AT6984B - Cooling device for explosion engines. - Google Patents

Cooling device for explosion engines.

Info

Publication number
AT6984B
AT6984B AT6984DA AT6984B AT 6984 B AT6984 B AT 6984B AT 6984D A AT6984D A AT 6984DA AT 6984 B AT6984 B AT 6984B
Authority
AT
Austria
Prior art keywords
outside air
cooling device
tubes
explosion engines
water tank
Prior art date
Application number
Other languages
German (de)
Original Assignee
Nesselsdorfer Wagenabau Fabrik
Vorm K K Priv Wagenfabrik Schu
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 Nesselsdorfer Wagenabau Fabrik, Vorm K K Priv Wagenfabrik Schu filed Critical Nesselsdorfer Wagenabau Fabrik
Application granted granted Critical
Publication of AT6984B publication Critical patent/AT6984B/en

Links

Landscapes

  • Exhaust Silencers (AREA)

Description

  

   <Desc/Clms Page number 1> 
 



  Kühlvorrichtung für   Explo8ionskraftmaschinen.   



   Vorliegende Erfindung hat eine Kühlvorrichtung für   Explosionskraftmaschinen   zum Gegenstande, bei welcher gegenüber den bisherigen eine Gewichts-und Raumersparnis, sowie eine Vereinfachung der Ausführung dadurch erzielt wird, dass man, statt die Cylinder mit einem   Kühlmantel   zu versehen und die Kühlflüssigkeit durch diesen und einen besonderen Kühlwasserbehälter kreisen zu lassen, durch welch'letzteren mittelst eines Venti- 
 EMI1.1 
 Ventilators, sondern auch mittelst eines Strahlgebläses saugen lässt, welches von den unter   hohem   Druck entweichenden Auspuffgasen der Maschine betrieben wird. Überdies ist bei vorliegender Einrichtung noch Vorsorge getroffen, um die Kühlung zu regeln, so dass sie, unabhängig von der Temperatur der   Aussenluft,   stets eine eben ausreichende ist. 



   In der beiliegenden Zeichnung ist : Fig. 1 ein wagrechter, Fig. 2 ein lothrechter Schnitt einer Kühlvorrichtung nach vorliegender Erfindung. Die Maschine ist dabei als Zweicylindermaschineausgeführtgedacht. 
 EMI1.2 
 der Kammer   V   ab ; ebenso wird auch der Ventilator M in Thätigkeit kommen und saugt gleichfalls Luft aus der Kammer D, derart, dass   Aussenluft   durch die Röhren R strömt 
 EMI1.3 
 ringerem   Masse   unmittelbar in die Kammer D gelangen lassen und hierdurch den Luftdurchgang durch   die Röhren R und   damit auch die   Kühlung   entsprechend verringern. 

**WARNUNG** Ende DESC Feld kannt Anfang CLMS uberlappen**.



   <Desc / Clms Page number 1>
 



  Cooling device for explosion engines.



   The subject of the present invention is a cooling device for explosion engines, in which, compared to the previous ones, weight and space savings and a simplification of the design are achieved in that, instead of providing the cylinders with a cooling jacket, and the cooling liquid through this and a special cooling water tank through which the latter by means of a valve
 EMI1.1
 Fan, but also by means of a jet blower, which is operated by the exhaust gases of the machine escaping under high pressure. In addition, with the present device, provision is made to regulate the cooling so that it is always sufficient regardless of the temperature of the outside air.



   In the accompanying drawing: Fig. 1 is a horizontal, Fig. 2 is a perpendicular section of a cooling device according to the present invention. The machine is designed as a two-cylinder machine.
 EMI1.2
 the chamber V from; likewise the ventilator M will also come into operation and likewise suck air from the chamber D in such a way that outside air flows through the tubes R.
 EMI1.3
 Allow less mass to pass directly into chamber D and thereby reduce the passage of air through the tubes R and thus also the cooling accordingly.

