RU2009135275A - AIR-REACTIVE ENGINE (OPTIONS) - Google Patents
AIR-REACTIVE ENGINE (OPTIONS) Download PDFInfo
- Publication number
- RU2009135275A RU2009135275A RU2009135275/06A RU2009135275A RU2009135275A RU 2009135275 A RU2009135275 A RU 2009135275A RU 2009135275/06 A RU2009135275/06 A RU 2009135275/06A RU 2009135275 A RU2009135275 A RU 2009135275A RU 2009135275 A RU2009135275 A RU 2009135275A
- Authority
- RU
- Russia
- Prior art keywords
- compressor
- mechanical energy
- jet engine
- ducts
- compressed air
- Prior art date
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- Compressors, Vaccum Pumps And Other Relevant Systems (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Abstract
1. Воздушно-реактивный двигатель, включающий компрессор, отличающийся тем, что содержит устройство для привода компрессора, в качестве которого используют роторную машину объемного типа, механически связанную с компрессором, и выполненную с возможностью поступления в ее рабочие объемы сжатого воздуха от компрессора и/или от других внешних источников посредством воздуховодов. ! 2. Воздушно-реактивный двигатель, включающий компрессор, отличающийся тем, что содержит устройства для приводов компрессора и других потребителей механической энергии, в качестве которых используют, по меньшей мере, две роторных машины объемного типа, одна из которых механически связана с компрессором, а, по меньшей мере, одна из них соединена последовательно с соответствующим потребителем механической энергии, при этом роторные машины выполнены с возможностью поступления в их рабочие объемы сжатого воздуха от компрессора и/или от других внешних источников посредством воздуховодов. ! 3. Воздушно-реактивный двигатель по п.2, отличающийся тем, что в качестве потребителя механической энергии двигатель содержит движитель или компрессор низкого давления, или самолетный агрегат. 1. The jet engine, comprising a compressor, characterized in that it contains a device for driving a compressor, which is used as a volumetric rotary machine, mechanically connected to the compressor, and configured to receive compressed air from the compressor and / or from other external sources through ducts. ! 2. A jet engine comprising a compressor, characterized in that it comprises devices for compressor drives and other consumers of mechanical energy, which are used as at least two volumetric rotary machines, one of which is mechanically connected to the compressor, and, at least one of them is connected in series with the corresponding consumer of mechanical energy, while the rotary machines are configured to receive compressed air from their compressor and / or from another x external sources through ducts. ! 3. The jet engine according to claim 2, characterized in that, as a consumer of mechanical energy, the engine comprises a low-pressure propulsion device or compressor, or an aircraft assembly.
Claims (3)
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| RU2009135275/06A RU2009135275A (en) | 2009-09-22 | 2009-09-22 | AIR-REACTIVE ENGINE (OPTIONS) |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| RU2009135275/06A RU2009135275A (en) | 2009-09-22 | 2009-09-22 | AIR-REACTIVE ENGINE (OPTIONS) |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| RU2009135275A true RU2009135275A (en) | 2011-03-27 |
Family
ID=44052574
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| RU2009135275/06A RU2009135275A (en) | 2009-09-22 | 2009-09-22 | AIR-REACTIVE ENGINE (OPTIONS) |
Country Status (1)
| Country | Link |
|---|---|
| RU (1) | RU2009135275A (en) |
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2009
- 2009-09-22 RU RU2009135275/06A patent/RU2009135275A/en unknown
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