US1767701A - Internal-combustion engine of the solid-fuel injection type - Google Patents

Internal-combustion engine of the solid-fuel injection type Download PDF

Info

Publication number
US1767701A
US1767701A US62040A US6204025A US1767701A US 1767701 A US1767701 A US 1767701A US 62040 A US62040 A US 62040A US 6204025 A US6204025 A US 6204025A US 1767701 A US1767701 A US 1767701A
Authority
US
United States
Prior art keywords
oil
ignition
fuel
solid
combustion 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
US62040A
Inventor
Riehm Wilhelm
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.)
MAN AG
Original Assignee
MAN Maschinenfabrik Augsburg Nuernberg AG
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 MAN Maschinenfabrik Augsburg Nuernberg AG filed Critical MAN Maschinenfabrik Augsburg Nuernberg AG
Application granted granted Critical
Publication of US1767701A publication Critical patent/US1767701A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02F—CYLINDERS, PISTONS OR CASINGS, FOR COMBUSTION ENGINES; ARRANGEMENTS OF SEALINGS IN COMBUSTION ENGINES
    • F02F1/00—Cylinders; Cylinder heads 
    • F02F1/24—Cylinder heads
    • F02F1/242—Arrangement of spark plugs or injectors
    • 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
    • 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

Definitions

  • This invention relates to internal combustion engines of the solid fuel injection type.
  • An arrangement of two separate fuel valves in internal combustion engines with air infsjection working on two different fuels, a light igniting oil and a heavier combustible oil, is known. It is also known in internal combustion engines with airless spray (i. e.
  • the present invention employs the first 2 mentioned arrangement and avoids the disadvantages resulting from the use of the airless spray or solid injection of the heavy oil, by using the said arrangement in conjunction with a known rotary or circulatory movement of the combustion air.
  • the ignition oil nozzles and the heavy oil nozzles are arranged in such a way that the flames from the ignition oil are driven towards the sprays of the heavy oil and strike the latter at the moment most suitable for ignition.
  • the ignition oil nozzles may be situated in front of the heavy oil nozzles and arranged laterally in the cylinder, but they can in certain cases be situated centrally in the cylinder cover.
  • Fig. 1 shows the arrangement with both fuel nozzles arranged laterally or adjacent the side wall of the cylinder
  • Fig.2 shows the light fuel nozzle arranged centrally.
  • a is the air inlet valve, which by way of example is provided with a screen I) for imparting to the ingoing air a rotary or circulatory movement as indicated by the arrows g.
  • the light oil fuel streamfrom the nozzle 6 isin small angular advance of the heavy oil stream, such angular advance being coordinated with the rotational speed of the air.
  • the front oil stream has an effective angular advance of substantially less than with reference to the rear oil stream.
  • the light oil fuel stream from the nozzle 6 being in front of the heavy oil stream from the nozzle 0 and thereby acting somewhat as a shield for the heavy oil stream, is more forcefully acted upon by the rotating air, and is driven more rapidly than the heavy oil in the direction of rotation of th air.
  • This serves to carry the light ignition oil into the path of movement of the heavy oil substantially throughout the extent of the heavy oil stream very shortly after the time of injection of the light oil. This secures an intimate mixing of the light oil flames at the time of their greatest heat intensity with heavy oil throughout a large part of the heavy oil stream, thereby securing highly effective ignition of the heavy oil stream and an efficient combustion within the cylinder.
  • FIG. 2 differs from the above only in so far that a central nozzle i'having a number of openings 71 for the ignition oil sprays is placed centrally in the cover of the cylinder. -The number of such openings 1 will depend upon the number of the heavy oil nozzles 0. These openings are so directed that the ignition oil is introduced in streams which lie closely adjacent and in front of the heavy 5 oil streams, whereby the ignition oil flames indicated by the arrows h are driven by the rotating or circulating air against the heavy oil sprays and strike them at the most favourable moment for ignition.
  • the invention is based essentially on the fact that the ignition of the ignition oil does not extend instantaneously through the whole combustionchamber but occurs 10-. cally and that therefore it is at such local spots that the most suitable temperature for the ignition of the heavy oil is to be found. Thus combustion of the heavy oil is made 'possible by a minimum consumption of ignition oil.
  • An internal combustion engine of the character described comprising, in combination, a cylinder having a combustion space therein, means for introducing combustion 5 air into said combustion space "and for imparting rotary motion thereto, means for injecting a heavy combustible fuel into said combustion space, and means for injecting a light ignition fuel into said combustion space in a separate but closely adjacent stream in small angular advance of said combustible fuel, whereby the rotating combustion air carries said ignition fuel into contact with said combustible fuel shortly after injection and during'the time of ignition of said ignition fuel.
  • the method which comprises introducing combustion air into the cylinder and imparting rotary motion thereto, injecting a combustible fuel oil into the moving air within said cylinder, and injecting a lighter and readily ignitible ignition fuelinto the moving air within said 4 cylinder along a separate but closely contignous path on the same cylinder side and in front of the combustible fuel oil, the positioning of the se arate streams within the combustion space eing coordinated with the rotational speed of the air such that the rotating combustion air carries the ignited ignition fuel into contact with said combustible fuel oil shortly after injection andoat the time of burning of said ignition fuel to inlsure combustion of such combustible fuel In testimony whereof I have hereto aflixed my signature.

