RU2014101280A - TWO-COMPONENT AIR-REACTIVE ENGINE - Google Patents
TWO-COMPONENT AIR-REACTIVE ENGINE Download PDFInfo
- Publication number
- RU2014101280A RU2014101280A RU2014101280/06A RU2014101280A RU2014101280A RU 2014101280 A RU2014101280 A RU 2014101280A RU 2014101280/06 A RU2014101280/06 A RU 2014101280/06A RU 2014101280 A RU2014101280 A RU 2014101280A RU 2014101280 A RU2014101280 A RU 2014101280A
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- RU
- Russia
- Prior art keywords
- combustion chamber
- supply system
- compressor
- nozzles
- gas turbine
- Prior art date
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- Fuel-Injection Apparatus (AREA)
Abstract
1. Двухкомпонентный воздушно-реактивный двигатель, содержащий воздухозаборник, корпус, компрессор с ротором компрессора, камеру сгорания, установленную за компрессором и соединенную с ним воздушным трактом, газовую турбину, вал соединяющий компрессор и газовую турбину, реактивное сопло и систему подачи топлива к камере сгорания, при этом к камере сгорания присоединена система подачи жидкого кислорода, отличающийся тем, что камера сгорания содержит две группы форсунок, к первой группе форсунок присоединена система подачи топлива, а ко второй - система подачи жидкого кислорода.2. Двухкомпонентный воздушно-реактивный двигатель по п. 1, отличающийся тем, что реактивное сопло выполнено сверхзвуковым.1. A two-component jet engine containing an air intake, a housing, a compressor with a compressor rotor, a combustion chamber installed behind the compressor and connected to it by an air path, a gas turbine, a shaft connecting the compressor and the gas turbine, a jet nozzle and a fuel supply system to the combustion chamber moreover, a liquid oxygen supply system is connected to the combustion chamber, characterized in that the combustion chamber contains two groups of nozzles, a fuel supply system is connected to the first group of nozzles, and w Oroi - liquid oxygen supply system. 2. The two-component jet engine according to claim 1, characterized in that the jet nozzle is made supersonic.
Claims (2)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
RU2014101280/06A RU2014101280A (en) | 2014-01-16 | 2014-01-16 | TWO-COMPONENT AIR-REACTIVE ENGINE |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
RU2014101280/06A RU2014101280A (en) | 2014-01-16 | 2014-01-16 | TWO-COMPONENT AIR-REACTIVE ENGINE |
Publications (1)
Publication Number | Publication Date |
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RU2014101280A true RU2014101280A (en) | 2015-08-10 |
Family
ID=53795613
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
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RU2014101280/06A RU2014101280A (en) | 2014-01-16 | 2014-01-16 | TWO-COMPONENT AIR-REACTIVE ENGINE |
Country Status (1)
Country | Link |
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RU (1) | RU2014101280A (en) |
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2014
- 2014-01-16 RU RU2014101280/06A patent/RU2014101280A/en unknown
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