US1865841A - Oil engine - Google Patents

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Publication number
US1865841A
US1865841A US433603A US43360330A US1865841A US 1865841 A US1865841 A US 1865841A US 433603 A US433603 A US 433603A US 43360330 A US43360330 A US 43360330A US 1865841 A US1865841 A US 1865841A
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Prior art keywords
piston
chamber
air
spray
conical
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Expired - Lifetime
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US433603A
Inventor
Clessie L Cummins
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OIL ENGINE DEV Co
OIL ENGINE DEVELOPMENT Co
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OIL ENGINE DEV Co
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Priority to US433603A priority Critical patent/US1865841A/en
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Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B23/00—Other engines characterised by special shape or construction of combustion chambers to improve operation
    • F02B23/02—Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition
    • F02B23/06—Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition the combustion space being arranged in working piston
    • F02B23/0618—Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition the combustion space being arranged in working piston having in-cylinder means to influence the charge motion
    • F02B23/0627—Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition the combustion space being arranged in working piston having in-cylinder means to influence the charge motion having additional bores or grooves machined into the piston for guiding air or charge flow to the piston bowl
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B23/00—Other engines characterised by special shape or construction of combustion chambers to improve operation
    • F02B23/02—Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition
    • F02B23/06—Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition the combustion space being arranged in working piston
    • F02B23/0696—W-piston bowl, i.e. the combustion space having a central projection pointing towards the cylinder head and the surrounding wall being inclined towards the cylinder wall
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B23/00—Other engines characterised by special shape or construction of combustion chambers to improve operation
    • F02B23/02—Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition
    • F02B23/06—Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition the combustion space being arranged in working piston
    • F02B23/0618—Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition the combustion space being arranged in working piston having in-cylinder means to influence the charge motion
    • F02B23/063—Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition the combustion space being arranged in working piston having in-cylinder means to influence the charge motion the combustion space in the piston interacting fluid dynamically with the cylinder head, the injector body or the cylinder wall
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B23/00—Other engines characterised by special shape or construction of combustion chambers to improve operation
    • F02B23/02—Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition
    • F02B23/06—Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition the combustion space being arranged in working piston
    • F02B23/0645—Details related to the fuel injector or the fuel spray
    • F02B23/0648—Means or methods to improve the spray dispersion, evaporation or ignition
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B3/00—Engines characterised by air compression and subsequent fuel addition
    • F02B3/06—Engines characterised by air compression and subsequent fuel addition with compression ignition
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T10/00—Road transport of goods or passengers
    • Y02T10/10—Internal combustion engine [ICE] based vehicles
    • Y02T10/12—Improving ICE efficiencies

