-shafts, and means for synchronizing the operation of said crank-shafts and for transmitting power from the crank-shaft receiving the minor amount of power 'to said driven part, said synchronizing means' being of such weight and strength as to be adapted to transmit less than half of the total power delivered to said driven part, the crank-shaft receiving the major amount of power -being more closely coupled to said driven part than said shaft receiving the minor amount of power.
  • crankshaft receiving the minor amount of power is coupled to more auxiliary machinery than said crank-shaft receiving the maior amount o power.
  • said vsynchronizing means comprises a train of gears, the driven member being mounted on one of the shafts of said gears.

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Transmission Devices (AREA)

Description

H. JUNKERS Feb. 18, 1936.
`-ENGINE Filed Nov. 9, 1929 Patented feb. 18,
. ENGINE cHugo Junkers, Dessau, Germany, assigner toI My invention refersztoiengines and more especially to the kind of engines in which two pistons are arranged in'each cylinder for reciprocation in opposite directions, these pistons acting ontwo separate crank shafts, one at each endof the plston,fwhich are positively coupled with each other by means of suitable. gearing, such as toothed wheels, chains, crank gear, orthe like.
If the power generated by th engine is transmitted only by one Aof these shafts or by a part of the intermediate gearing adjoining one of the shafts, these gears are called-.up on to transferV that half of the output, which is transmitted by the second shaft, towards the first `crank shaft, `and. are therefore required to be comparatively heavy and large, so that considerable losses of power are incurred.
The present invention contemplates a considerable reduction of the percentage of power tobe transmitted from the intermediate gearing ltothe place ofconsumption, in order to effect a saving of space, weight, cost, and power4 losses.
To this end I employ means well known per seY for making the percentage of work to be transmitted by each of the two crank shafts unequal and I cause the major portion of the engine output to be taken oif the more heavily loaded shaft, or if the intermediate gearing has the form of" a toothed wheel gearing with a plurality Vof intermediate wheels arranged 'in series, from the axle of the toothed wheel directly adjoiningthis shaft. I thereby obtain that the power to be transmitted by the intermediate gearing is less firm: Junkers-Motorenbau Germany G. m. b. H., Dessau,V
Application November 9, 1929", serial No. 406,090
Germany November 20, 1928 than one half of the total power.
Inbrder to obtain'an unequal .distribution of work onto the two crank shafts, I may for instance use the following means: l
(a) In internal combustion engines, the cranks of .those pistons, which transmit the major amount of power, are made to lead the cranks of the pistons transmitting the minor amount of power.
(b) Pistons ployed;
In the drawing amxed to' forming .part thereof. twol modications of an engine embodying my invention are illustrated diagrammauesuy by way' In. the drawing of example.
different strokesare ema.
(c) That crank shaft receiving thel minor amount of power is ,utilizedl for operating the auxiliary, devices to be-driven by the engine, such as for instance the pumps for cooling water, combustion air, f fuel,` lubricant, etc., the electrical this speci-ca'tion and Fig. 1 is a diagram which illustrates the unequal distribution of the output, which. results in an internal combustion engine with double pistons from the leading of the crank for the exhaust piston.
Figs. 2 and 3 are an axial longitudinal section `and an axial cross section, respectively, of the first,i and v Figs. 4 and 5 are similar views of the second modification.
Fig. l illustrates thev pressure-volume-diagrams corresponding to the` thrust of an internal combustion engine having two pistons operating in opposite directions, the cranks of these pistons u relative to their extreme positions. The dla.-
' gram surface bordered by the curved line I corresponds to the percentage of. power which is transmitted to the piston controlling the exhaust ports, which is connected with the leading crank. 20
The surface bordered by the curved line 2 corresponds to thg percentage of power transmitted by the piston controlling the scavenging ports, this latter percentage being considerably lower than the one transmitted by the iirst mentioned 25 piston. The relation between the two characteristics and the angle of lead d can easily be guessed from the diagram. i n
