RU2008123685A - SILENT-FREE SUPERUNICAL AIR-TURBINE ENGINE FOR SCREW PLANES OPERATING FROM COLD AND HOT HEAT SOURCES - Google Patents
SILENT-FREE SUPERUNICAL AIR-TURBINE ENGINE FOR SCREW PLANES OPERATING FROM COLD AND HOT HEAT SOURCES Download PDFInfo
- Publication number
- RU2008123685A RU2008123685A RU2008123685/06A RU2008123685A RU2008123685A RU 2008123685 A RU2008123685 A RU 2008123685A RU 2008123685/06 A RU2008123685/06 A RU 2008123685/06A RU 2008123685 A RU2008123685 A RU 2008123685A RU 2008123685 A RU2008123685 A RU 2008123685A
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- RU
- Russia
- Prior art keywords
- air
- isothermal
- silent
- cold
- working
- Prior art date
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- 239000012530 fluid Substances 0.000 claims abstract 2
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- Engine Equipment That Uses Special Cycles (AREA)
Abstract
Бесшумный суперуникальный воздухотурбинный двигатель для винтовых самолетов, работающих от холодного и горячего источников тепла, состоящий из изотермической части, где происходит приготовление двух рабочих тел при расширении и сжатии для них атмосферного воздуха одновременно, адиабатической части (поршневого компрессора) и силовой установки: спирального нагревателя рабочих тел, турбины с электрогенератором, не имеющих аналогов в мире, отличающийся тем, что оба рабочих тела образуются в изотермической части (цилиндрах за счет отбора тепла от поступающего в цилиндры атмосферного воздуха при его сжатии и передаче его расширяемому изотермически воздуху, который далее поступает в поршневой компрессор, а из него в печь, а сжатый воздух при Р=25 кг/см2 поступает в спиральный нагреватель и обеспечивает работу всей системы двигателя с КПД, близким к 100%, что является главным достижением технического результата.Silent super-unique air-turbine engine for airliners operating from cold and hot heat sources, consisting of an isothermal part, where two working fluids are prepared while expanding and compressing atmospheric air for them at the same time, an adiabatic part (piston compressor) and a power plant: spiral working heater bodies, turbines with an electric generator that have no analogues in the world, characterized in that both working bodies are formed in the isothermal part (cylinders due to selection heat from atmospheric air entering the cylinders when it is compressed and transferred to expandable isothermal air, which then enters the piston compressor, and from it into the furnace, and compressed air at P = 25 kg / cm2 enters the spiral heater and ensures the operation of the entire engine system with an efficiency close to 100%, which is the main achievement of the technical result.
Claims (1)
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| RU2008123685/06A RU2008123685A (en) | 2008-06-10 | 2008-06-10 | SILENT-FREE SUPERUNICAL AIR-TURBINE ENGINE FOR SCREW PLANES OPERATING FROM COLD AND HOT HEAT SOURCES |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| RU2008123685/06A RU2008123685A (en) | 2008-06-10 | 2008-06-10 | SILENT-FREE SUPERUNICAL AIR-TURBINE ENGINE FOR SCREW PLANES OPERATING FROM COLD AND HOT HEAT SOURCES |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| RU2008123685A true RU2008123685A (en) | 2009-12-20 |
Family
ID=41625424
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| RU2008123685/06A RU2008123685A (en) | 2008-06-10 | 2008-06-10 | SILENT-FREE SUPERUNICAL AIR-TURBINE ENGINE FOR SCREW PLANES OPERATING FROM COLD AND HOT HEAT SOURCES |
Country Status (1)
| Country | Link |
|---|---|
| RU (1) | RU2008123685A (en) |
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2008
- 2008-06-10 RU RU2008123685/06A patent/RU2008123685A/en not_active Application Discontinuation
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| FA92 | Acknowledgement of application withdrawn (lack of supplementary materials submitted) |
Effective date: 20100406 |