DE739663C - Self-igniting, air-compressing internal combustion engine - Google Patents
Self-igniting, air-compressing internal combustion engineInfo
- Publication number
- DE739663C DE739663C DEV37041D DEV0037041D DE739663C DE 739663 C DE739663 C DE 739663C DE V37041 D DEV37041 D DE V37041D DE V0037041 D DEV0037041 D DE V0037041D DE 739663 C DE739663 C DE 739663C
- Authority
- DE
- Germany
- Prior art keywords
- recess
- combustion engine
- internal combustion
- air
- antechamber
- 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
Links
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
- F02B19/00—Engines characterised by precombustion chambers
- F02B19/02—Engines characterised by precombustion chambers the chamber being periodically isolated from its cylinder
-
- 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
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
Selbstzündende, luftverdichtende Brennkraftmaschine Selbstzündende, luftverdichtende Brennkraftmaschine mit einer vom Hubraum durch ein bewegliches Abschlußorgan zeitweise getrennten Vorkarnmer, bei der der durch eine Niederdruckpumpe zugebrachte flüssige Brennstoff in dem Abschlußorgan eingelagert sowie von der während des Verdichtungshubes in die Vorkammer strömenden Luft dorthin mitgenommen und in der Vorkammer gezündet wird, sind bereits bekannt.Self-igniting, air-compressing internal combustion engine Self-igniting, Air-compressing internal combustion engine with one of the displacement through a movable Closing organ temporarily separated antechamber, in which the by a low pressure pump Brought liquid fuel stored in the closure member as well as from the during of the compression stroke in the antechamber air flowing there and in the antechamber is ignited are already known.
Bei den bekannten Maschinen wurde jedoch als Abschlußorgan ein Schieber mit hin und her gehender Bewegung verwandt. Demgegenüber besteht die vorliegende Erfindung nun darin, daß das Abschlußorgan als rotierende Welle mit einer zur Einlagerung des flüssigen Brennstoffes dienenden Aussparung ausgebildet ist.In the known machines, however, a slide was used as the closing element related to moving back and forth. In contrast, there is the present Invention now is that the closure member as a rotating shaft with a storage of the liquid fuel serving recess is formed.
Der Erfindungsgegenstand hat gegenüber der bekannten Einrichtung vor allem den Vorteil, daß durch die rotierende Welle die ruckweise hin und her gehende Bewegung des bisher verwandten Schiebers vermieden ist.The subject of the invention has before the known device all the advantage that the rotating shaft jerks back and forth Movement of the previously used slide is avoided.
Weiterhin kann der Antrieb des Abschluß-und Brennstoffeinlagerorgans ,auf diese Weise einfacher gehalten werden. Durch die Anordnung gemäß der Erfindung wird weiter eine gute Mitnahme, Zerstäubung und Mischung des Brennstoffes mit der heißen Luft in der Vorkammer gewährleistet.Furthermore, the drive of the closure and fuel storage element , can be kept simpler that way. By the arrangement according to the invention is further a good entrainment, atomization and mixing of the fuel with the guaranteed hot air in the antechamber.
In der Zeichnung ist ein Ausführungsbeispiel einer Brennkraftmaschine mit den Merkmalen gemäß der Erfindung dargestellt.The drawing shows an embodiment of an internal combustion engine shown with the features according to the invention.
Fig. i zeigt einen Schnitt durch Zylinder und Welle.Fig. I shows a section through the cylinder and shaft.
Fig. a stellt einen Schnitt nach der Linie II-II der Fig. i dar.Fig. A shows a section along the line II-II of Fig. I.
Fig. 3 zeigt einen Schnitt durch die Welle in vergrößertem Maßstabe.Fig. 3 shows a section through the shaft on an enlarged scale.
Fig..I stellt den Schnitt nach der Linie IV-IV der Fig. 3 dar.Fig..I shows the section along the line IV-IV of FIG.
Die Welle i ist in der Hohlwelle 7 gelagert. Die Hohlwelle ist mit einer Aussparung 2 versehen, in welche das an der Welle i angeschraubte Prisinenstück 8 eingreift.The shaft i is mounted in the hollow shaft 7. The hollow shaft is with a recess 2 is provided, in which the prism piece screwed to the shaft i 8 intervenes.
Durch Verschieben des Prismenstückes 8 in der länglichen Aussparung 2 der Hohlwelle ; kann der Raum der Aussparung verändert werden.By moving the prism piece 8 in the elongated recess 2 of the hollow shaft; the space of the recess can be changed.
Dicht neben der Welle i und dein Verbindungskanal 3 zum Zylinder. befindet sich die Vorkammer 5.Close to the shaft i and your connecting channel 3 to the cylinder. the antechamber 5 is located.
Das durch den Kanal 6 zufließende Öl iviid der Aussparung 2 zugeleitet und aus dieser von dem durch den Kanal 3 hindurchtretenden Strom der verdichteten Luft herausgerissen, um sich in der Kammer 5, irr der die Zündung erfolgt, durch Wirbelung innig mit der verdichteten Luft zu mischen. The oil flowing in through the channel 6 is fed to the recess 2 and torn out of this by the stream of compressed air passing through the channel 3 in order to mix intimately with the compressed air by vortexing in the chamber 5, where the ignition takes place .
Claims (1)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DEV37041D DE739663C (en) | 1940-10-08 | 1940-10-08 | Self-igniting, air-compressing internal combustion engine |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DEV37041D DE739663C (en) | 1940-10-08 | 1940-10-08 | Self-igniting, air-compressing internal combustion engine |
Publications (1)
Publication Number | Publication Date |
---|---|
DE739663C true DE739663C (en) | 1943-10-01 |
Family
ID=7590270
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DEV37041D Expired DE739663C (en) | 1940-10-08 | 1940-10-08 | Self-igniting, air-compressing internal combustion engine |
Country Status (1)
Country | Link |
---|---|
DE (1) | DE739663C (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2827883A (en) * | 1956-04-24 | 1958-03-25 | Goede Henri | Internal combustion engine |
-
1940
- 1940-10-08 DE DEV37041D patent/DE739663C/en not_active Expired
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2827883A (en) * | 1956-04-24 | 1958-03-25 | Goede Henri | Internal combustion engine |
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