RU2008101228A - TURBINS AIRCRAFT ENGINE - Google Patents
TURBINS AIRCRAFT ENGINE Download PDFInfo
- Publication number
- RU2008101228A RU2008101228A RU2008101228/06A RU2008101228A RU2008101228A RU 2008101228 A RU2008101228 A RU 2008101228A RU 2008101228/06 A RU2008101228/06 A RU 2008101228/06A RU 2008101228 A RU2008101228 A RU 2008101228A RU 2008101228 A RU2008101228 A RU 2008101228A
- Authority
- RU
- Russia
- Prior art keywords
- compressor
- cascade
- low
- turbocompressor
- propeller
- Prior art date
Links
Landscapes
- Structures Of Non-Positive Displacement Pumps (AREA)
Abstract
1. Турбовинтовой авиационный двигатель, содержащий турбокомпрессор с корпусом, ротором турбокомпрессора, компрессором, камерой сгорания, выход из которой соединен газовым трактом с турбиной, реактивное сопло и воздушный вин, 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, а воздушный винт соединен с корпусом каскада компрессора низкого давления. ! 2. Двигатель по п.1, отличающийся тем, что воздушный винт установлен на входном обтекателе двигателя, соединенным с корпусом каскада компрессора низкого давления. 1. A turboprop aircraft engine containing a turbocompressor with a housing, a turbocompressor rotor, a compressor, a combustion chamber, the output of which is connected by a gas path to the turbine, a jet nozzle and an airscrew, characterized in that the compressor is made in two stages with low and high pressure cascades, this cascade of the low-pressure compressor is made birotative with a casing that can rotate in the direction opposite to the rotation of the turbocompressor rotor, and the propeller is connected to the cascade casing Low pressure compressors. ! 2. The engine according to claim 1, characterized in that the propeller is mounted on the inlet cowl of the engine connected to the cascade of the low pressure compressor.
Claims (2)
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| RU2008101228/06A RU2008101228A (en) | 2008-01-09 | 2008-01-09 | TURBINS AIRCRAFT ENGINE |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| RU2008101228/06A RU2008101228A (en) | 2008-01-09 | 2008-01-09 | TURBINS AIRCRAFT ENGINE |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| RU2008101228A true RU2008101228A (en) | 2009-07-20 |
Family
ID=41046789
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| RU2008101228/06A RU2008101228A (en) | 2008-01-09 | 2008-01-09 | TURBINS AIRCRAFT ENGINE |
Country Status (1)
| Country | Link |
|---|---|
| RU (1) | RU2008101228A (en) |
-
2008
- 2008-01-09 RU RU2008101228/06A patent/RU2008101228A/en unknown
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN105221295B (en) | Stamping-turbine air injection composite aero-engine | |
| SE0301412D0 (en) | Turbocharger system for an internal combustion engine | |
| GB588096A (en) | Improvements in or relating to internal combustion turbine power plants | |
| TR200603859T2 (en) | Turbo-cyclic integrated thrust motor | |
| RU2008101228A (en) | TURBINS AIRCRAFT ENGINE | |
| RU2007101124A (en) | COMBINED AIRCRAFT ENGINE | |
| RU2008100494A (en) | BIOTATIVE VENTILATION FAN AIRCRAFT ENGINE | |
| KR20110125717A (en) | Four-flow compressor | |
| RU2008100496A (en) | BIOTATIVE VENTILATION FAN AIRCRAFT ENGINE | |
| RU2007149538A (en) | BIOTATIVE VENTILATION FAN AIRCRAFT GAS TURBINE ENGINE | |
| RU2008100469A (en) | TURBINS AIRCRAFT ENGINE | |
| RU2006124303A (en) | GAS TURBINE COOLING SYSTEM OF A TURBOREACTIVE TWO-CIRCUIT ENGINE WITH ADDITIONAL COMPRESSION OF AIR IN A SMALL-SIZED FAN | |
| RU136492U1 (en) | COOLED TURBIN STAGE OF GAS TURBINE ENGINE | |
| RU2007147567A (en) | FAN AIRCRAFT ENGINE | |
| RU2008101575A (en) | TURBINS AIRCRAFT ENGINE | |
| RU2008115651A (en) | GAS TURBOCHEMBER AND TURBO-SCREW GAS TURBINE ENGINE | |
| RU2008110287A (en) | VERTICAL TAKEOFF AND LANDING AIRCRAFT ENGINE | |
| RU2023108455A (en) | GAS TURBINE ENGINE | |
| RU2008110285A (en) | VERTICAL TAKEOFF AND LANDING AIRCRAFT ENGINE | |
| RU2008113488A (en) | TURBOCHARGER AND POWER PLANT OF A TURBOCHARGER | |
| RU2023113890A (en) | Single-shaft turbofan engine | |
| RU2010105608A (en) | AIR REACTIVE ENGINE | |
| RU2008112095A (en) | TURBOCHARGER AND BASIC POWER PLANT OF A TURBOCHARGER | |
| RU2023108456A (en) | METHOD OF OPERATION OF A GAS TURBINE ENGINE | |
| PL424280A1 (en) | Revolving-block heat engine |