AT63176B - Centrifugal compressor. - Google Patents
Centrifugal compressor.Info
- Publication number
- AT63176B AT63176B AT63176DA AT63176B AT 63176 B AT63176 B AT 63176B AT 63176D A AT63176D A AT 63176DA AT 63176 B AT63176 B AT 63176B
- Authority
- AT
- Austria
- Prior art keywords
- centrifugal compressor
- blades
- inner ends
- closer
- paddle wheel
- Prior art date
Links
- 239000007789 gas Substances 0.000 description 1
Landscapes
- Structures Of Non-Positive Displacement Pumps (AREA)
Description
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zwischen den Winkeln des ersten und letzten Schaufelrades sein oder es kann auch bei dem einen oder anderen Schaufelrad dieselbe Schaufelform wie in dem früheren Schaufelrad verwendet werden.
Eine weitere Eigentümlichkeit des Schleuderverdichters nach der Erfindung besteht darin, dass die inneren Enden der folgenden Schaufeln näher an die Wellenachse heranrücken als die inneren Enden der vorhergehenden Schaufeln. Es stehen also die inneren Enden der Schaufeln 11 der Wellenachse näher als die inneren Enden der Schaufeln 10 und ebenso liegen die inneren Enden der Schaufeln 12 und 13 näher an der Wellenmitte. Die Verkleinerung des Verhältnisses der radialen Entfernung der inneren Enden der Schaufeln von der Wellenmitte zu den Halbmessern der aufeinanderfolgenden Schaufelräder hat die Wirkung, dass die Luft weniger leicht
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stützt wird.
PATENT-ANSPRÜCHE :
1. Schleuderverdichter für Luft oder Gase mit mehreren Schaufelrädern, durch die das zu verdichtende Mittel nacheinander hindurchgeht, dadurch gekennzeichnet, dass der Austrittswinkel der Schaufeln in einem oder mehreren der Schaufelräder grösser ist als m einem vorhergehenden Schaufelrad.
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be between the angles of the first and last paddle wheel, or the same paddle shape as in the earlier paddle wheel can also be used for one or the other paddle wheel.
Another peculiarity of the centrifugal compressor according to the invention is that the inner ends of the following blades move closer to the shaft axis than the inner ends of the preceding blades. The inner ends of the blades 11 are therefore closer to the shaft axis than the inner ends of the blades 10, and the inner ends of the blades 12 and 13 are also closer to the center of the shaft. The reduction in the ratio of the radial distance of the inner ends of the blades from the shaft center to the radii of the successive blades has the effect of making the air less light
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is supported.
PATENT CLAIMS:
1. Centrifugal compressor for air or gases with several impellers through which the agent to be compressed passes one after the other, characterized in that the exit angle of the blades in one or more of the impellers is greater than a preceding impeller.
Claims (1)
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| AT63176T | 1913-01-02 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| AT63176B true AT63176B (en) | 1914-01-26 |
Family
ID=3585080
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| AT63176D AT63176B (en) | 1913-01-02 | 1913-01-02 | Centrifugal compressor. |
Country Status (1)
| Country | Link |
|---|---|
| AT (1) | AT63176B (en) |
-
1913
- 1913-01-02 AT AT63176D patent/AT63176B/en active
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