FIELD: aircraft engineering. SUBSTANCE: aircraft engine has additional propeller with gas turbine concentric with reactive drives. Main and additional propellers are positioned on support posts for reversing their rotation. EFFECT: improved design. 2 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| ROTARY ENGINE | 0 |
|
SU1809858A3 |
| STEAM-TURBINE ENGINE | 1994 |
|
RU2086790C1 |
| KRISHTOP COMBINED TURBOPROP - TURBOJET ENGINE (KTVTRDK) AND METHOD OF ITS FUNCTIONING | 2021 |
|
RU2791783C1 |
| VORTEX GAS COMPRESSOR DEVICE FOR COMBINED AIR-JET ENGINE | 2019 |
|
RU2766496C2 |
| METHOD OF CREATING A TRAIL AND POWER INSTALLATION FOR ITS IMPLEMENTATION | 2017 |
|
RU2680214C1 |
| SUBSONIC AND STATIONARY RAMJETS | 2009 |
|
RU2516075C2 |
| HYPERSONIC TURBO EJECTOR ENGINE | 2009 |
|
RU2386829C1 |
| PULSE GAS-TURBINE EJECTOR ENGINE (VERSIONS) | 2005 |
|
RU2362033C2 |
| METHOD OF ENERGY CONVERSION IN POWER PLANT (VERSIONS), JET-ADAPTIVE ENGINE AND GAS GENERATOR | 2001 |
|
RU2188960C1 |
| TURBOFAN ENGINE | 2001 |
|
RU2209329C2 |
Authors
Dates
1994-05-30—Published
1991-05-21—Filed