RU2012145927A - GAS TURBINE UNIT WITH HEAT PUMP - Google Patents
GAS TURBINE UNIT WITH HEAT PUMP Download PDFInfo
- Publication number
- RU2012145927A RU2012145927A RU2012145927/06A RU2012145927A RU2012145927A RU 2012145927 A RU2012145927 A RU 2012145927A RU 2012145927/06 A RU2012145927/06 A RU 2012145927/06A RU 2012145927 A RU2012145927 A RU 2012145927A RU 2012145927 A RU2012145927 A RU 2012145927A
- Authority
- RU
- Russia
- Prior art keywords
- heat exchanger
- gas turbine
- turbine engine
- fuel
- evaporative
- Prior art date
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- Output Control And Ontrol Of Special Type Engine (AREA)
- Engine Equipment That Uses Special Cycles (AREA)
Abstract
Газотурбинная установка, содержащая газотурбинный двигатель с компрессором, устройство воздухоподготовки газотурбинного двигателя, топливную систему с камерами сгорания, устройством подачи и регулирования топлива, масляную систему узлов трения газотурбинного двигателя и исполнительных агрегатов с теплообменником охлаждения масла, нагнетающим насосом, теплообменником подогрева топлива, выполненными в отдельном регулируемом циркуляционном контуре, отличающаяся тем, что она дополнительно снабжена тепловым насосом, содержащим последовательно соединенные, по меньшей мере, один испарительный теплообменник, одно устройство повышения давления, один конденсаторный теплообменник, одно устройство понижения давления, при этом вход испарительного теплообменника подключен к выходу устройства воздухоподготовки газотурбинного двигателя, выход испарительного теплообменника соединен с входом компрессора, вход конденсаторного теплообменника соединен с устройством подачи топлива, а выход - с теплообменником подогрева топлива.A gas turbine installation comprising a gas turbine engine with a compressor, an air preparation device for a gas turbine engine, a fuel system with combustion chambers, a fuel supply and regulation device, an oil system of friction units of a gas turbine engine and actuating units with an oil cooling heat exchanger, a discharge pump, and a fuel heating heat exchanger made in a separate adjustable circulation circuit, characterized in that it is additionally equipped with a heat pump containing the last at least one evaporative heat exchanger, one pressure boosting device, one condenser heat exchanger, one pressure reducing device are connected together, while the input of the evaporative heat exchanger is connected to the output of the air treatment device of the gas turbine engine, the output of the evaporative heat exchanger is connected to the compressor inlet, the input of the condenser heat exchanger is connected with a fuel supply device, and the outlet with a fuel heat exchanger.
Claims (1)
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| RU2012145927/06A RU2515910C1 (en) | 2012-10-29 | 2012-10-29 | Gas turbine plant with heat pump |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| RU2012145927/06A RU2515910C1 (en) | 2012-10-29 | 2012-10-29 | Gas turbine plant with heat pump |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| RU2012145927A true RU2012145927A (en) | 2014-05-10 |
| RU2515910C1 RU2515910C1 (en) | 2014-05-20 |
Family
ID=50629208
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| RU2012145927/06A RU2515910C1 (en) | 2012-10-29 | 2012-10-29 | Gas turbine plant with heat pump |
Country Status (1)
| Country | Link |
|---|---|
| RU (1) | RU2515910C1 (en) |
Families Citing this family (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2021062185A1 (en) * | 2019-09-27 | 2021-04-01 | Nooter/Eriksen, Inc. | Refrigeration system for a gas turbine |
Family Cites Families (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR2216175B1 (en) * | 1973-02-05 | 1975-03-07 | Snecma | |
| US4041697A (en) * | 1975-07-17 | 1977-08-16 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Oil cooling system for a gas turbine engine |
| US4104873A (en) * | 1976-11-29 | 1978-08-08 | The United States Of America As Represented By The Administrator Of The United States National Aeronautics And Space Administration | Fuel delivery system including heat exchanger means |
| US4354345A (en) * | 1980-04-29 | 1982-10-19 | United Technologies Corporation | Fuel heating system for gas turbine engine |
| SU1495415A1 (en) * | 1987-11-18 | 1989-07-23 | В.П.Короткое | Steam-gas turbine unit |
| RU2353787C1 (en) * | 2007-09-06 | 2009-04-27 | Открытое акционерное общество "Российские железные дороги" (ОАО "РЖД") | Gas-turbine plant |
-
2012
- 2012-10-29 RU RU2012145927/06A patent/RU2515910C1/en not_active IP Right Cessation
Also Published As
| Publication number | Publication date |
|---|---|
| RU2515910C1 (en) | 2014-05-20 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| MM4A | The patent is invalid due to non-payment of fees |
Effective date: 20181030 |