DE377063C - Air cooling for explosion engines - Google Patents

Air cooling for explosion engines

Info

Publication number
DE377063C
DE377063C DEG56354D DEG0056354D DE377063C DE 377063 C DE377063 C DE 377063C DE G56354 D DEG56354 D DE G56354D DE G0056354 D DEG0056354 D DE G0056354D DE 377063 C DE377063 C DE 377063C
Authority
DE
Germany
Prior art keywords
air cooling
cooling
explosion engines
air
capsule
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
Application number
DEG56354D
Other languages
German (de)
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.)
RICHARD GRUHN
Original Assignee
RICHARD GRUHN
Publication date
Priority to DEG56354D priority Critical patent/DE377063C/en
Application granted granted Critical
Publication of DE377063C publication Critical patent/DE377063C/en
Expired legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01PCOOLING OF MACHINES OR ENGINES IN GENERAL; COOLING OF INTERNAL-COMBUSTION ENGINES
    • F01P1/00Air cooling
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01MLUBRICATING OF MACHINES OR ENGINES IN GENERAL; LUBRICATING INTERNAL COMBUSTION ENGINES; CRANKCASE VENTILATING
    • F01M13/00Crankcase ventilating or breathing
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01PCOOLING OF MACHINES OR ENGINES IN GENERAL; COOLING OF INTERNAL-COMBUSTION ENGINES
    • F01P5/00Pumping cooling-air or liquid coolants

Landscapes

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

Description

Kühlung für Explosionskraftmaschinen durch Luft. Die Erfindung bezieht sich auf die Kühlung von Esplosionskraftmaschinen mittels der durch die Kolbenbewegungen angesaugten und durch das geschlossene Kurbelgehäuse gepreßten Luft, welche in bekannter Weise dein heißesten Teile der durch Rippen gekühlten Zylinderwand zugeführt wird.Air cooling for explosion engines. The invention relates on the cooling of esplosion engines by means of the piston movements sucked in and pressed through the closed crankcase air, which in known Way your hottest part is fed to the rib-cooled cylinder wall.

Der Zweck der Erfindung besteht darin, diese heißesten Teile, welche infolge der hohen Konipressionsteniperaturen der Zer->törung am meisten ausgesetzt sind, nicht nur wirksam zti kühlen, sondern auch ölfeucht zu erhalten. Daher wird nach vorliegender Erfindung die Külilluftrnenge, bevor sie dein Zylinder zugeführt wird. durch (las clbad @ler Räderkapsel für (las Steuerungsvorgelege geleitet, so claß die Luft mit einem Teil der :ich aus dein 011iali entwickelnden Dämpfe gesättigt wird.The purpose of the invention is to find these hottest parts, which most exposed to destruction as a result of the high compression stiffness are not only effective for cooling, but also to keep them moist. Hence will According to the present invention, the cooling air volume before it is supplied to the cylinder will. through (read clbad @ler gear capsule for (read control transmission, see above Let the air be saturated with some of the vapors that develop from your 011iali will.

Die Zeichnung stellt ein Ausführungsbeispiel einer reit der Luftkühlung gemäß der I?rfindung ausgerüsteten Ezplosionskraftniaschine in Abb. i in Gesamtansicht, in Abh.2 im senkrechten Schnitt dar. Abb.3 ist ein rechtwinklig zu Abb. -2 ausgeführter senkrechter Schnitt nach Linie 111-III der Abb. 2. Abb. ;. ist eine Einzeldarstellung des in (las Auslaßrohr eingebauten Rückschlagventils ini Schnitt.The drawing represents an embodiment of a ride of air cooling Ezplosionskraftniaschine equipped according to the I? invention in Fig. i in general view, in Abh.2 in vertical section. Fig.3 is a perpendicular to Fig. -2 vertical section along line III-III of Fig. 2. Fig.;. is a single representation of the non-return valve installed in the outlet pipe in section.

Das allseitig geschlossene Kurbelgehäuse i, dessen Innenraum sich unmittelbar an den Motorzylinder anschließt. ist mit (lein fnnenratun 3 der am Gehäuse i sitzenden Räderkapsel 2 durch eine Anzahl von Löchern d. in Verbindung. An die obere Wand der Räderkapsel 2 ist (las Rohr 5 angeschlossen. (las in Ausschnitte 6a der Kühlrippen 6 verlegt ist und an derjenigen Stelle zwischen den Ventilkannnern mündet, wo infolge der sehr hohen Temperatur leicht ein Glühendwerden der Z#,Ilin(lerwancl und der Kühlrippen 6 eintritt.The crankcase i, which is closed on all sides, the interior of which is connects directly to the engine cylinder. is with (line interior 3 that on the housing i seated wheel capsule 2 through a number of holes d. in connection. To the upper wall of the wheel capsule 2 is connected (read pipe 5. (read in cutouts 6a of the cooling fins 6 is laid and at that point between the valve cans opens where, due to the very high temperature, the Z #, Ilin (lerwancl and the cooling fins 6 enters.

