SU1453997A1 - TURBOCHARGER ENGINE - Google Patents
TURBOCHARGER ENGINEInfo
- Publication number
- SU1453997A1 SU1453997A1 SU4215286/06A SU4215286A SU1453997A1 SU 1453997 A1 SU1453997 A1 SU 1453997A1 SU 4215286/06 A SU4215286/06 A SU 4215286/06A SU 4215286 A SU4215286 A SU 4215286A SU 1453997 A1 SU1453997 A1 SU 1453997A1
- Authority
- SU
- USSR - Soviet Union
- Prior art keywords
- air intake
- additional
- intake housing
- fixed
- drive shaft
- Prior art date
Links
Landscapes
- Supercharger (AREA)
Abstract
1. Турбовентиляторный двигатель, содержащий воздухозаборник, расположенные в нем входной обтекатель и два нагнетательных венца, один из которых закреплен на внутренней поверхности корпуса воздухозаборника, и приводной вал, соединенный через редуктор с винтовентилятором, закрепленным на корпусе воздухозаборника, отличающийся тем, что, с целью повышения КПД, он снабжен дополнительным валом, соединенным с приводным валом, и редуктором, посредством которого второй нагнетательный венец подсоединен к дополнительному валу.2. Двигатель по п.1, отличающийся тем, что он снабжен дополнительным нагнетательным венцом, расположенным перед вторым нагнетательным венцом и закрепленным на внутренней поверхности корпуса воздухозаборника и входном обтекателе.1. A turbofan engine containing an air intake, an inlet fairing located therein and two pressure rings, one of which is fixed to the inner surface of the air intake housing, and a drive shaft connected through a reducer to a fan drive mounted on the air intake housing, characterized in that increase efficiency, it is equipped with an additional shaft connected to the drive shaft, and a gearbox, through which the second discharge ring is connected to an additional shaft. The engine according to claim 1, characterized in that it is provided with an additional discharge ring located in front of the second injection ring and fixed to the inner surface of the air intake housing and the inlet fairing.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
SU4215286/06A SU1453997A1 (en) | 1987-03-24 | 1987-03-24 | TURBOCHARGER ENGINE |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
SU4215286/06A SU1453997A1 (en) | 1987-03-24 | 1987-03-24 | TURBOCHARGER ENGINE |
Publications (1)
Publication Number | Publication Date |
---|---|
SU1453997A1 true SU1453997A1 (en) | 2005-10-10 |
Family
ID=60536459
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
SU4215286/06A SU1453997A1 (en) | 1987-03-24 | 1987-03-24 | TURBOCHARGER ENGINE |
Country Status (1)
Country | Link |
---|---|
SU (1) | SU1453997A1 (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
RU2482311C1 (en) * | 2011-12-14 | 2013-05-20 | Открытое акционерное общество "Авиадвигатель" | Gas turbine engine with aft location of open propeller fan |
-
1987
- 1987-03-24 SU SU4215286/06A patent/SU1453997A1/en active
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
RU2482311C1 (en) * | 2011-12-14 | 2013-05-20 | Открытое акционерное общество "Авиадвигатель" | Gas turbine engine with aft location of open propeller fan |
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