Definitions

  • My invention relates .to oil burning engines.
  • the principal object of my invention is t0 provide for pro erdistribution and adL 6 mixture of the fuell) charge throughout the' air in the combustion s ace with the result that more perfect com ustion takes place, the eiiiciene7 of the engine being thusgreat ly improve l 1Q
  • Another object of my invention is to provide an auxiliary air chamber projecting from the head of the piston anl constructed and arran edwith respect to the ejector so that the a1r chamber supplies substantially l fresh air to the zone adjacent the end of the ejector and the charge of fuel ejected by the ejector is not sprayed against the casing forming the air chamber.
  • the fuel injector in general, is similar to that .disclosed in my U. S. Patents. No. 1,561,913 and No. 1,762,653, and may comprise a body member orplug 10, an inject ing plunger 11 operable in a central bore 12.
  • theA plunger 11 is lowered byany suitable means, to eject o lower projecting end of the injector and the surrounding surface of thecylinder head, I provide an auxiliary air chamber 27 on the piston head.
  • the head of the piston is provided with bore 28 having its upper portion threaded.
  • a hollow member 29 has its upper portion vconical shaped and its lower cylindrical por- 'tion is externally threaded and screwed into the threaded portion of the bore 28.
  • the member 29 together with the lower part of the bore 28 forms the air chamber 27 which is closed except for a nozzle or opening 30 at the upper end of the conical portion of the member 29.
  • the upper end of the piston has an upwardly extending circumferential rim 32 which is fiat on its upper face. Vhen the ⁇ A piston is at the end of its compression stroke, as shown in the drawing, the clearance between the fiat face of the rim 32 and the bottom face of the cylinder head is as small as practical, the rim being recessed at 33v to clear the exhaust and inlet valves 5 and 6.
  • the chamber being formed around the cas- 1n ⁇ 1219 by the rim 32.
  • e line broken lines 35 indicate approximately the spray of the fuel charge ejected radiatingly through the ports 24 in the ejector.
  • the spray is conical in shapeand generally speaking, the contour of the chamber 34 is such as to conform to -the shape of the spray so that the spray is Well distributed without directly striking the casing 29, cylinder head or piston.l
  • the turbulence of the air set up by the rim 32 and the action of the air chamber aids in furthering the distribution. I have found that it is highly beneficial to keep the spray from striking the projecting casing 29 forming the air chamber. As this casing projects into the combustion chamber it becomes very hot and should part of the spray strike it, its top would burn off and its life thus shortened and the efficiency of the engine impaired.
  • I would refer here to the conical space within the center of the spray (i. e., between the lines marked A and B in the drawing) as the zone within the fuel spray.
  • the length of the fuel spray is somewhat limited as the charge is injected at a time when the air in the combustion space is highly compressed.
  • the width of the rim 32 may be widened so that the diameter of the chamber 34 is generally such as to accommodate the length of the fuel spray, the chamber being deepened to accommodate the compressed air andthe increased conical spread of the spray.
  • a fuel ejector havingY an end projecting into the combustion space and adapted to inject the fuel charge radiatingly into the combustion space in the form of a conical spray at about the end of the compression stroke of the piston, an auxiliary air chamber on the head of the piston, projecting into the combustion space and having an opening in close proximity to and in axial alignment with the projecting end of the injector at the end of the compression stroke of the piston, the direction of the conical spray and the shape and the projecting end of the air chamber being so related that the spray does not contact; with the wall of said chamber.
  • a cylinder and a piston operable therein, of a fuel injector having an end projecting into the combustion space and provided-with aplurality of restricted radiating ports through which the fuel charge is sprayedin the form of a cone, an auxiliary air chamber on the head of the piston, projecting into' the combustion space and having a conical end with an opening in the apex thereof, the conical end beingiwholly in the conical zone within the fuel spray at the end of the compression stroke of the piston so that the fuel is not sprayed on the walls of the chamber.
  • Y posed to the head of said piston, means carv ried ⁇ by the iston head substantiall in alignment wit said conical space an defining an auxiliary air chamber, said chamber-delim'ng means having a conicallyshaped outenwall within said conical space of lesser dimensions than said conical space, said ejector end and piston being so related that said chamber-defining means does not directly contact said spray in any operable position of said piston.