** WARNING ** End of DESC field may overlap beginning of CLMS **.

 

Claims (1)

PATENT-ANSPRUCH : Ein von Röhren, die einerseits in die Aussenluft, und andererseits in eine mit Ventilator (M) versehene Kammer mündeu, durchsetzter Kühlwasserbehälter für Explosions- kraftmaschinon. dadurch gekennzeichnet, dass die mantellosen Cylinder unmittelbar in den Kühlwassorbohälter eingebaut sind und die genannte Kammer (D) mit der Luftdüse eines von den Auspuffgasen der Maschine betriebenen Strahlgebläses (C) in Verbindung steht und mit einer Klappe (A) ausgestattet ist, welch'letztere gegen die Aussenluft geöffnet werden kann, um die Menge der durch die Röhren (R) angesaugten Aussenluft zu regeln. **WARNUNG** Ende CLMS Feld Kannt Anfang DESC uberlappen**. PATENT CLAIM: A cooling water tank for an explosive power machine, penetrated by tubes, which on the one hand lead into the outside air and on the other hand into a chamber provided with a fan (M). characterized in that the jacketed cylinders are built directly into the cooling water tank and said chamber (D) is connected to the air nozzle of a jet blower (C) operated by the exhaust gases of the machine and is equipped with a flap (A), which is the latter can be opened to the outside air in order to regulate the amount of outside air sucked in through the tubes (R). ** WARNING ** End of CLMS field may overlap beginning of DESC **.
AT6984D 1900-01-29 1900-01-29 Cooling device for explosion engines. AT6984B (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
AT6984T 1900-01-29

Publications (1)

Publication Number Publication Date
AT6984B true AT6984B (en) 1902-03-10

Family

ID=3497446

Family Applications (1)

Application Number Title Priority Date Filing Date
AT6984D AT6984B (en) 1900-01-29 1900-01-29 Cooling device for explosion engines.

Country Status (1)

Country Link
AT (1) AT6984B (en)

Similar Documents

Publication Publication Date Title
AT6984B (en) Cooling device for explosion engines.
DE1551614A1 (en) Process and device for liquefying neon by means of an expansion turbine
AT48663B (en) Method for injecting the liquid fuel into the combustion chamber of constant pressure internal combustion engines, which is filled with compressed air.
AT16789B (en) Explosive engine with controlling piston.
AT18759B (en) Process and equipment to avoid gas losses in Siemens regenerative furnaces.
AT77097B (en) Procedure for the operation of gas turbines and the device for its implementation.
AT248012B (en) System for generating compressed air
AT25961B (en) Burner arrangement for motor vehicles with steam operation.
AT39572B (en) Injection capacitor.
AT37358B (en) Suction pipe for explosion engines.
AT71172B (en) Gas machine with a fan for sucking in and compressing the cargo.
US1135142A (en) Gasolene-motor respirator.
AT79978B (en) Piston cooling device for internal combustion enginesPiston cooling device for internal combustion engines. en.
DE551376C (en) Device for the pretreatment of operating materials for internal combustion engines
AT303245B (en) Jet pump for pumping hot gases
AT68743B (en) Four-stroke combustion engine with separate introduction of air and fuel into the spray chamber and utilization of the mixture in two stages.
AT45590B (en) Three-stage pressure pump.
AT94506B (en) Firing for pulverulent fuels.
AT22520B (en) Starting device for suction injectors.
US180853A (en) Improvement in draft-pipes for locomotives
AT45898B (en) Device for the systematic and economically advantageous absorption of a gas from a gas mixture.
AT86455B (en) Device for equalizing the draft in the smoke tubes of locomotive, locomobile and ship boilers.
DE394061C (en) Mechanical induced draft system for locomotives
AT31649B (en) Carburator for explosion engines.
DE424C (en) Steam boiler with steam formation outside the surfaces in contact with the fire