DE809614C - Back pressure internal combustion turbine with piston propellant gas generator - Google Patents

Back pressure internal combustion turbine with piston propellant gas generator

Info

Publication number
DE809614C
DE809614C DEN349A DEN0000349A DE809614C DE 809614 C DE809614 C DE 809614C DE N349 A DEN349 A DE N349A DE N0000349 A DEN0000349 A DE N0000349A DE 809614 C DE809614 C DE 809614C
Authority
DE
Germany
Prior art keywords
propellant gas
back pressure
gas generator
internal combustion
combustion turbine
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
DEN349A
Other languages
German (de)
Inventor
Emil Neuhaus
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.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Priority to DEN349A priority Critical patent/DE809614C/en
Application granted granted Critical
Publication of DE809614C publication Critical patent/DE809614C/en
Expired legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C5/00—Gas-turbine plants characterised by the working fluid being generated by intermittent combustion
    • F02C5/02—Gas-turbine plants characterised by the working fluid being generated by intermittent combustion characterised by the arrangement of the combustion chamber in the chamber in the plant
    • F02C5/04—Gas-turbine plants characterised by the working fluid being generated by intermittent combustion characterised by the arrangement of the combustion chamber in the chamber in the plant the combustion chambers being formed at least partly in the turbine rotor
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C5/00—Gas-turbine plants characterised by the working fluid being generated by intermittent combustion
    • F02C5/06—Gas-turbine plants characterised by the working fluid being generated by intermittent combustion the working fluid being generated in an internal-combustion gas generated of the positive-displacement type having essentially no mechanical power output

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Connection Of Motors, Electrical Generators, Mechanical Devices, And The Like (AREA)

Description

Die Erfindung bezieht sich auf eine Rückdruck-Brennkrafttürbine mit Kölbentreibgaserzeuger und ist in der Zeichnung dargestellt. Das Inbetriebsetzen der Maschine erfolgt durch Handantrieb oder durch entsprechende Apparate. Reine Luft oder Brennstoffgemisch tritt auf bekannte Weise in die Zylinder i, 2, 3 und 4. Die Zylinder sind um die mit Kurbel oder Exzenter versehene Antriebswelle 3 festgelagert. Auf der Antriebswelle 3 sitzt festgelagert der Turbinenläufer 4, in dessen äußerstem Rande ist der Rückdrucktreibgaskanal 5 vorgesehen. Der Treibgaskanal 5, dem Flachgewinde ähnelnd, ist mit entsprechender Steigung rings um das Rad ' zu führen. Die Länge des Treibgaskanals entspricht der Wirkungsdauer der sich entspannenden Gase. Die Zylinder sind mit der kreisrunden Gleitschiene 6 fest verbunden. Die Überströmkanäle 7 und 8 der Zylinder enden in der Gleitschiene. Die Gleitschiene ermöglicht das Abdichten der Überströmkanäle 7 und 8 der Zylinder wie auch das Verschließen des Treibgaskanals 5 im Läufer 4 nach erfolgter Explosion und Eintritt der hochgespannten Gase in den Treibgaskanal.The invention relates to a back pressure internal combustion engine with Piston propellant gas generator and is shown in the drawing. Commissioning the machine is carried out by hand drive or by appropriate apparatus. Pure Air or fuel mixture enters cylinders i, 2, 3 and in a known manner 4. The cylinders are fixedly mounted around the drive shaft 3, which is provided with a crank or eccentric. The turbine runner 4 sits firmly on the drive shaft 3, in its extreme position The back pressure propellant gas channel 5 is provided at the edge. The propellant gas channel 5, the flat thread similar, has to be guided around the wheel with a corresponding incline. The length of the propellant gas channel corresponds to the duration of the effect of the relaxing gases. the Cylinders are firmly connected to the circular slide rail 6. The overflow channels 7 and 8 of the cylinders end in the slide rail. The slide rail makes that possible Sealing the overflow channels 7 and 8 of the cylinder as well as closing the Propellant gas channel 5 in the rotor 4 after the explosion and entry of the high tension Gases in the propellant gas duct.