Description

rate-naaien s, 1932 'UNITED STATI-:s
cmssm L. GUmS, F COLUMBUS, INDlANA, `ASSIGNOB. T0 OIL'ENGINE DEVENE- HENT COMM, OF COLUMBUS, A CORPORATION 0Fv INDIANA on. ENGINE .Anuman meca maren e,
My invention relates .to oil burning engines. V The principal object of my invention is t0 provide for pro erdistribution and adL 6 mixture of the fuell) charge throughout the' air in the combustion s ace with the result that more perfect com ustion takes place, the eiiiciene7 of the engine being thusgreat ly improve l 1Q Another object of my invention is to provide an auxiliary air chamber projecting from the head of the piston anl constructed and arran edwith respect to the ejector so that the a1r chamber supplies substantially l fresh air to the zone adjacent the end of the ejector and the charge of fuel ejected by the ejector is not sprayed against the casing forming the air chamber. v
. With the above and incidental objects Iin 2"- view, the invention consists of certain novel features of construction and combination of parts, the essential elements whereof are recited in the a pended claims and the ypre-- ferrediorm o embodiment of which is described in detail hereinafter and illustrated ,in full in the accompanying drawing, which4 forms part of4 this specification. Y Said drawing illustrates, in section, part of a cylinder head 2 and the upper parts of a cylinder 3 and reciprocatin piston 4 of a four-cycle engine of the ummins type to which for the purpose of illustration, I have shown the preferred form of embodi-j ment of my invention applied. An air intake valve 5 and an exhaust valve 6, which is shown broken away at its lower end, may be of any improved construction. The upper end of the cylinder wall is provided with recesses 7 to accommodate movement of these 4 valves. j
The fuel injector, in general, is similar to that .disclosed in my U. S. Patents. No. 1,561,913 and No. 1,762,653, and may comprise a body member orplug 10, an inject ing plunger 11 operable in a central bore 12.
'cup-shaped member 13, so that when the 1930. Serial No. 433,603.
of the plug, an inner cup-shaped member 13 Iitting over and about the lower end of the pli/1g 10, a second cup-shaped member 14 of generally similar shape, tting over the member 13, and a third or outer cup-shaped insulating member 15 fitting over the member 14. The lower end of the central bore 12 in the plug vis closed, except for a small opening` 18, by the lower conical end of the plunger 11 isretracted or elevated to the position illustrated in Fig. 1` an` atomizing or mixing chamber 19 is formed under the plunger. A charge of fuel oil is fed to the mixing chamber 19 through a conduit 21 in the plug 10 and passa es 22 formed-between the cups'13 and 14. he lowerprotruding end of the cup 14 extends through a centra openingin the' cup'15 and is provided with l very restricted ports 24 communicating with the combustion chamber of the engine. The
inner conical surface of the lower end of the cup 15 has a close grounded fit with the bottom conical surface of the cup 14.
lThe operation of the injecting mechanism is preferably aboutvthe same as that described in my aforesaid PatentvNo."1,561,913. During the suction stroke of the piston 4, air is drawn into the cylinder. past the air inlet valvel 5 and durng the same stroke a charge of-fuel oil is forced in any desirable manner from the passages 22 between the cups 13 and 14 into the pointed end of the mixing chamber 19. While the liquid charge of oily is being deposited in the lower end of the chamber 19 the plungerll is slowly elevated.
During the compression stroke of the piston, i
part of the heated air, compressed inthe .combustion space of the cylinder and heated due to its compression, is forced to How through the ports 24 and 18 into the chamber 19 where the oil is entrained and thoroughly mixed with the air. i Near the beginning of the power stroke of the piston, theA plunger 11 is lowered byany suitable means, to eject o lower projecting end of the injector and the surrounding surface of thecylinder head, I provide an auxiliary air chamber 27 on the piston head. The head of the piston is provided with bore 28 having its upper portion threaded.
A hollow member 29 has its upper portion vconical shaped and its lower cylindrical por- 'tion is externally threaded and screwed into the threaded portion of the bore 28. The member 29 together with the lower part of the bore 28 forms the air chamber 27 which is closed except for a nozzle or opening 30 at the upper end of the conical portion of the member 29. p
As fully explained in my Patent No. 1,762,653, during the compression stroke of the piston air from the combustion space is forced into the air chamber 27 through its opening 30 and during the combustion stroke this air in the chamber which is relatively pure, rushes out through the opening 30, to feed fresh air to theV zone around the lower end of the ejector, thus effecting improved distribution and admixture, better combustion and the elimination of carbon deposit on the projecting end of the ejector.
The upper end of the piston has an upwardly extending circumferential rim 32 which is fiat on its upper face. Vhen the`A piston is at the end of its compression stroke, as shown in the drawing, the clearance between the fiat face of the rim 32 and the bottom face of the cylinder head is as small as practical, the rim being recessed at 33v to clear the exhaust and inlet valves 5 and 6.
As the piston approaches top center on the compression stroke, the air above the rim 32 1s driven towards the center of the cylinder from all directions thus setting up a turbulence of the air within the combustion space, which at the end of the compression stroke, is formed almost wholly by the annular chamber 34 in the upper end of the piston,
the chamber being formed around the cas- 1n`1219 by the rim 32.
e line broken lines 35 indicate approximately the spray of the fuel charge ejected radiatingly through the ports 24 in the ejector. The spray is conical in shapeand generally speaking, the contour of the chamber 34 is such as to conform to -the shape of the spray so that the spray is Well distributed without directly striking the casing 29, cylinder head or piston.l The turbulence of the air set up by the rim 32 and the action of the air chamber aids in furthering the distribution. I have found that it is highly beneficial to keep the spray from striking the projecting casing 29 forming the air chamber. As this casing projects into the combustion chamber it becomes very hot and should part of the spray strike it, its top would burn off and its life thus shortened and the efficiency of the engine impaired. For convenience, I would refer here to the conical space within the center of the spray (i. e., between the lines marked A and B in the drawing) as the zone within the fuel spray.
, The length of the fuel spray is somewhat limited as the charge is injected at a time when the air in the combustion space is highly compressed. As the size of the engine cylinder increases in diameter the width of the rim 32 may be widened so that the diameter of the chamber 34 is generally such as to accommodate the length of the fuel spray, the chamber being deepened to accommodate the compressed air andthe increased conical spread of the spray.
I claim:
l. In an oil burning engine, the combination of a cylinder and a piston operable therein, of a fuel ejector havingY an end projecting into the combustion space and adapted to inject the fuel charge radiatingly into the combustion space in the form of a conical spray at about the end of the compression stroke of the piston, an auxiliary air chamber on the head of the piston, projecting into the combustion space and having an opening in close proximity to and in axial alignment with the projecting end of the injector at the end of the compression stroke of the piston, the direction of the conical spray and the shape and the projecting end of the air chamber being so related that the spray does not contact; with the wall of said chamber.
2. In an oil burning engine, the combination of a cylinder and a piston operable therein, of a fuel injector having an end projecting into the combustion space and provided-with aplurality of restricted radiating ports through which the fuel charge is sprayedin the form of a cone, an auxiliary air chamber on the head of the piston, projecting into' the combustion space and having a conical end with an opening in the apex thereof, the conical end beingiwholly in the conical zone within the fuel spray at the end of the compression stroke of the piston so that the fuel is not sprayed on the walls of the chamber.
Y posed to the head of said piston, means carv ried `by the iston head substantiall in alignment wit said conical space an defining an auxiliary air chamber, said chamber-delim'ng means having a conicallyshaped outenwall within said conical space of lesser dimensions than said conical space, said ejector end and piston being so related that said chamber-defining means does not directly contact said spray in any operable position of said piston.
,In testimony whereof, I have subscribed my name. d
CLESSIE L. CUMMINS.
US433603A 1930-03-06 1930-03-06 Oil engine Expired - Lifetime US1865841A (en)

