AT61197B - Explosion or internal combustion engine combined with a compressed air machine. - Google Patents

Explosion or internal combustion engine combined with a compressed air machine.

Info

Publication number
AT61197B
AT61197B AT61197DA AT61197B AT 61197 B AT61197 B AT 61197B AT 61197D A AT61197D A AT 61197DA AT 61197 B AT61197 B AT 61197B
Authority
AT
Austria
Prior art keywords
explosion
compressed air
internal combustion
combustion engine
air machine
Prior art date
Application number
Other languages
German (de)
Inventor
Paul Nolet
Original Assignee
Paul Nolet
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 Paul Nolet filed Critical Paul Nolet
Application granted granted Critical
Publication of AT61197B publication Critical patent/AT61197B/en

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B41/00Engines characterised by special means for improving conversion of heat or pressure energy into mechanical power
    • F02B41/02Engines with prolonged expansion
    • F02B41/06Engines with prolonged expansion in compound cylinders
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B1/00Engines characterised by fuel-air mixture compression
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B2700/00Measures relating to the combustion process without indication of the kind of fuel or with more than one fuel
    • F02B2700/02Four stroke engines
    • F02B2700/026Four stroke engines with measures for increasing the part of the heat transferred to power, compound engines

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Compressors, Vaccum Pumps And Other Relevant Systems (AREA)

Description

  

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  Mit einer   Druckluftma8chlne   vereinigte Explosions- oder Verbrennungskraftmaschine. 
 EMI1.1 
 dieser letzteren und bevor sie den Kolben bewegt, eine Arbeit geleistet wird, die den Druck und damit die   Anfangstemperatur im Motor herabmindert   ; die derart aufgewendete Energiemenge wird wieder   rückgellommen   und zur Betätigung des Kolbens verwendet, wozu man ausserdem auch den Druck der Auspuffgase mitwirken lassen kann. 



   Zu diesem Zweck ist die Explosions-oder Verbrennungskraftmaschine mit einer Druckluftkraftmaschine kopbiniert, und zwar derart, dass ihre zugehörigen Kompressionskammern durch eine bewegliche Wand voneinander getrennt sind und dass ihre miteinander festverbundenen Kolben gleichzeitig den Kompressionshub ausführen.

   Im Zeitpunkte der Explosion oder Ver-   brennung   wirkt diese auf die   bewegliche Scheidewand, verschiebt aie in das Innere der   Luft-   kammer   und verringert so deren Rauminhalt und erhöht den   Druck der   darin   befindlichen Luft.   Sobald sich die zwei miteinander verbundenen Kolben in Bewegung setzen, beginnt gleichzeitig die Expansion in beiden Zylindern und infolge der   bekannten   Eigenschaften der verdichteten Luft wird die während ihrer Weiterverdichtung aufgenommene Arbeit zur   Ganze vom Druck-     luftmotor     zurückergebcn,   in dem die Expansion bis zum Atmosphärendruck stattfindet.

   Die 
 EMI1.2 
 kann jedoch dadurch   behoben werden, dass   die   Auspuffgase in   eine unter dem Kolben des   Druckluftmotors gelegene Kammer   geleitet werden, damit sie auf die untere Kolbenflche   w ahrend des folgenden Hubes des Kolbens   einwirken ; man erreicht dadurch die Kompoundierung der Maschine. 



   In der Zeichnung ist eine Ausführungsform einer solchen Maschine in Fig. 1 und 2 im 
 EMI1.3 
    ieWirkungswelse des Motors   ist folgende : Zu Beginn der   Ansaugperiode   nehmen die Kolben 2 und 4 die in Fig. 1 angegebene Lage ein, die bewegliche Scheidewand 7 ruht   indessen   auf dem Anschlag 15. Während der Kompressionsperiode wird das Gasgemisch in der Kammer 6 unterhalb der Scheidewand 7, die Luft in der Kammer 5 oberhalb dieser Scheidewand verdichtet. 



    Die Abmessungen dieser Kammern müssen derart sein, dass die Luftverdichtung genügend gross   ist. um die    cheidewand 7 an   ihrem Platze zu belassen. 



   Wenn die Zündung des Gasgemisches erfolgt, wirkt die durch Explosion oder Verbrennung   entwickelte Kraft augenblicklich auf die bewegliche Scheidewand   ein, und zwar w hrend des   Ansteigens des hiebei entstehenden Druckes   und bevor dieser den Kolben 2, dessen Kurbel sich 
 EMI1.4 
 

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  Explosion or internal combustion engine combined with a compressed air machine.
 EMI1.1
 this latter and before it moves the piston, a work is done that reduces the pressure and thus the initial temperature in the engine; the amount of energy expended in this way is taken back and used to actuate the piston, for which purpose the pressure of the exhaust gases can also contribute.



   For this purpose, the explosion or internal combustion engine is combined with a compressed air engine, specifically in such a way that its associated compression chambers are separated from one another by a movable wall and that their pistons, which are firmly connected to one another, simultaneously execute the compression stroke.

   At the time of the explosion or combustion, this acts on the movable partition, pushes it into the interior of the air chamber and thus reduces its volume and increases the pressure of the air inside. As soon as the two connected pistons start to move, the expansion in both cylinders begins at the same time and, due to the known properties of the compressed air, the work absorbed during its further compression is completely returned by the compressed air motor, in which the expansion takes place up to atmospheric pressure.

   The
 EMI1.2
 However, this can be remedied by directing the exhaust gases into a chamber located under the piston of the air motor so that they act on the lower piston surface during the following stroke of the piston; this achieves the compounding of the machine.



   In the drawing, an embodiment of such a machine in Figs. 1 and 2 is in
 EMI1.3
    The engine works as follows: At the beginning of the intake period, the pistons 2 and 4 assume the position indicated in FIG. 1, while the movable partition 7 rests on the stop 15. During the compression period, the gas mixture in the chamber 6 is below the partition 7 , the air in the chamber 5 above this partition is compressed.



    The dimensions of these chambers must be such that the air compression is sufficiently large. to leave the partition 7 in place.



   When the gas mixture is ignited, the force developed by the explosion or combustion acts instantly on the movable septum, while the pressure that occurs is increasing and before the piston 2, its crank, moves
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AT61197D 1911-09-23 1912-08-21 Explosion or internal combustion engine combined with a compressed air machine. AT61197B (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
BE239060 1911-09-23

Publications (1)

Publication Number Publication Date
AT61197B true AT61197B (en) 1913-09-10

Family

ID=32330645

Family Applications (1)

Application Number Title Priority Date Filing Date
AT61197D AT61197B (en) 1911-09-23 1912-08-21 Explosion or internal combustion engine combined with a compressed air machine.

Country Status (4)

Country Link
AT (1) AT61197B (en)
AU (1) AU652812B (en)
GB (1) GB191204987A (en)
NL (1) NL159C (en)

Also Published As

Publication number Publication date
GB191204987A (en) 1912-09-26
NL159C (en) 1914-03-16
AU652812B (en) 1913-05-20

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