RU2010129629A - SPIRAL REACTIVE ENGINE - Google Patents
SPIRAL REACTIVE ENGINE Download PDFInfo
- Publication number
- RU2010129629A RU2010129629A RU2010129629/06A RU2010129629A RU2010129629A RU 2010129629 A RU2010129629 A RU 2010129629A RU 2010129629/06 A RU2010129629/06 A RU 2010129629/06A RU 2010129629 A RU2010129629 A RU 2010129629A RU 2010129629 A RU2010129629 A RU 2010129629A
- Authority
- RU
- Russia
- Prior art keywords
- spiral
- jet
- engine
- center
- shaped tube
- Prior art date
Links
Landscapes
- Jet Pumps And Other Pumps (AREA)
Abstract
Спиралевидный реактивный двигатель содержащий реактивный двигатель и трубный канал спиралевидной формы, отличающийся тем, что, с целью увеличения силы тяги реактивного двигателя за счет дополнительного увеличения скорости истечения реактивной струи, к выходному соплу двигателя подсоединяется трубный канал спиралевидной формы концом наиболее удаленным от центра спирали с дальнейшим прохождением реактивной струи через конец наименее удаленный от центра спирали с выходом во внешнее пространство. A spiral jet engine containing a jet engine and a spiral-shaped tube channel, characterized in that, in order to increase the thrust of the jet engine due to an additional increase in the jet flow rate, a spiral-shaped tube channel is connected to the engine output nozzle with the end farthest from the center of the spiral with a further the passage of the jet through the end least distant from the center of the spiral with access to the outer space.
Claims (1)
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| RU2010129629/06A RU2010129629A (en) | 2010-07-15 | 2010-07-15 | SPIRAL REACTIVE ENGINE |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| RU2010129629/06A RU2010129629A (en) | 2010-07-15 | 2010-07-15 | SPIRAL REACTIVE ENGINE |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| RU2010129629A true RU2010129629A (en) | 2012-01-20 |
Family
ID=45785380
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| RU2010129629/06A RU2010129629A (en) | 2010-07-15 | 2010-07-15 | SPIRAL REACTIVE ENGINE |
Country Status (1)
| Country | Link |
|---|---|
| RU (1) | RU2010129629A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| RU2672240C1 (en) * | 2016-07-20 | 2018-11-12 | Виталий Валериевич Кожевин | Pulsejet engine |
| CN110566363A (en) * | 2019-09-03 | 2019-12-13 | 中国航空工业集团公司西安飞机设计研究所 | Engine exhaust system |
-
2010
- 2010-07-15 RU RU2010129629/06A patent/RU2010129629A/en not_active Application Discontinuation
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| RU2672240C1 (en) * | 2016-07-20 | 2018-11-12 | Виталий Валериевич Кожевин | Pulsejet engine |
| CN110566363A (en) * | 2019-09-03 | 2019-12-13 | 中国航空工业集团公司西安飞机设计研究所 | Engine exhaust system |
| CN110566363B (en) * | 2019-09-03 | 2021-08-17 | 中国航空工业集团公司西安飞机设计研究所 | an engine exhaust system |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| MY172496A (en) | A tube module | |
| WO2015047509A3 (en) | Vena contracta swirling dilution passages for gas turbine engine combustor | |
| EA201490789A1 (en) | COOLED ENVIRONMENTAL TOP SUBMERSHIP LASKS | |
| GB2480199A (en) | Reversible oil pan with integrated oil suction tube | |
| GB0920115D0 (en) | A tubular conduit | |
| RU2012139075A (en) | NEUBULIZER SET AND NEBULIZER | |
| MX2011012080A (en) | Anti-siphon device. | |
| WO2015160403A3 (en) | Additive manufactured non-round, septum tied, conformal high pressure tubing | |
| RU2010129629A (en) | SPIRAL REACTIVE ENGINE | |
| RU2014144080A (en) | COMBUSTION CHAMBER WITH FORCED FLOW REVERSE | |
| RU2010124212A (en) | HYDRAULIC MIXER | |
| EA201650126A1 (en) | IMPLOSIVE TUBULAR REACTOR | |
| RU2009120771A (en) | DEVICE FOR COOLING BARKS OF SYSTEMS OF Rifle-guns | |
| CN204385820U (en) | Concealed bubbler | |
| CN203743691U (en) | Spiral T-branch pipe | |
| CN103470863A (en) | Ascending pipe | |
| RU2013111091A (en) | BELL DEVICE FOR RELEASING AN EXHAUST GAS | |
| RU2009141463A (en) | FUEL MIXER-DOSER | |
| MY168150A (en) | An exit assembly having a fluid diverter that displaces the pathway of a fluid into two or more pathway | |
| CN201851746U (en) | Pipe fitting connection structure | |
| RU2010109918A (en) | SUPERSONIC TUBE OF TEMPERATURE STRATIFICATION | |
| UA88736U (en) | Jet diode | |
| CN203284203U (en) | Ozone generation tube-air pump connection structure | |
| RU2010109920A (en) | SUPERSONIC TUBE OF TEMPERATURE STRATIFICATION | |
| RU2008136443A (en) | COOLING WATER DISCHARGE |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| FA93 | Acknowledgement of application withdrawn (no request for examination) |
Effective date: 20130716 |