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Cited By (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2662510A (en) * 1950-12-18 1953-12-15 Louis O French Compression ignition internal-combustion engine
US5099809A (en) * 1989-08-09 1992-03-31 Mitsubishi Jidosha Kogyo Kabushiki Kaisha Combustion chamber for a diesel engine
EP0589178A1 (en) * 1992-08-27 1994-03-30 MAN Nutzfahrzeuge Aktiengesellschaft Shape of the combustion chamber for air compressing, self-ignited engines
US5322042A (en) * 1992-06-17 1994-06-21 Sonex Research, Inc. Combustion chamber for internal combustion engine and process of combustion using fuel radical species
US5553588A (en) * 1994-07-27 1996-09-10 Toyota Jidosha Kabushiki Kaisha Spark-ignited direct cylinder fuel injection engine
US5868112A (en) * 1996-12-19 1999-02-09 Cummins Engine Company, Inc. Deep angle injection nozzle and piston having complementary combustion bowl
US6732703B2 (en) 2002-06-11 2004-05-11 Cummins Inc. Internal combustion engine producing low emissions
US20060070603A1 (en) * 2002-06-11 2006-04-06 Cummins Inc. Internal combustion engine producing low emissions
US8677970B2 (en) 2011-03-17 2014-03-25 Cummins Intellectual Property, Inc. Piston for internal combustion engine
US20160298529A1 (en) * 2015-04-13 2016-10-13 Caterpillar Inc. Ducted Combustion Systems Utilizing Duct Structures

Cited By (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2662510A (en) * 1950-12-18 1953-12-15 Louis O French Compression ignition internal-combustion engine
US5099809A (en) * 1989-08-09 1992-03-31 Mitsubishi Jidosha Kogyo Kabushiki Kaisha Combustion chamber for a diesel engine
US5322042A (en) * 1992-06-17 1994-06-21 Sonex Research, Inc. Combustion chamber for internal combustion engine and process of combustion using fuel radical species
EP0589178A1 (en) * 1992-08-27 1994-03-30 MAN Nutzfahrzeuge Aktiengesellschaft Shape of the combustion chamber for air compressing, self-ignited engines
US5553588A (en) * 1994-07-27 1996-09-10 Toyota Jidosha Kabushiki Kaisha Spark-ignited direct cylinder fuel injection engine
US5868112A (en) * 1996-12-19 1999-02-09 Cummins Engine Company, Inc. Deep angle injection nozzle and piston having complementary combustion bowl
US6732703B2 (en) 2002-06-11 2004-05-11 Cummins Inc. Internal combustion engine producing low emissions
US20040182358A1 (en) * 2002-06-11 2004-09-23 Cummins Inc. Internal combustion engine producing low emissions
US6966294B2 (en) 2002-06-11 2005-11-22 Cummins Inc. Internal combustion engine producing low emissions
US20060070603A1 (en) * 2002-06-11 2006-04-06 Cummins Inc. Internal combustion engine producing low emissions
US7210448B2 (en) 2002-06-11 2007-05-01 Cummins, Inc. Internal combustion engine producing low emissions
US8677970B2 (en) 2011-03-17 2014-03-25 Cummins Intellectual Property, Inc. Piston for internal combustion engine
USRE46806E1 (en) 2011-03-17 2018-04-24 Cummins Intellectual Property, Inc. Piston for internal combustion engine
US20160298529A1 (en) * 2015-04-13 2016-10-13 Caterpillar Inc. Ducted Combustion Systems Utilizing Duct Structures
US9803538B2 (en) * 2015-04-13 2017-10-31 Caterpillar Inc. Ducted combustion systems utilizing duct structures

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