Referring now to Figs. 2 and 3, I0 area plurality of juxtaposed cylinders, and II, I2` are two` 30 pistons arranged in each cylinder for reciproca.- tion in opposite directions. I3 are the intake ports for the scavenging air or mixture arranged f-at one end of the working chamber of each cylinder. opposite end. of the working chamber. The pistons vI I controlling the scavenging ports I3 transmit power yto the crank shaft l5, the pistons I2 controlling the exhaust ports operate the crank shaft I6. The two shafts are positively con- 40 nected with each other by bevel gearlngs I'I,y I8, and I9, 20, respectively, and an intermediate shaft 2l in such manner that each crank of shaft IB leads with regard to the crank, belongingi'to the same cylinder, of lshaft I5 by a predeter- 45 mined angle a (Fig. 3). 'Ihe power generatedV by the engine is transmitted for instance to a water or air propeller 23 driven by the engine by means of an extension 22 of the crank shaft I6 arranged on the exhaust side. In consequence of `this ar- 50 rangement shaft I6 is acted upon with more than one half of the engine output, and in consequence thereofl the intermediate gearing I1 to 2| is not called upon to transmit one half, but less thanv onehalfofthetotaloutrmt; Inordertofun-gg being staggered through alpredeterminedangle 15 I4 are the exhaust ports arranged at the 35 ther reduce the power to be transmitted by this gearing, the auxiliary devices 30, 3|, to be opercrankshaft I5'. 'I'he two crank shafts are positively coupled by toothed wheels I1', I8', I9', 20', arranged in series, in such manner that the crank l shaft rI6' leads with respect to the shaft ISby an angle a, whereby also an increased transmission of power to shaft I6' is obtained. In order to further increase the percentage of power transmitted to shaft I6', the radius of the cranks oi shaft I6 is made longer than theI radius of the cranks of shaft I5. Here power is transmitted by means of the extension 25 of the axle of the intermediate wheel 20' directly adjoining crank shaft I 6', so that only this intermediate wheel is more heavily strained, while the other intermediate wheels Il' to I 9' are much less loaded. According to the diameter of the toothed wheels 2i'- and 22' mounted on the crank shafts and of the intermediate wheel 20 transmitting power, an increase or reduction of the number of revolutions can be obtained for the power transmitting axle 25 with iespect to the crank shafts. Auxiliary devices 38', which are to be operated by the engine, are here again connected to the crank shaft I5'. Y
The most advantageous embodiment of my invention, comprises a twin-shaft, two-cycle internal combustion 'aeroplane engine, a plurality of juxtaposed cylinders having intake and exhaust ports, a pair of crank-shafts one mounted at each end of-said cylinders rotating at the same speed, a pair of pistons mounted to reciprocate in each of said cylinders in opposite directions and operatively connected by means of crank arms to transmit power to said crank-shafts, one of said pistons being adapted to control said intake ports and the other being adapted to control said exhaust ports, means including crank arms of unequal crank throw producing an unequal distribution of power to said crank-shafts; the crank arms having the greater crank throw transmitting the major amount of power; a driven part `coupled to both crank-shafts, and means for synchronizing the operation of said crank-shafts and for transmitting power from the crank-shaft receiving the minor amount of power to said driven part, said synchronizing means being of such weight and strength as to be adapted to transmit less thanvhalf of the total power delivered' to said driven part, the crank-shaft receivingthe major amount of power being more closely coupled to said driven part than said shaft receivingof power, I mean that the former shaft is 'closer to the driven part or is coupled therewith more directly or through fewer moving' parts or through ore sturdy mechanism.
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 modifications will occur to a person skilled in theart.
1. In a twin-shaft', two-cycle, internal combustion engine, a plurality of juxtaposed cylinders having intake and exhaust ports, a pair of crankshafts one mounted at each end of said cylinders rotating at the same speed, a pair of pistons mounted to reciprocate in each of said cylinders in opposite directions and operatively connected by means of cranks and crank arms to transmit power to said crank-shafts. one of said pistons being adapted to controlA said intake ports and the `other being adapted to control said exhaust ports, means 'including leading and lagging cranks producing an unequal distribution of power to said crank-shafts, said leading cranks, beingconnected to the crank-shaft receiving the major amount of power. a driven part coupled to both crank-shafts, and means for synchronizing the operation of said crank-shafts and for transmitting power from the crank-shaft receiving the minor amount of power 'to said driven part, said synchronizing means' being of such weight and strength as to be adapted to transmit less than half of the total power delivered to said driven part, the crank-shaft receiving the major amount of power -being more closely coupled to said driven part than said shaft receiving the minor amount of power.
2. 'I'he engine of claim 1 wherein the driven part is mounted on the crank-shaft receiving the major amount of power.
3'. The engine of claim 1 wherein said crankshaft receiving the minor amount of power is coupled to more auxiliary machinery than said crank-shaft receiving the maior amount o power. r
4. 'I-'he engine of claim 1 wherein said vsynchronizing means comprises a train of gears, the driven member being mounted on one of the shafts of said gears.
' HUGO JUNKERS.
US406090A 1928-11-20 1929-11-09 Engine Expired - Lifetime US2031318A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE2031318X 1928-11-20