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Combustion Methods Of Internal-Combustion Engines (AREA)

Description

w. RIEHM 1,767,701 INTERNAL COMBUSTION ENGINE OF THE SOLID FUEL INJECTION TYPE June 24, 1930.
Filed Oct. 12, 1925 Patented June 24, 1930 UNITED STATES PATENT OFFICE' WILHELM RIEHM, OF AUGSBURG, GERMANY, ASSIGNOR TO MASCHINENFABRIK AUGS- BURG-N'UERNBERG, AKTIENGESELLSCHAFT, OF AUGSBURG, GERMANY, .A. GERMAN CORPORATION INTERNAL-COMBUSTION ENGINE OF THE SOLID-FUEL INJECTION 'IY'PE Application filed. October 12,1925, Serial No. 62,040, and in Germany October 25, 1924.
This invention relates to internal combustion engines of the solid fuel injection type. An arrangement of two separate fuel valves in internal combustion engines with air infsjection working on two different fuels, a light igniting oil and a heavier combustible oil, is known. It is also known in internal combustion engines with airless spray (i. e.
engines of the solid fuel injection type) to I! arrange the separate pipes for both fuels within the body of a nozzle'and to direct the fuel sprays in such a way that the heavy oil spray meets the ignition oil spray at a point suitable for ignition. This latter arrange- 5. ment has proved, generally, unsuitable, be-
cause the nozzle is too large in comparison with the cylinder and takes up so much space that it cannot be accommodated.
The present invention employs the first 2 mentioned arrangement and avoids the disadvantages resulting from the use of the airless spray or solid injection of the heavy oil, by using the said arrangement in conjunction with a known rotary or circulatory movement of the combustion air. In this invention the ignition oil nozzles and the heavy oil nozzles are arranged in such a way that the flames from the ignition oil are driven towards the sprays of the heavy oil and strike the latter at the moment most suitable for ignition. The ignition oil nozzles may be situated in front of the heavy oil nozzles and arranged laterally in the cylinder, but they can in certain cases be situated centrally in the cylinder cover.
Each of the above-mentioned forms of the invention is shown diagrammatically in the drawing in which Fig. 1 shows the arrangement with both fuel nozzles arranged laterally or adjacent the side wall of the cylinder, and Fig.2 shows the light fuel nozzle arranged centrally.
a is the air inlet valve, which by way of example is provided with a screen I) for imparting to the ingoing air a rotary or circulatory movement as indicated by the arrows g.
In the construction according to Figure 1 there are arranged laterally in the wall of the cylinder and diametrically opposite so that proper ignition of the heavy oil is assured. As shown clearly in the drawing, the nozzles c and e for the heavy oil and the light oil respectively have discharge ports so arranged as to direct the streams into the combustion space of the cylinder in closely adjacent and converging paths. The
light oil fuel streamfrom the nozzle 6 isin small angular advance of the heavy oil stream, such angular advance being coordinated with the rotational speed of the air. As shown, the front oil stream has an effective angular advance of substantially less than with reference to the rear oil stream. The light oil fuel stream from the nozzle 6 being in front of the heavy oil stream from the nozzle 0 and thereby acting somewhat as a shield for the heavy oil stream, is more forcefully acted upon by the rotating air, and is driven more rapidly than the heavy oil in the direction of rotation of th air. This serves to carry the light ignition oil into the path of movement of the heavy oil substantially throughout the extent of the heavy oil stream very shortly after the time of injection of the light oil. This secures an intimate mixing of the light oil flames at the time of their greatest heat intensity with heavy oil throughout a large part of the heavy oil stream, thereby securing highly effective ignition of the heavy oil stream and an efficient combustion within the cylinder.
The arrangement shown in Figure 2 differs from the above only in so far that a central nozzle i'having a number of openings 71 for the ignition oil sprays is placed centrally in the cover of the cylinder. -The number of such openings 1 will depend upon the number of the heavy oil nozzles 0. These openings are so directed that the ignition oil is introduced in streams which lie closely adjacent and in front of the heavy 5 oil streams, whereby the ignition oil flames indicated by the arrows h are driven by the rotating or circulating air against the heavy oil sprays and strike them at the most favourable moment for ignition.
The invention is based essentially on the fact that the ignition of the ignition oil does not extend instantaneously through the whole combustionchamber but occurs 10-. cally and that therefore it is at such local spots that the most suitable temperature for the ignition of the heavy oil is to be found. Thus combustion of the heavy oil is made 'possible by a minimum consumption of ignition oil.
What is claimed is:
1. An internal combustion engine of the character described comprising, in combination, a cylinder having a combustion space therein, means for introducing combustion 5 air into said combustion space "and for imparting rotary motion thereto, means for injecting a heavy combustible fuel into said combustion space, and means for injecting a light ignition fuel into said combustion space in a separate but closely adjacent stream in small angular advance of said combustible fuel, whereby the rotating combustion air carries said ignition fuel into contact with said combustible fuel shortly after injection and during'the time of ignition of said ignition fuel.
2. In the operation of an internal combustion engine using fuel injection, the method which comprises introducing combustion air into the cylinder and imparting rotary motion thereto, injecting a combustible fuel oil into the moving air within said cylinder, and injecting a lighter and readily ignitible ignition fuelinto the moving air within said 4 cylinder along a separate but closely contignous path on the same cylinder side and in front of the combustible fuel oil, the positioning of the se arate streams within the combustion space eing coordinated with the rotational speed of the air such that the rotating combustion air carries the ignited ignition fuel into contact with said combustible fuel oil shortly after injection andoat the time of burning of said ignition fuel to inlsure combustion of such combustible fuel In testimony whereof I have hereto aflixed my signature.
- DR. VVILHELM RIEHM.
US62040A 1924-10-25 1925-10-12 Internal-combustion engine of the solid-fuel injection type Expired - Lifetime US1767701A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE1767701X 1924-10-25

