RU2012103762A - AIR REACTIVE ENGINE - Google Patents
AIR REACTIVE ENGINE Download PDFInfo
- Publication number
- RU2012103762A RU2012103762A RU2012103762/06A RU2012103762A RU2012103762A RU 2012103762 A RU2012103762 A RU 2012103762A RU 2012103762/06 A RU2012103762/06 A RU 2012103762/06A RU 2012103762 A RU2012103762 A RU 2012103762A RU 2012103762 A RU2012103762 A RU 2012103762A
- Authority
- RU
- Russia
- Prior art keywords
- engine
- air
- compressor
- combustion chamber
- jet nozzle
- Prior art date
Links
- 238000002485 combustion reaction Methods 0.000 claims abstract 6
- 230000007246 mechanism Effects 0.000 claims abstract 4
- 239000012530 fluid Substances 0.000 claims abstract 2
- 239000000446 fuel Substances 0.000 claims abstract 2
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- Supercharger (AREA)
Abstract
Воздушно-реактивный двигатель, состоящий из корпуса, камеры сгорания, воздушного компрессора, вала, турбины, воздухозаборника, реактивного сопла и механизмов, обеспечивающих пуск и работу двигателя, отличающийся тем, что в предлагаемом двигателе привод механизмов, обеспечивающих работу двигателя, воздушного аппарата и двухстороннего центробежного компрессора осуществляет пульсирующий газотурбинный двигатель, расположенный перед тяговой камерой сгорания, куда от компрессора поступает воздушная масса, а после подачи топлива и его воспламенения продуктами сгорания от пульсирующего двигателя в камере объем рабочего тела возрастает и оно стремительно выходит в реактивное сопло, создавая тягу двигателя.Air-jet engine, consisting of a housing, a combustion chamber, an air compressor, a shaft, a turbine, an air intake, a jet nozzle and mechanisms for starting and operating the engine, characterized in that in the proposed engine the drive mechanisms for ensuring the operation of the engine, air device and two-sided the centrifugal compressor carries out a pulsating gas turbine engine located in front of the traction combustion chamber, where the air mass comes from the compressor, and after the fuel is supplied and lameneniya pulsating combustion products from the engine in the chamber volume of the working fluid increases and it goes rapidly into the jet nozzle, creating thrust of the engine.
Claims (1)
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| RU2012103762/06A RU2012103762A (en) | 2012-02-03 | 2012-02-03 | AIR REACTIVE ENGINE |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| RU2012103762/06A RU2012103762A (en) | 2012-02-03 | 2012-02-03 | AIR REACTIVE ENGINE |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| RU2012103762A true RU2012103762A (en) | 2013-08-10 |
Family
ID=49159240
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| RU2012103762/06A RU2012103762A (en) | 2012-02-03 | 2012-02-03 | AIR REACTIVE ENGINE |
Country Status (1)
| Country | Link |
|---|---|
| RU (1) | RU2012103762A (en) |
-
2012
- 2012-02-03 RU RU2012103762/06A patent/RU2012103762A/en unknown
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