Die Maschine arbeitet folgendermaßen: Nach Abb. i der Zeichnung hat der Kolben des Treibgaserzeugers 9 das Brennstoffgemisch oder reine Luft hochkomprimiert. Die entzündeten Gase treten durch den Überströmkanal 7 in den Treibgaskanal 5 des Läufers 4, da im Augenblick der Zündung beide Kanäle gegenüberstehen. Infolge weiterer Drehung der Maschine sind sofort beide Kanäle getrennt und geschlossen durch das Gleiten des Läufers an der Gleitschiene, die während des Ausströmens das eine Ende des Treibgaskanals 5 verschließt. Die hochgespannten Gase im Treibgaskanal, erzeugen beim Entspannenund Ausströmen an den Schrägflächen des Treibgaskanals den Rückdruck, welcher den Läufer in Uhrzeigerrichtung antreibt. Die entspannten Gase treten durch den Auspuffkanal ir im fest stehenden Gleitsegment 12 ins Freie. Bei weiterer Umdrehung der Maschine komprimiert der Treibgaserzeugerkolben io das Brennstoffgemisch oder die Luft. Wenn der Treibgaskanal 5 den Zylinderkanal 8 erreicht hat, so wiederholt sich der Vorgang fortlaufend. Die Regelung der Maschine erfolgt durch mehr oder weniger Brennstoffzuführung.The machine works as follows: According to fig. I of the drawing has the piston of the propellant gas generator 9 highly compresses the fuel mixture or pure air. The ignited gases pass through the overflow channel 7 into the propellant gas channel 5 of the Runner 4, because at the moment of ignition, both channels are opposite. As a result of further Rotation of the machine, both channels are immediately separated and closed by the Sliding of the runner on the slide rail, which is one end during the outflow of the propellant gas channel 5 closes. Generate the high tension gases in the propellant gas duct the back pressure when releasing and flowing out on the inclined surfaces of the propellant gas channel, which drives the rotor clockwise. The relaxed gases come through the exhaust duct ir in the fixed sliding segment 12 into the open. With further rotation the engine compresses the propellant gas generator piston io the fuel mixture or the air. When the propellant gas channel 5 has reached the cylinder channel 8, it is repeated the process is ongoing. The machine is controlled by more or less fuel supply.

Der wesentlichste Vorteil der Maschine ist - ihre Brennstoffverwendungsmöglichkeit. Außer mit allen bisher bekannten Brennstoffen arbeitet die Maschine auch mit nur hochkomprimierter reiner Luft.The main advantage of the machine is - its ability to use fuel. In addition to all previously known fuels, the machine also works with only highly compressed pure air.

Claims (1)

PATENTANSPRUCH: Rückdruck-Brennkraftturbine mit Kolbentreibgaserzeuger, gekennzeichnet durch die Kombination folgender Merkmale: a) Die Zylinder des Treibgaserzeugers sind um die mit Exzenter oder Kurbel versehene Turbinenwelle feststehend angeordnet und die Kolben über Schubstangen an Exzenter oder Kurbel angelenkt, b) die Zylinderköpfe liegen auf der einen Seite einer kreisrunden, feststehenden Gleitschiene, welche im Bereich der im Zylinder- . kopf angeordneten Treibgasauslaßkanäle durchbrochen ist. c) Der Turbinenläufer liegt an der anderen Gleitschienenseite an und ist mit spiraligen, einem Flachgewinde ähnlichen Rückdruck-Treibgaskanälen versehen. PATENT CLAIM: Back pressure internal combustion turbine with piston propellant gas generator, characterized by the combination of the following features: a) The cylinders of the propellant gas generator are fixed around the turbine shaft equipped with an eccentric or crank and the pistons are linked to the eccentric or crank via push rods, b) the cylinder heads rest on the one side of a circular, fixed slide rail, which in the area of the cylinder. head arranged propellant gas outlet channels is broken. c) The turbine runner rests on the other side of the slide rail and is provided with spiral back pressure propellant gas channels similar to a flat thread.
DEN349A 1950-01-03 1950-01-03 Back pressure internal combustion turbine with piston propellant gas generator Expired DE809614C (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
DEN349A DE809614C (en) 1950-01-03 1950-01-03 Back pressure internal combustion turbine with piston propellant gas generator

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DEN349A DE809614C (en) 1950-01-03 1950-01-03 Back pressure internal combustion turbine with piston propellant gas generator

Publications (1)

Publication Number Publication Date
DE809614C true DE809614C (en) 1951-07-30

Family

ID=7337401

Family Applications (1)

Application Number Title Priority Date Filing Date
DEN349A Expired DE809614C (en) 1950-01-03 1950-01-03 Back pressure internal combustion turbine with piston propellant gas generator

Country Status (1)

Country Link
DE (1) DE809614C (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE888334C (en) * 1951-11-28 1953-08-31 Jakob Wagner Rotary vane-controlled back pressure internal combustion turbine with compression cylinders arranged in the impeller

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE888334C (en) * 1951-11-28 1953-08-31 Jakob Wagner Rotary vane-controlled back pressure internal combustion turbine with compression cylinders arranged in the impeller

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