RU2008100496A - BIOTATIVE VENTILATION FAN AIRCRAFT ENGINE - Google Patents
BIOTATIVE VENTILATION FAN AIRCRAFT ENGINE Download PDFInfo
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- RU2008100496A RU2008100496A RU2008100496/06A RU2008100496A RU2008100496A RU 2008100496 A RU2008100496 A RU 2008100496A RU 2008100496/06 A RU2008100496/06 A RU 2008100496/06A RU 2008100496 A RU2008100496 A RU 2008100496A RU 2008100496 A RU2008100496 A RU 2008100496A
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- RU
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- Prior art keywords
- turbocompressor
- engine according
- turbine
- casing
- fan
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Abstract
1. Биротативный винтовентиляторный авиационный газотурбинный двигатель, содержащий турбокомпрессор с корпусом, ротором турбокомпрессора, имеющим вал турбокомпрессора, компрессором, камерой сгорания, выход из которой соединен газовым трактом с турбиной, реактивное сопло и двухступенчатый винтовентилятор, отличающийся тем, что турбина выполнена биротативной с корпусом, имеющим возможность вращения в сторону, противоположную вращению ротора турбокомпрессора, первая ступень винтовентилятора установлена на корпусе турбины, а вторая соединена с валом турбокомпрессора. ! 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 перед ступенями винтовентилятора. ! 5. Двигатель по п.1, отличающийся тем, что вторая ступень винтовентилятора соединена с валом турбокомпрессора посредством внутренних опор, находящихся внутри реактивного сопла. ! 6. Двигатель по п.5, отличающийся тем, что внутренние опоры имеют профиль лопаток турбины.1. A rotational propeller-driven aviation gas turbine engine comprising a turbocompressor with a casing, a turbocompressor rotor having a turbocompressor shaft, 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, characterized in that the turbine is made of a turbotransformer with a casing, having the ability to rotate in the direction opposite to the rotation of the rotor of the turbocompressor, the first stage of the fan is mounted on the turbine housing, and the second dinene with turbocharger shaft. ! 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 in front of the stages of the fan. ! 5. The engine according to claim 1, characterized in that the second stage of the fan is connected to the turbocompressor shaft by means of internal bearings located inside the jet nozzle. ! 6. The engine according to claim 5, characterized in that the internal bearings have a profile of the turbine blades.
Claims (6)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
RU2008100496/06A RU2008100496A (en) | 2008-01-09 | 2008-01-09 | BIOTATIVE VENTILATION FAN AIRCRAFT ENGINE |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
RU2008100496/06A RU2008100496A (en) | 2008-01-09 | 2008-01-09 | BIOTATIVE VENTILATION FAN AIRCRAFT ENGINE |
Publications (1)
Publication Number | Publication Date |
---|---|
RU2008100496A true RU2008100496A (en) | 2009-07-20 |
Family
ID=41046619
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
RU2008100496/06A RU2008100496A (en) | 2008-01-09 | 2008-01-09 | BIOTATIVE VENTILATION FAN AIRCRAFT ENGINE |
Country Status (1)
Country | Link |
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RU (1) | RU2008100496A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
RU2698497C1 (en) * | 2018-12-10 | 2019-08-28 | Николай Борисович Болотин | Vertical take-off and landing aircraft |
-
2008
- 2008-01-09 RU RU2008100496/06A patent/RU2008100496A/en unknown
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
RU2698497C1 (en) * | 2018-12-10 | 2019-08-28 | Николай Борисович Болотин | Vertical take-off and landing aircraft |
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