AT27427B - Gas turbine. - Google Patents

Gas turbine.

Info

Publication number
AT27427B
AT27427B AT27427DA AT27427B AT 27427 B AT27427 B AT 27427B AT 27427D A AT27427D A AT 27427DA AT 27427 B AT27427 B AT 27427B
Authority
AT
Austria
Prior art keywords
gas turbine
chamber
gas mixture
impeller
explosion
Prior art date
Application number
Other languages
German (de)
Inventor
Peter Heinzl
Original Assignee
Peter Heinzl
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 Peter Heinzl filed Critical Peter Heinzl
Priority to AT27428D priority Critical patent/AT27428B/en
Application granted granted Critical
Publication of AT27427B publication Critical patent/AT27427B/en

Links

Landscapes

  • Turbine Rotor Nozzle Sealing (AREA)

Description

  

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

 <Desc/Clms Page number 2> 

 der Pfeilrichtung aus dem Vergaser 8 ansaugen. Dieses nun im Räume   6'und 12 an-   gesaugte Gasgemisch wird bei der Weiterbewegung des Laufrades 2 in die Kammer 12 komprimiert. In dem Momente, wo die Kammer 12 mit der im Gehäuse 1 vorgesehenen Kammer 9 korrespondiert, erfolgt die Zündung bezw. Explosion und das Laufrad wird nach vorwärts getrieben. Die explodierten Gase können durch den knapp hinter der Kammer 9 angeordneten Kanal 11 auspuffen.

   Während nun die verbrannten Gase nach vollbrachter Arbeit ins Freie gelangen, tritt der Schieber 14 der gegenüberliegenden   Kammer J3 in   den erweiterten Raum 6 und komprimiert die durch den vorherigen   Schieber J4   angesaugte Gasmischung, worauf der Vorgang sich wiederholt Die Regulierung der Maschine erfolgt durch Drosselung der   Gasgemischzufuhr.   



   PATENT-ANSPRÜCHE :   1.   Gasturbine, dadurch gekennzeichnet, dass das in einer im Laufrade   (2)   vorgesehenen Explosionskammer (12) komprimierte Gasgemisch unmittelbar vor dem Ausströmen zur Explosion gebracht wird, zu dem Zwecke, auf dem kurzen Wege zwischen Explosion und   Ausströmung   jeden Spannungsabfall infolge Undichtheiten zu verhindern und das Gasgemisch mit hohem Druck ausströmen zu lassen.



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

 <Desc / Clms Page number 2>

 in the direction of the arrow from the carburetor 8. This gas mixture, which is now drawn in in spaces 6 ′ and 12, is compressed into chamber 12 as the impeller 2 moves on. At the moment when the chamber 12 corresponds to the chamber 9 provided in the housing 1, the ignition takes place respectively. Explosion and the impeller is propelled forward. The exploded gases can exhaust through the channel 11 arranged just behind the chamber 9.

   While the burnt gases are released after the work is done, the slide 14 of the opposite chamber J3 enters the enlarged space 6 and compresses the gas mixture sucked in by the previous slide J4, whereupon the process is repeated.The machine is regulated by throttling the gas mixture supply .



   PATENT CLAIMS: 1. Gas turbine, characterized in that the gas mixture compressed in an explosion chamber (12) provided in the impeller (2) is made to explode immediately before the outflow, for the purpose of preventing any voltage drop on the short path between explosion and outflow to prevent leaks and to let the gas mixture flow out at high pressure.

Claims (1)

2. Auführuagsform der Turbine nach Anspruch 1, dadurch gekennzeichnet, dass die von den Explosionskammern angeordneten Schieber (13) durch Anschläge (17) oder dgl. verhindert werden, nicht mehr als zur Abdichtung notwendig aus dem Laufrade (2) auszutreten, zu dem Zwecke, ein Abschliessen der Yerdichtungskammer durch diese Schieber ( zu verhindern. EMI2.1 2. Auführuagsform the turbine according to claim 1, characterized in that the arranged by the explosion chambers slide (13) by stops (17) or the like. Are prevented from emerging from the impeller (2) no more than necessary for sealing, for the purpose to prevent the sealing chamber from being closed off by these slides. EMI2.1
AT27427D 1905-03-27 1905-03-27 Gas turbine. AT27427B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
AT27428D AT27428B (en) 1905-03-27 1905-08-30 Gas turbine.

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
AT27427T 1905-03-27

Publications (1)

Publication Number Publication Date
AT27427B true AT27427B (en) 1907-02-11

Family

ID=3539569

Family Applications (1)

Application Number Title Priority Date Filing Date
AT27427D AT27427B (en) 1905-03-27 1905-03-27 Gas turbine.

Country Status (1)

Country Link
AT (1) AT27427B (en)

Similar Documents

Publication Publication Date Title
DE2716470A1 (en) COMBUSTION ENGINE WITH AN EXHAUST GAS TURBOCHARGER
AT27427B (en) Gas turbine.
DE692383C (en) Safety device for the starting air line of internal combustion engines
DE2818278A1 (en) Continuous combustion rotary piston engine - has air compressed into external store vessel, preheater and continuous combustion chamber for expansion
DE2301865A1 (en) COMBUSTION MACHINE WITH EXTERNAL COMBUSTION
DE2200102B2 (en) Device for generating a working gas flow
DE970711C (en) Gas turbine system for generating hot compressed air
DE625694C (en) Back pressure combustion power turbine with combustion chambers in the impeller
DE500124C (en) Outlet valve housing on the combustion cylinder of a compressed gas generator
DE224908C (en)
DE673448C (en) Gas turbine system with constant pressure combustion
DE328142C (en) Gun lock
DE188354C (en)
AT78348B (en) Rotating internal combustion engine.
AT72610B (en) Protective ring for the cylinder wall in the combustion or pressure chambers of internal combustion engines.
DE2249545A1 (en) MACHINE GUN OF THE GAS PRESSURE CHARGING SYSTEM
AT62195B (en) Automotive torpedo powered by a gas turbine.
DE2021663C3 (en) Post-combustion system for the exhaust gases from piston internal combustion engines equipped with an exhaust gas turbocharger
AT18258B (en) Device for producing a mixture of gas and air for lighting systems by means of scoop devices.
AT278865B (en) Control device for combustion and steam turbine systems arranged on a shaft
AT146661B (en) Internal combustion engine.
AT8304B (en) Exhaust device for gas machines.
AT51593B (en) Device for extracting steam from the cylinders of direct current steam engines.
AT85422B (en) Two-stroke internal combustion engine.
DE179580C (en)