JPS5669422A - Gas turbine engine - Google Patents
Gas turbine engineInfo
- Publication number
- JPS5669422A JPS5669422A JP14579179A JP14579179A JPS5669422A JP S5669422 A JPS5669422 A JP S5669422A JP 14579179 A JP14579179 A JP 14579179A JP 14579179 A JP14579179 A JP 14579179A JP S5669422 A JPS5669422 A JP S5669422A
- Authority
- JP
- Japan
- Prior art keywords
- impeller
- air
- fuel
- gas turbine
- nozzle
- 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.)
- Pending
Links
Abstract
PURPOSE: To improve thermal efficiency, by providing a fuel combustor at a part of a rotary member.
CONSTITUTION: A gas turbine comprises an impeller A, a main pipe for supplying fuel and a casing. When the impeller A is rotated by an appropriate method, air is sucked from a port near the center of a passage 7 and accelerated by the impeller 4 of a centrifugal compressor because the impeller A has the same construction as the impeller 4. The air is supplied from a compression section 8 to a combustion chamber 9 while the air is compressed by centrifugal force. The air is then ejected from a nozzle 10 in a circumferential direction opposite to the direction of the rotation. The fuel is burned in the combustion chamber 9 to heat the compressed air to eject it from the nozzle 10 at a speed higher than the circumferential velocity of the impeller A. The impeller A is caused to start self-rotation by the reaction of the ejected air.
COPYRIGHT: (C)1981,JPO&Japio
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP14579179A JPS5669422A (en) | 1979-11-11 | 1979-11-11 | Gas turbine engine |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP14579179A JPS5669422A (en) | 1979-11-11 | 1979-11-11 | Gas turbine engine |
Publications (1)
Publication Number | Publication Date |
---|---|
JPS5669422A true JPS5669422A (en) | 1981-06-10 |
Family
ID=15393235
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP14579179A Pending JPS5669422A (en) | 1979-11-11 | 1979-11-11 | Gas turbine engine |
Country Status (1)
Country | Link |
---|---|
JP (1) | JPS5669422A (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS6223537A (en) * | 1985-05-08 | 1987-01-31 | ホセ、ロレンソ、ロペス、サンチエス | Rotary engine |
JP2010133273A (en) * | 2008-12-02 | 2010-06-17 | Shuzo Onodera | Rotary exhaust-type engine for air plane body |
-
1979
- 1979-11-11 JP JP14579179A patent/JPS5669422A/en active Pending
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS6223537A (en) * | 1985-05-08 | 1987-01-31 | ホセ、ロレンソ、ロペス、サンチエス | Rotary engine |
JP2010133273A (en) * | 2008-12-02 | 2010-06-17 | Shuzo Onodera | Rotary exhaust-type engine for air plane body |
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