RU2009110072A - TWO-CIRCULAR GAS-TURBINE ENGINE WITH ELECTROMAGNETIC ACCELERATOR - Google Patents
TWO-CIRCULAR GAS-TURBINE ENGINE WITH ELECTROMAGNETIC ACCELERATOR Download PDFInfo
- Publication number
- RU2009110072A RU2009110072A RU2009110072/06A RU2009110072A RU2009110072A RU 2009110072 A RU2009110072 A RU 2009110072A RU 2009110072/06 A RU2009110072/06 A RU 2009110072/06A RU 2009110072 A RU2009110072 A RU 2009110072A RU 2009110072 A RU2009110072 A RU 2009110072A
- Authority
- RU
- Russia
- Prior art keywords
- engine
- low
- middle support
- turbine
- nozzle
- Prior art date
Links
- 229910052754 neon Inorganic materials 0.000 claims abstract 6
- 238000002485 combustion reaction Methods 0.000 claims abstract 4
- 239000007788 liquid Substances 0.000 claims abstract 4
- GKAOGPIIYCISHV-UHFFFAOYSA-N neon atom Chemical compound [Ne] GKAOGPIIYCISHV-UHFFFAOYSA-N 0.000 claims abstract 4
- 238000001816 cooling Methods 0.000 claims abstract 2
- 238000004804 winding Methods 0.000 claims abstract 2
Landscapes
- Engine Equipment That Uses Special Cycles (AREA)
Abstract
Двухконтурный газотурбинный двигатель с электромагнитным ускорителем содержащий воздушно-неоновый теплообменник с регенератором холода, расположенный на входе и вписанный в проточную часть двигателя, среднюю опору, камеру сгорания с шароторовым конвектором, турбины высокого и низкого давлений, форсажную камеру, сопло Лаваля, отличающийся тем, что он снабжен криотурбогенератором, ротор которого охлаждается жидким неоном, а статор жидким воздухом и расположен между неоновым теплообменником и средней опорой по оси двигателя, соединен валом с турбиной низкого давления, шнеком-бустером, расположенным между средней опорой и камерой сгорания с шароторовым конвектором, связанным валом с турбиной высокого давления, электромагнитным ускорителем, обмотки которого охватывают наружный корпус двигателя над криотурбогенератором, ядерным реактором на быстрых нейтронах, расположенным за турбиной низкого давления по оси двигателя под стекателем сопла, на левой цапфе шнек-бустера смонтирован вентилятор, подающий воздух для охлаждения дисков и лопаток турбин высокого и низкого давлений. A double-circuit gas turbine engine with an electromagnetic accelerator containing an air-neon heat exchanger with a cold regenerator located at the inlet and inscribed in the engine's flow part, a middle support, a combustion chamber with a charotor convector, high and low pressure turbines, afterburner, a Laval nozzle, characterized in that it is equipped with a cryoturbogenerator, the rotor of which is cooled by liquid neon, and the stator by liquid air and is located between the neon heat exchanger and the middle support along the axis of the engine, connected to Scrap with a low-pressure turbine, a booster screw located between the middle support and the combustion chamber with a sharotor convector, a shaft connected to a high-pressure turbine, an electromagnetic accelerator, the windings of which cover the outer engine casing above the cryoturbogenerator, a fast fast neutron nuclear reactor located behind the low-turbine pressure along the axis of the engine under the nozzle nozzle, a fan is mounted on the left axle of the auger booster, which supplies air for cooling disks and blades of high and low turbines yes phenomena.
Claims (1)
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| RU2009110072/06A RU2009110072A (en) | 2009-03-19 | 2009-03-19 | TWO-CIRCULAR GAS-TURBINE ENGINE WITH ELECTROMAGNETIC ACCELERATOR |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| RU2009110072/06A RU2009110072A (en) | 2009-03-19 | 2009-03-19 | TWO-CIRCULAR GAS-TURBINE ENGINE WITH ELECTROMAGNETIC ACCELERATOR |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| RU2009110072A true RU2009110072A (en) | 2010-09-27 |
Family
ID=42939866
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| RU2009110072/06A RU2009110072A (en) | 2009-03-19 | 2009-03-19 | TWO-CIRCULAR GAS-TURBINE ENGINE WITH ELECTROMAGNETIC ACCELERATOR |
Country Status (1)
| Country | Link |
|---|---|
| RU (1) | RU2009110072A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| RU2686815C1 (en) * | 2018-05-10 | 2019-04-30 | Андрей Юрьевич Бельский | Nuclear turbojet |
-
2009
- 2009-03-19 RU RU2009110072/06A patent/RU2009110072A/en not_active Application Discontinuation
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| RU2686815C1 (en) * | 2018-05-10 | 2019-04-30 | Андрей Юрьевич Бельский | Nuclear turbojet |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| FA92 | Acknowledgement of application withdrawn (lack of supplementary materials submitted) |
Effective date: 20101010 |