JPS6477723A - Gas turbine - Google Patents
Gas turbineInfo
- Publication number
- JPS6477723A JPS6477723A JP23254687A JP23254687A JPS6477723A JP S6477723 A JPS6477723 A JP S6477723A JP 23254687 A JP23254687 A JP 23254687A JP 23254687 A JP23254687 A JP 23254687A JP S6477723 A JPS6477723 A JP S6477723A
- Authority
- JP
- Japan
- Prior art keywords
- turbine
- combustor
- compressor
- driven
- gas
- 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 attempt the improvement of reliability and the like by completely separating a high temperature section from a low temperature section in such a way as to drive a compressor driven turbine by gas dropped in both temperature and pressure after an output turbine has been driven by gas kept high in both temperature and pressure exhausted from a combustor. CONSTITUTION:A two shaft type high temperature gas turbine is composed of a compressor 1, an intake air duct 2, an exhaust air duct 3, a heat exchanger 4, an intermediate duct 5, a combustor 6, a combustor outer cylinder 7, a compressor driven turbine 8, an output turbine 9 and the like. In this constitution, the output turbine 9 is arranged beneath the combustor 6, and the compressor driven turbine 8 is arranged in the downstream of the output turbine 9 concurrently. Then, the compressor driven turbine 8 is driven by gas dropped in both temperature and pressure after the output turbine 9 has been driven by gas kept high in both temperature and pressure exhausted from the combustor 6. Owing to this constitution, the combustor 6 and the output turbine 9 forming a high temperature section is completely separated from both the compressor 1 and the compressor driven turbine 8 forming a low temperature section.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP23254687A JPS6477723A (en) | 1987-09-18 | 1987-09-18 | Gas turbine |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP23254687A JPS6477723A (en) | 1987-09-18 | 1987-09-18 | Gas turbine |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| JPS6477723A true JPS6477723A (en) | 1989-03-23 |
Family
ID=16941016
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP23254687A Pending JPS6477723A (en) | 1987-09-18 | 1987-09-18 | Gas turbine |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPS6477723A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2010075393A2 (en) * | 2008-12-23 | 2010-07-01 | Solar Turbines Incorporated | Gas turbine engine and system for servicing a gas turbine engine |
| US8590151B2 (en) | 2006-06-30 | 2013-11-26 | Solar Turbines Inc. | System for supporting and servicing a gas turbine engine |
-
1987
- 1987-09-18 JP JP23254687A patent/JPS6477723A/en active Pending
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US8590151B2 (en) | 2006-06-30 | 2013-11-26 | Solar Turbines Inc. | System for supporting and servicing a gas turbine engine |
| US8672606B2 (en) | 2006-06-30 | 2014-03-18 | Solar Turbines Inc. | Gas turbine engine and system for servicing a gas turbine engine |
| WO2010075393A2 (en) * | 2008-12-23 | 2010-07-01 | Solar Turbines Incorporated | Gas turbine engine and system for servicing a gas turbine engine |
| WO2010075393A3 (en) * | 2008-12-23 | 2010-10-14 | Solar Turbines Incorporated | Gas turbine engine and system for servicing a gas turbine engine |
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