RU2009149354A - ROTARY REACTIVE ENGINE - Google Patents
ROTARY REACTIVE ENGINE Download PDFInfo
- Publication number
- RU2009149354A RU2009149354A RU2009149354/06A RU2009149354A RU2009149354A RU 2009149354 A RU2009149354 A RU 2009149354A RU 2009149354/06 A RU2009149354/06 A RU 2009149354/06A RU 2009149354 A RU2009149354 A RU 2009149354A RU 2009149354 A RU2009149354 A RU 2009149354A
- Authority
- RU
- Russia
- Prior art keywords
- compressor
- adjacent
- casing
- combustion chambers
- rotary
- Prior art date
Links
- 238000002485 combustion reaction Methods 0.000 claims abstract 6
- 238000001816 cooling Methods 0.000 claims abstract 2
- 230000007246 mechanism Effects 0.000 claims abstract 2
- 239000000203 mixture Substances 0.000 claims abstract 2
Landscapes
- Supercharger (AREA)
Abstract
Роторно-реактивный двигатель, содержащий: корпус, ротор с валом, ц. компрессор, камеры сгорания, системы пуска, питания, зажигания и др. вспомогательные механизмы, обеспечивающие его работу, отличающийся тем, что в корпусе устройства, выполненном воздухозаборником, приготавливающим рабочую смесь, прилегающим к ц. компрессору с лопатками, заключенными в кожух с примыкающими к нему по внешней окружности симметрично расположенные окна входа камер сгораний, как минимум две и окнами выхода направленными по касательной в прилегающий к диску ц. компрессора, увеличенного в диаметре, кольцевому сборнику газовых продуктов с выхлопными патрубками, откуда, удаляясь, смешиваются с воздухом, охлаждающим камеры сгорания. A rotary-jet engine, comprising: a housing, a rotor with a shaft, c. compressor, combustion chambers, start-up systems, power supply, ignition, and other auxiliary mechanisms that ensure its operation, characterized in that in the casing of the device, made by an air intake preparing the working mixture, adjacent to c. a compressor with blades enclosed in a casing with symmetrically located windows of the entrance of the combustion chambers adjacent to it along the outer circumference, at least two and exit windows directed tangentially to the c adjacent to the disk. compressor, increased in diameter, an annular collection of gas products with exhaust pipes, from where, moving away, mixed with air cooling the combustion chamber.
Claims (1)
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| RU2009149354/06A RU2009149354A (en) | 2009-12-29 | 2009-12-29 | ROTARY REACTIVE ENGINE |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| RU2009149354/06A RU2009149354A (en) | 2009-12-29 | 2009-12-29 | ROTARY REACTIVE ENGINE |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| RU2009149354A true RU2009149354A (en) | 2011-07-10 |
Family
ID=44740018
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| RU2009149354/06A RU2009149354A (en) | 2009-12-29 | 2009-12-29 | ROTARY REACTIVE ENGINE |
Country Status (1)
| Country | Link |
|---|---|
| RU (1) | RU2009149354A (en) |
-
2009
- 2009-12-29 RU RU2009149354/06A patent/RU2009149354A/en not_active Application Discontinuation
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| HE9A | Changing address for correspondence with an applicant | ||
| HE9A | Changing address for correspondence with an applicant | ||
| FA92 | Acknowledgement of application withdrawn (lack of supplementary materials submitted) |
Effective date: 20141127 |