AT25400B - Working methods for explosion engines. - Google Patents

Working methods for explosion engines.

Info

Publication number
AT25400B
AT25400B AT25400DA AT25400B AT 25400 B AT25400 B AT 25400B AT 25400D A AT25400D A AT 25400DA AT 25400 B AT25400 B AT 25400B
Authority
AT
Austria
Prior art keywords
compression
compressed
air
explosion engines
approximately
Prior art date
Application number
Other languages
German (de)
Inventor
Richard Becker
Adolf Reisser
Original Assignee
Richard Becker
Adolf Reisser
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 Richard Becker, Adolf Reisser filed Critical Richard Becker
Application granted granted Critical
Publication of AT25400B publication Critical patent/AT25400B/en

Links

Description

  

   <Desc/Clms Page number 1> 
 
 EMI1.1 
 
 EMI1.2 
 

 <Desc/Clms Page number 2> 

 
 EMI2.1 
 gleiche Spannung wie die Luft verdichtete Gas durchströmt den obenfalls gekühlten Zwischen-   bohalter (7. Kurz   nach dem Endo des Auspuffhubos im Arbeitszylinder öffnet sich das 
 EMI2.2 
 Ventile geschlossen werden, worauf das eingeschlossene Gemisch während des übrigen Kolbenweges expandiert, um dann beim Rückhub wieder verdichtet und   schliesslich am   Hubende entzündet zu werden, worauf dann die Expansion und der Auspuff wie bei einem 
 EMI2.3 
 Gemisches bei 60% des Kolbenweges ermöglicht, den Verdichtungsraum im Verhältnis zum Hubvolumen möglichst klein und hiemit die Expansion   möglichst   gross zu erhalten, so dass die Expansionsendspannung trotz des hohen,

   Explosionsdruckes von ungefähr 40   Atm.   abs. und mehr nicht wesentlich höher ist als bei den gewöhnlichen Motoren. Selbstverständlich kann der Arbeitskolben beim Rückgange statt reiner Luft auch Luft und Gas gemischt ansaugen, wobei dann die besondere Gaspumpe und der dazugehörige zweite Kühler entfalten können. 



   Die beschriebene Ausführungsform ist nur beispielsweise gewählt. Es können Gas und Luft statt gesondert auch gemischt verdichtet und gekühlt werden, und die Zahl der Stufen, in denen die Vordichtung erfolgt, beliebig gewählt werden. Wesentlich ist, dass nach jeder Verdichtung eine Abkühlung bis ungefähr auf die   äussere   Lufttemperatur erfolgt. 



   Ebenso ist es für das Wesen der vorliegenden Erfindung gleichgiltig, ob zur Vorverdichtung besondere Pumpen vorgesehen sind, oder ob die Verdichtung in den nicht arbeitverrichtendon Seiten der Zylinder erfolgt.



   <Desc / Clms Page number 1>
 
 EMI1.1
 
 EMI1.2
 

 <Desc / Clms Page number 2>

 
 EMI2.1
 The same tension as the air, compressed gas, flows through the intermediate bohalter, which is cooled at the top (7. Shortly after the end of the exhaust stroke in the working cylinder, this opens
 EMI2.2
 Valves are closed, whereupon the trapped mixture expands during the rest of the piston travel, to be compressed again on the return stroke and finally ignited at the end of the stroke, whereupon the expansion and the exhaust as with one
 EMI2.3
 Mixture at 60% of the piston travel makes it possible to keep the compression space as small as possible in relation to the stroke volume and thus to keep the expansion as large as possible, so that the expansion stress despite the high,

   Explosion pressure of about 40 atm. Section. and more is not significantly higher than that of ordinary engines. It goes without saying that the working piston can also suck in mixed air and gas instead of pure air when decelerating, in which case the special gas pump and the associated second cooler can deploy.



   The embodiment described is only chosen as an example. Gas and air can be compressed and cooled mixed instead of separately, and the number of stages in which the pre-sealing takes place can be selected as desired. It is essential that after each compression there is a cooling down to approximately the external air temperature.



   It is also irrelevant to the essence of the present invention whether special pumps are provided for pre-compression or whether compression takes place in the non-working sides of the cylinders.

 

Claims (1)

PATENT-ANSPRUCH : Arbeitsverfahren für Explosionskraftmaschinen, dadurch gekennzeichnet, dass die Bestandteile des aus gasförmigem Brennstoff und Luft bestehenden Betriebsmittels oder deren Gemisch in besonderen Pumpenräumen in einer oder mehreren Stufen verdichtet und nach jeder Verdichtung bis ungefähr auf die Temperatur der Aussenluft abgekühlt werden, worauf das verdichtete und abgekühlte Gasluftgemisch oder seine Bestandteile in den Arbeitszylinder eingeführt, in demselben weiter verdichtet und ungefähr am Hubende des Kolbens entzündet wird, so dass die im Arbeitszylinder erreichte Verdichtungsendspanuung ungefähr proportional der vorhergegangenen Vorverdicbtung höher, die Verdichtungsend- EMI2.4 PATENT CLAIM: Working method for explosion engines, characterized in that the components of the equipment consisting of gaseous fuel and air or their mixture are compressed in special pump rooms in one or more stages and after each compression are cooled down to approximately the temperature of the outside air, whereupon the compressed and cooled gas-air mixture or its components are introduced into the working cylinder, further compressed in the same and ignited approximately at the end of the stroke of the piston, so that the compression end stress reached in the working cylinder is approximately proportional to the previous pre-compression higher, the compression end EMI2.4
AT25400D 1901-04-28 1901-04-28 Working methods for explosion engines. AT25400B (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
AT25400T 1901-04-28

Publications (1)

Publication Number Publication Date
AT25400B true AT25400B (en) 1906-08-25

Family

ID=3536086

Family Applications (1)

Application Number Title Priority Date Filing Date
AT25400D AT25400B (en) 1901-04-28 1901-04-28 Working methods for explosion engines.

Country Status (1)

Country Link
AT (1) AT25400B (en)

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