Publications (1)

Publication Number Publication Date
US2031318A true US2031318A (en) 1936-02-18

Family

ID=7981781

Family Applications (1)

Application Number Title Priority Date Filing Date
US406090A Expired - Lifetime US2031318A (en) 1928-11-20 1929-11-09 Engine

Country Status (1)

Country Link
US (1) US2031318A (en)

Cited By (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2420779A (en) * 1944-04-10 1947-05-20 Carl L Holmes Opposed piston engine
US2473759A (en) * 1946-08-02 1949-06-21 Mallory Res Co Two-cycle opposed piston engine
US2541594A (en) * 1947-09-11 1951-02-13 Mallory Res Co Internal-combustion engine
US2545098A (en) * 1949-09-30 1951-03-13 Mallory Marion Opposed piston engine
US2805654A (en) * 1950-10-06 1957-09-10 Harold M Jacklin Opposed piston two cycle engine
US20070039572A1 (en) * 2004-06-10 2007-02-22 Achates Power, Llc Two-stroke, opposed-piston internal combustion engine
ES2288075A1 (en) * 2005-06-24 2007-12-16 Jose Luis Antuña Suarez Device for forming platform in existing wall, has multiple supports for framework of beams, where each support has cantilever with lower support step in wall, and upper clamp has locking security pin for horizontal hooking in fixed cable
US20100212638A1 (en) * 2009-02-20 2010-08-26 Achates Power, Inc. Opposed piston engines with controlled provision of lubricant for lubrication and cooling
US20100212637A1 (en) * 2009-02-20 2010-08-26 Achates Power, Inc. Cylinder and piston assemblies for opposed piston engines
US20100212613A1 (en) * 2009-02-20 2010-08-26 Achates Power, Inc. Multi-Cylinder opposed piston engines
US9435290B2 (en) 2014-08-04 2016-09-06 Achates Power, Inc. Opposed-piston engine structure with a split cylinder block
US9915188B2 (en) 2015-02-27 2018-03-13 Achates Power, Inc. Hybrid opposed-piston engine system
US11598259B2 (en) 2019-08-29 2023-03-07 Achates Power, Inc. Hybrid drive system with an opposed-piston, internal combustion engine