Publications (1)

Publication Number Publication Date
US1767701A true US1767701A (en) 1930-06-24

Family

ID=7742444

Family Applications (1)

Application Number Title Priority Date Filing Date
US62040A Expired - Lifetime US1767701A (en) 1924-10-25 1925-10-12 Internal-combustion engine of the solid-fuel injection type

Country Status (1)

Country Link
US (1) US1767701A (en)

Cited By (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2443502A (en) * 1941-02-08 1948-06-15 Constantine N Guerasimoff Engine construction
US2484009A (en) * 1948-02-25 1949-10-11 Texas Co Internal-combustion engine and method of operating same
US2595915A (en) * 1947-04-18 1952-05-06 Texas Co Internal-combustion engine
US2692587A (en) * 1952-06-23 1954-10-26 Texas Co Internal-combustion engine
DE2849778A1 (en) * 1977-11-23 1979-05-31 Volvo Ab FUEL INJECTION FOR COMBUSTION ENGINES ACCORDING TO THE DIESEL PRINCIPLE
US4368702A (en) * 1979-01-13 1983-01-18 Klockner-Humboldt-Deutz Aktiengesellschaft Method of operating an air-compressing, self-igniting internal combustion engine
US4370958A (en) * 1979-01-13 1983-02-01 Franz Pischinger Method of operating an air-compressing, self-igniting engine for liquid fuel
US4549511A (en) * 1981-12-24 1985-10-29 Robert Bosch Gmbh Fuel injection system for direct fuel injection in internal combustion engines
US4612898A (en) * 1985-01-11 1986-09-23 Sulzer Brothers Limited Cylinder head for a piston internal combustion engine
US4748949A (en) * 1985-02-05 1988-06-07 Sulzer Brothers Limited Method and system for injecting a pilot fuel into a combustion chamber
US5605127A (en) * 1994-05-27 1997-02-25 Mitsubishi Jukogyo Kabushiki Kaisha Cylinder cover for diesel engine
US6463890B1 (en) * 1998-01-23 2002-10-15 Wartsila Nsd Oy Ab Combined diesel-rankine cycle reciprocating engine

