AT70757B - Gas turbine. - Google Patents
Gas turbine.Info
- Publication number
- AT70757B AT70757B AT70757DA AT70757B AT 70757 B AT70757 B AT 70757B AT 70757D A AT70757D A AT 70757DA AT 70757 B AT70757 B AT 70757B
- Authority
- AT
- Austria
- Prior art keywords
- gas turbine
- bottle
- compressed
- desc
- housing
- Prior art date
Links
- 238000002485 combustion reaction Methods 0.000 description 3
- 239000000446 fuel Substances 0.000 description 2
- 239000007789 gas Substances 0.000 description 2
- 239000002184 metal Substances 0.000 description 2
- 230000006835 compression Effects 0.000 description 1
- 238000007906 compression Methods 0.000 description 1
- 238000006073 displacement reaction Methods 0.000 description 1
- 239000000203 mixture Substances 0.000 description 1
Landscapes
- Supercharger (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Description
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Gasturbine.
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radgehäuse in Verbindung setzen. Dies ist jedesmal dann der Fall, wenn der Verdichterkolben vier Fünftel seines Weges zurückgelegt hat. Gleichzeitig mit der Verschiebung des Kolbens in der Verbrennungskammet wird die Stromleitung der Abreisszündvorrichtung 7 unterbrochen und hiedurch ein Funke erzeugt, der das verdichtete Gemisch zur Entzündung bringt.
Der Brennstoff wird den Verbrennungakammem mit Hilfe einer gleichfalls doppeltwirkenden Pumpe ? zugefahrt, die den betreffenden Brennstoff bei jedesmaligem Hub aus einem Behälter 23 in diejenige Verbrennungskammer fördert, der von dem Verdichtungszylinder 11 aus Luft zu-
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nach Bedarf regelt.
Die Abgase werden durch eine Auslassöffnung in der allgemein üblichen Weise aus dem Turbinengehäuse ausgelassen. Auf den Speichen des Laufrades sind Flügel oder Fächer 27 an-
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von Druckluft, angelassen, die unter 60 oder mehr Atmosphären Druck in eine Metallflasche 30 pmgppresst wird. Nach jedesmaligem Anlassen wird der Inhalt der Flasche auf diesen Normaldruck von 60 Atmosphären mit Hilfe des Verdichters 11 zurückgebracht, der mit der Flasche. 30 durch eine enge Rohrleitung 31 in Verbindung steht. Eine entsprechend weitere Rohrleitung 32 verbindet sodann die Matallflasche 30 mit dem Laufradgehäuse 2. Sowohl die Rohrleitung 31 als auch die Leitung 32 sind natürlich mit geeigneten Absperrventilen versehen. PATENT ANSPRÜCHE :
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<Desc / Clms Page number 1>
Gas turbine.
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<Desc / Clms Page number 2>
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connect wheel housing. This is the case every time the compressor piston has covered four fifths of its way. Simultaneously with the displacement of the piston in the combustion chamber, the current line of the detachable ignition device 7 is interrupted and a spark is thereby generated which ignites the compressed mixture.
The fuel is fed into the combustion chambers with the help of an equally double-acting pump? supplied, which conveys the relevant fuel with each stroke from a container 23 into the combustion chamber that is supplied from the compression cylinder 11 from air.
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regulates as required.
The exhaust gases are discharged from the turbine housing through an outlet opening in the generally customary manner. Wings or fans 27 are attached to the spokes of the wheel.
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of compressed air, cranked, which is compressed into a metal bottle of 30 pmg under 60 or more atmospheres pressure. After each start-up, the contents of the bottle are brought back to this normal pressure of 60 atmospheres with the aid of the compressor 11, which comes with the bottle. 30 through a narrow pipe 31 in connection. A correspondingly further pipeline 32 then connects the metal bottle 30 with the impeller housing 2. Both the pipeline 31 and the line 32 are of course provided with suitable shut-off valves. PATENT CLAIMS:
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Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| AT70757T | 1913-06-28 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| AT70757B true AT70757B (en) | 1915-12-27 |
Family
ID=3592490
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| AT70757D AT70757B (en) | 1913-06-28 | 1913-06-28 | Gas turbine. |
Country Status (1)
| Country | Link |
|---|---|
| AT (1) | AT70757B (en) |
-
1913
- 1913-06-28 AT AT70757D patent/AT70757B/en active
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