Cited By (29)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2420779A (en) * 1944-04-10 1947-05-20 Carl L Holmes Opposed piston engine
US2473759A (en) * 1946-08-02 1949-06-21 Mallory Res Co Two-cycle opposed piston engine
US2541594A (en) * 1947-09-11 1951-02-13 Mallory Res Co Internal-combustion engine
US2545098A (en) * 1949-09-30 1951-03-13 Mallory Marion Opposed piston engine
US2805654A (en) * 1950-10-06 1957-09-10 Harold M Jacklin Opposed piston two cycle engine
US20080163848A1 (en) * 2004-06-10 2008-07-10 Achates Power, Inc. Opposed piston engine with piston compliance
US20070245892A1 (en) * 2004-06-10 2007-10-25 Achates Power, Llc Two-Cycle, Opposed-Piston Internal Combustion Engine
US20070039572A1 (en) * 2004-06-10 2007-02-22 Achates Power, Llc Two-stroke, opposed-piston internal combustion engine
US7784436B2 (en) 2004-06-10 2010-08-31 Achates Power, Inc. Two-cycle, opposed-piston internal combustion engine
US20080314688A1 (en) * 2004-06-10 2008-12-25 Achates Power, Inc. Internal combustion engine with provision for lubricating pistons
US7546819B2 (en) 2004-06-10 2009-06-16 Achates Power. Two-stroke, opposed-piston internal combustion engine
US7549401B2 (en) 2004-06-10 2009-06-23 Achates Power, Inc. Two-cycle, opposed-piston internal combustion engine
US7591235B2 (en) 2004-06-10 2009-09-22 Achates Power, Inc. Opposed piston engine with piston compliance
US20100012055A1 (en) * 2004-06-10 2010-01-21 Achates Power, Inc. Cylinder and piston assemblies for opposed piston engines
US20100186723A1 (en) * 2004-06-10 2010-07-29 Achates Power, Llc Two-cycle, opposed-piston internal combustion engine
US8281755B2 (en) 2004-06-10 2012-10-09 Achates Power, Inc. Internal combustion engine with provision for lubricating pistons
US7861679B2 (en) 2004-06-10 2011-01-04 Achates Power, Inc. Cylinder and piston assemblies for opposed piston engines
ES2288075A1 (en) * 2005-06-24 2007-12-16 Jose Luis Antuña Suarez Device for forming platform in existing wall, has multiple supports for framework of beams, where each support has cantilever with lower support step in wall, and upper clamp has locking security pin for horizontal hooking in fixed cable
US20100212613A1 (en) * 2009-02-20 2010-08-26 Achates Power, Inc. Multi-Cylinder opposed piston engines
US20100212637A1 (en) * 2009-02-20 2010-08-26 Achates Power, Inc. Cylinder and piston assemblies for opposed piston engines
US20100212638A1 (en) * 2009-02-20 2010-08-26 Achates Power, Inc. Opposed piston engines with controlled provision of lubricant for lubrication and cooling
US8539918B2 (en) 2009-02-20 2013-09-24 Achates Power, Inc. Multi-cylinder opposed piston engines
US8550041B2 (en) 2009-02-20 2013-10-08 Achates Power, Inc. Cylinder and piston assemblies for opposed piston engines
US9328692B2 (en) 2009-02-20 2016-05-03 Achates Power, Inc. Opposed piston engines with controlled provision of lubricant for lubrication and cooling
US9435290B2 (en) 2014-08-04 2016-09-06 Achates Power, Inc. Opposed-piston engine structure with a split cylinder block
US9915188B2 (en) 2015-02-27 2018-03-13 Achates Power, Inc. Hybrid opposed-piston engine system
US10329996B2 (en) 2015-02-27 2019-06-25 Achates Power, Inc. Hybrid opposed-piston engine system
US11598259B2 (en) 2019-08-29 2023-03-07 Achates Power, Inc. Hybrid drive system with an opposed-piston, internal combustion engine
US11982225B2 (en) 2019-08-29 2024-05-14 Achates Power, Inc. Hybrid drive system with an opposed-piston, internal combustion engine

Similar Documents

Publication Publication Date Title
US2031318A (en) Engine
US2199625A (en) Double-piston internal combustion engine
US1410019A (en) Internal-combustion engine
US1736639A (en) Driving mechanism for internal-combustion engines
US1875838A (en) Internal combustion engine
US2781749A (en) Opposed piston sleeve valve outboard motor
GB172617A (en) Improvements in driving gear for engines
US1680017A (en) Two-stroke engine of the opposed-piston type
US2103787A (en) Internal combustion engine
US1304129A (en) Engine
US1191827A (en) Internal-combustion engine.
US2367963A (en) Two-cycle sleeve-valve engine
US1997396A (en) Crankless mechanism
US2342410A (en) Two-shaft opposed-piston internal combustion engine
US2347521A (en) Device for reducing torsional oscillations
US660679A (en) Balancing engine or motor.
US1679958A (en) Internal-combustion engine
US3521615A (en) Internal combustion engine
US1615895A (en) Internal-combustion engine
US2790431A (en) Camshaftt gear for internal combustioin engines
US1361619A (en) Internal-combustion engine
US2043529A (en) Internal combustion engine
US1671796A (en) Internal-combustion engine
US2350626A (en) Internal-combustion engine
SU14309A1 (en) Internal combustion engine