RU2008141793A - ATOMIC GAS-TURBINE ENGINE - Google Patents
ATOMIC GAS-TURBINE ENGINE Download PDFInfo
- Publication number
- RU2008141793A RU2008141793A RU2008141793/06A RU2008141793A RU2008141793A RU 2008141793 A RU2008141793 A RU 2008141793A RU 2008141793/06 A RU2008141793/06 A RU 2008141793/06A RU 2008141793 A RU2008141793 A RU 2008141793A RU 2008141793 A RU2008141793 A RU 2008141793A
- Authority
- RU
- Russia
- Prior art keywords
- engine
- turbine
- shaft
- cylinders
- atomic gas
- Prior art date
Links
- 238000002485 combustion reaction Methods 0.000 claims abstract 2
- 239000002826 coolant Substances 0.000 claims abstract 2
Landscapes
- Engine Equipment That Uses Special Cycles (AREA)
Abstract
1. Атомный газотурбинный двигатель, содержащий внутренний и второй контуры, два вала, вентилятор установленный в задней части двигателя на втором валу, компрессор, камеру сгорания и турбину, с, по меньшей мере, одним рабочим колесом турбины, установленном на первом валу и реактивное сопло, отличающийся тем, что за турбиной на втором валу установлен двигатель Стерлинга, соединенный трубопроводами циркуляции теплоносителя с ядерным реактором. ! 2. Атомный газотурбинный двигатель по п.1, отличающийся тем, что двигатель Стерлинга выполнен из двух групп цилиндров: рабочих и поршневых, при этом рабочие цилиндры размещены в первом контуре, а расширительные - за вентилятором. 1. Atomic gas turbine engine containing internal and second circuits, two shafts, a fan mounted in the rear of the engine on the second shaft, a compressor, a combustion chamber and a turbine with at least one turbine impeller mounted on the first shaft and a jet nozzle characterized in that behind the turbine on the second shaft a Stirling engine is installed, connected by pipelines for the circulation of the coolant with a nuclear reactor. ! 2. The atomic gas turbine engine according to claim 1, characterized in that the Sterling engine is made of two groups of cylinders: working and piston, while the working cylinders are located in the primary circuit, and expansion cylinders are located behind the fan.
Claims (2)
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| RU2008141793/06A RU2008141793A (en) | 2008-10-21 | 2008-10-21 | ATOMIC GAS-TURBINE ENGINE |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| RU2008141793/06A RU2008141793A (en) | 2008-10-21 | 2008-10-21 | ATOMIC GAS-TURBINE ENGINE |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| RU2008141793A true RU2008141793A (en) | 2010-04-27 |
Family
ID=42672121
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| RU2008141793/06A RU2008141793A (en) | 2008-10-21 | 2008-10-21 | ATOMIC GAS-TURBINE ENGINE |
Country Status (1)
| Country | Link |
|---|---|
| RU (1) | RU2008141793A (en) |
-
2008
- 2008-10-21 RU RU2008141793/06A patent/RU2008141793A/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: 20100520 |