In das Rohr 5 ist in der Nälie der an der Räderkapsel belegenen Eintrittsstelle zweckmäßig ein Kugelrückschlagventil mit geschlitztem Ventilsitz und durch Ouerstift lT-renztein Hub eingebaut.In the tube 5 is in the vicinity of the entry point located on the wheel capsule appropriately a ball check valve with a slotted valve seat and through Ouerstift Integrated lT-renztein hub.

D'e Wirkungsweise der vorstehend erläuterten Einrichtung gestaltet sich wie folgt: Die beim Aufwärtsgange des Kolbens ; .angesaugte Luftmenge wird beim Abwärts-"ange des Kolbens ini Kurbelgehäuse t komprimiert und durch die Löcher. (Abb.3) in ,len lnnen'rauin 3 der Räderkapsel 2 gepreßt. wo _ ie sich mit Öldämpfen sättigt und von hier aus durch las Ventil in das Rohr 5 übertritt. Der Austritt dieser mit Öldämpfen gesättigten komprimierten Luft aus der Rohrmündung erfolgt nun in den zwischen den Rippen C des Motorzylinders i und den Ventilkammern befindlichen Ausschnitt Üu gerade -in der Stelle, wo infolge der hohen Kompr essionsteniperaturen Zylinderwand und Rippen leicht glühend werden, so (laß diese Stellen wirksam gekühlt und ölfeucht gehalten «-erden.D'e mode of operation of the device explained above designed are as follows: The when the piston is moving upwards; . The amount of air sucked in is as the piston moves downward, it is compressed into the crankcase and through the holes. (Fig.3) pressed into the inner part 3 of the wheel capsule 2. where _ you deal with oil vapors saturates and from here passes through the valve into the pipe 5. The exit this compressed air, saturated with oil vapors, takes place from the pipe mouth now in the between the ribs C of the engine cylinder i and the valve chambers Excerpt from Üu just in the place where owing to the high levels of compression The cylinder wall and ribs become slightly glowing, so (let these areas be effectively cooled and kept oil-moist.

Claims (1)

PATENT-ANSPRUcH Kühlung für Explosionskraftniaschinen mittels der durch die Kolbenbewegun- ; gen angesaugten und durch das geschlossene Kurbelgehäuse gepreßten Luft, dadurch gekennzeichnet, daß diese Luftmenge, bevor sie in bekannter Weise dem heißesten Teile der durch Rippen gekühlten Zylinderwand zugeführt wird, durch das Ölbad der Räderkapsel für das Steuerungsvorgelege geleitet wird.PATENT CLAIM Cooling for explosion power machines by means of the by the piston movement; gen sucked in and through the closed crankcase compressed air, characterized in that this amount of air before it is known Way is fed to the hottest part of the rib-cooled cylinder wall, is passed through the oil bath of the gear capsule for the control gear.
DEG56354D Air cooling for explosion engines Expired DE377063C (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
DEG56354D DE377063C (en) Air cooling for explosion engines

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DEG56354D DE377063C (en) Air cooling for explosion engines

Publications (1)

Publication Number Publication Date
DE377063C true DE377063C (en) 1923-06-09

Family

ID=7131300

Family Applications (1)

Application Number Title Priority Date Filing Date
DEG56354D Expired DE377063C (en) Air cooling for explosion engines

Country Status (1)

Country Link
DE (1) DE377063C (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2532893A1 (en) * 1982-09-09 1984-03-16 Peugeot Cooling device of a timing gear casing on an internal combustion engine
FR2564898A1 (en) * 1984-05-24 1985-11-29 Daimler Benz Ag AERATION DEVICE FOR AN INTERNAL COMBUSTION ENGINE.

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2532893A1 (en) * 1982-09-09 1984-03-16 Peugeot Cooling device of a timing gear casing on an internal combustion engine
FR2564898A1 (en) * 1984-05-24 1985-11-29 Daimler Benz Ag AERATION DEVICE FOR AN INTERNAL COMBUSTION ENGINE.

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