FIELD: power engineering.
SUBSTANCE: operation of gas turbine engine with augmentation chamber consists in the making of fuel-air mix to be combusted in the main combustion chamber. Combustion products are expanded in the turbine and fed into the augmenter wherein combustion products are mixed with augmentation fuel. Said augmentation fuel is composed of aluminium nanoparticles, their radius not exceeding 25 nm. Water vapours and carbon dioxide contained in the main combustion chamber products are used as the oxidizer for augmentation fuel.
EFFECT: higher thrust of the engines.
6 cl, 1 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| COMBUSTION IN HYPERSONIC AIR JET ENGINE | 2014 |
|
RU2573425C1 |
| NANO-COMPONENT ENERGY SUPPLEMENT AND LIQUID HYDROCARBON FUEL | 2013 |
|
RU2529035C1 |
| METHOD OF CONTINUOUS OPERATION GAS TURBINE PLANT ACTION | 2015 |
|
RU2599407C1 |
| HYBRID AEROSPACE ROCKET RAMJET | 2014 |
|
RU2563641C2 |
| METHOD TO AUGMENT AIRCRAFT ENGINE | 2009 |
|
RU2386832C1 |
| NANOCOMPOSITE SOLID FUEL FOR RAMJET | 2016 |
|
RU2646933C1 |
| CONTROL OVER DUAL-FLOW TURBOJET ENGINE WITH AUGMENTER | 2014 |
|
RU2574213C1 |
| TURBO-JET ENGINE AND CONTROL METHOD THEREOF | 2016 |
|
RU2645373C1 |
| METHOD OF GAS TURBINE ENGINE AFTERBURNING | 2013 |
|
RU2523510C1 |
| METHOD OF TURBOJET AFTERBURNING AND ENGINE TO THIS END (VERSIONS) | 2011 |
|
RU2474718C2 |
