RU2008129501A - METHOD FOR WORKING A GAS TURBINE ENGINE - Google Patents
METHOD FOR WORKING A GAS TURBINE ENGINE Download PDFInfo
- Publication number
- RU2008129501A RU2008129501A RU2008129501/06A RU2008129501A RU2008129501A RU 2008129501 A RU2008129501 A RU 2008129501A RU 2008129501/06 A RU2008129501/06 A RU 2008129501/06A RU 2008129501 A RU2008129501 A RU 2008129501A RU 2008129501 A RU2008129501 A RU 2008129501A
- Authority
- RU
- Russia
- Prior art keywords
- heat exchanger
- pumped
- liquefied
- compressor
- heated
- Prior art date
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- Filling Or Discharging Of Gas Storage Vessels (AREA)
Abstract
Способ работы газотурбинного двигателя, использующего запасаемый в баке жидкий хладоагент, по которому атмосферный воздух контура питания газогенератора принимают в заборник, предварительно сжимают в компрессоре, нагнетают до высокого давления, используют в газогенераторе для сжигания горючего, а продукты сгорания используют на турбине и подают в реактивное сопло, ! отличающийся тем, что жидкий хладоагент используют в контуре циркуляции, где его нагнетают насосом, нагревают в первом теплообменнике, сжижают во втором теплообменнике, а атмосферный воздух после компрессора, сжижают в первом теплообменнике, нагнетают насосом, испаряют и нагревают во втором теплообменнике, а в качестве хладоагента используют воздух или более низкокипящие газы.The method of operation of a gas turbine engine using a liquid refrigerant stored in a tank, according to which the atmospheric air of the gas generator supply circuit is taken into the intake, pre-compressed in a compressor, pumped to high pressure, used in a gas generator to burn fuel, and combustion products are used on a turbine and fed to a jet nozzle! characterized in that the liquid refrigerant is used in the circulation circuit, where it is pumped, heated in the first heat exchanger, liquefied in the second heat exchanger, and atmospheric air after the compressor, liquefied in the first heat exchanger, pumped, evaporated and heated in the second heat exchanger, and as the refrigerant uses air or lower boiling gases.
Claims (1)
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| RU2008129501/06A RU2008129501A (en) | 2008-07-21 | 2008-07-21 | METHOD FOR WORKING A GAS TURBINE ENGINE |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| RU2008129501/06A RU2008129501A (en) | 2008-07-21 | 2008-07-21 | METHOD FOR WORKING A GAS TURBINE ENGINE |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| RU2008129501A true RU2008129501A (en) | 2010-01-27 |
Family
ID=42121523
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| RU2008129501/06A RU2008129501A (en) | 2008-07-21 | 2008-07-21 | METHOD FOR WORKING A GAS TURBINE ENGINE |
Country Status (1)
| Country | Link |
|---|---|
| RU (1) | RU2008129501A (en) |
-
2008
- 2008-07-21 RU RU2008129501/06A patent/RU2008129501A/en not_active Application Discontinuation
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| FA92 | Acknowledgement of application withdrawn (lack of supplementary materials submitted) |
Effective date: 20100112 |