RU2008100494A - BIOTATIVE VENTILATION FAN AIRCRAFT ENGINE - Google Patents
BIOTATIVE VENTILATION FAN AIRCRAFT ENGINE Download PDFInfo
- Publication number
- RU2008100494A RU2008100494A RU2008100494/06A RU2008100494A RU2008100494A RU 2008100494 A RU2008100494 A RU 2008100494A RU 2008100494/06 A RU2008100494/06 A RU 2008100494/06A RU 2008100494 A RU2008100494 A RU 2008100494A RU 2008100494 A RU2008100494 A RU 2008100494A
- Authority
- RU
- Russia
- Prior art keywords
- turbocompressor
- compressor
- rotor
- low
- engine according
- Prior art date
Links
- 238000009423 ventilation Methods 0.000 title 1
- 241000036848 Porzana carolina Species 0.000 claims abstract 2
- 238000002485 combustion reaction Methods 0.000 claims abstract 2
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- Structures Of Non-Positive Displacement Pumps (AREA)
Abstract
1. Биротативный винтовентиляторный авиационный газотурбинный двигатель, содержащий турбокомпрессор с корпусом, ротором турбокомпрессора, компрессором, камерой сгорания, выход из которой соединен газовым трактом с турбиной, реактивное сопло и двухступенчатый винтовентилятор, отличающийся тем, что компрессор выполнен двухкаскадным, с каскадами низкого и высокого давления, при этом каскад компрессора низкого давления выполнен биротативным с корпусом, имеющим возможность вращения в сторону, противоположную вращению ротора турбокомпрессора, первая ступень винтовентилятора соединена с ротором турбокомпрессора, а вторая установлена на корпусе каскада компрессора низкого давления. ! 2. Двигатель по п.1, отличающийся тем, что концентрично корпусу турбокомпрессора выполнен внешний корпус. ! 3. Двигатель по п.2, отличающийся тем, что внешний корпус прикреплен к корпусу турбокомпрессора при помощи опор. ! 4. Двигатель по п.3, отличающийся тем, что опоры установлены за винтовентилятором.1. A rotational propeller-driven aviation gas turbine engine containing a turbocompressor with a housing, a turbocompressor rotor, a compressor, a combustion chamber, the outlet of which is connected by a gas path to the turbine, a jet nozzle and a two-stage propeller fan, characterized in that the compressor is made in two stages with low and high pressure stages wherein the cascade of the low-pressure compressor is made birotative with a housing having the ability to rotate in the direction opposite to the rotation of the turbocompressor rotor sora, the first stage of the fan heater is connected to the rotor of the turbocompressor, and the second is installed on the cascade of the low-pressure compressor. ! 2. The engine according to claim 1, characterized in that the outer housing is made concentric to the turbocharger body. ! 3. The engine according to claim 2, characterized in that the outer casing is attached to the casing of the turbocompressor using supports. ! 4. The engine according to claim 3, characterized in that the bearings are installed behind the fan.
Claims (4)
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| RU2008100494/06A RU2008100494A (en) | 2008-01-09 | 2008-01-09 | BIOTATIVE VENTILATION FAN AIRCRAFT ENGINE |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| RU2008100494/06A RU2008100494A (en) | 2008-01-09 | 2008-01-09 | BIOTATIVE VENTILATION FAN AIRCRAFT ENGINE |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| RU2008100494A true RU2008100494A (en) | 2009-07-20 |
Family
ID=41046618
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| RU2008100494/06A RU2008100494A (en) | 2008-01-09 | 2008-01-09 | BIOTATIVE VENTILATION FAN AIRCRAFT ENGINE |
Country Status (1)
| Country | Link |
|---|---|
| RU (1) | RU2008100494A (en) |
-
2008
- 2008-01-09 RU RU2008100494/06A patent/RU2008100494A/en unknown
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