Cited By (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2443502A (en) * 1941-02-08 1948-06-15 Constantine N Guerasimoff Engine construction
US2595915A (en) * 1947-04-18 1952-05-06 Texas Co Internal-combustion engine
US2484009A (en) * 1948-02-25 1949-10-11 Texas Co Internal-combustion engine and method of operating same
US2692587A (en) * 1952-06-23 1954-10-26 Texas Co Internal-combustion engine
DE2849778A1 (en) * 1977-11-23 1979-05-31 Volvo Ab FUEL INJECTION FOR COMBUSTION ENGINES ACCORDING TO THE DIESEL PRINCIPLE
US4370958A (en) * 1979-01-13 1983-02-01 Franz Pischinger Method of operating an air-compressing, self-igniting engine for liquid fuel
US4368702A (en) * 1979-01-13 1983-01-18 Klockner-Humboldt-Deutz Aktiengesellschaft Method of operating an air-compressing, self-igniting internal combustion engine
US4463719A (en) * 1979-01-13 1984-08-07 Franz Pischinger Air-compressing, self-igniting engine for liquid fuel
US4549511A (en) * 1981-12-24 1985-10-29 Robert Bosch Gmbh Fuel injection system for direct fuel injection in internal combustion engines
US4612898A (en) * 1985-01-11 1986-09-23 Sulzer Brothers Limited Cylinder head for a piston internal combustion engine
US4748949A (en) * 1985-02-05 1988-06-07 Sulzer Brothers Limited Method and system for injecting a pilot fuel into a combustion chamber
US5605127A (en) * 1994-05-27 1997-02-25 Mitsubishi Jukogyo Kabushiki Kaisha Cylinder cover for diesel engine
US6463890B1 (en) * 1998-01-23 2002-10-15 Wartsila Nsd Oy Ab Combined diesel-rankine cycle reciprocating engine

Similar Documents

Publication Publication Date Title
US1767701A (en) Internal-combustion engine of the solid-fuel injection type
US4463719A (en) Air-compressing, self-igniting engine for liquid fuel
US3270722A (en) Method of conditioning liquid fuels
US2100143A (en) Internal combustion engine
US3661125A (en) Method and apparatus for adapting engine to stratified charge oepration
US3980059A (en) Internal combustion engine
US2269104A (en) Internal combustion engine
US1988754A (en) Internal combustion engine
US2753852A (en) Heavy oil internal combustion engines
US2921566A (en) Internal combustion engine and method of operating it
US4120273A (en) Starting aid for internal combustion engines
US2021744A (en) Internal-combustion engine of the fuel-injection type
US2019298A (en) Internal combustion engine
US1286435A (en) Internal-combustion engine.
USRE21750E (en) Internal combustion engine
US1235725A (en) Internal-combustion engine.
US1662553A (en) Internal-combustion engine
US2071241A (en) Internal combustion engine
US2345256A (en) Internal combustion engine of the solid injection type
US4338898A (en) Apparatus for distribution of fuel from an injection nozzle with respect to a piston in an air compressing internal combustion engine with direct fuel injection
US1939180A (en) Primary- combustion- or explosion-device for internal combustion engines
US1302653A (en) Internal-combustion engine.
US1772742A (en) Internal-combustion engine
US1833445A (en) Combustion chamber for internal combustion engines
US1758460A (en) Internal-combustion engine and method of operating the same