FIELD: aircraft engineering.
SUBSTANCE: invention relates to the field of aviation, in particular to methods for rotating the lifting propellers of rotary-wing aircraft. The method for rotating the lifting propeller using at least one jet engine is that a mixture of gaseous fuel and an oxidizer is burned at the combustion site to produce a jet stream that creates thrust for the rotation of the lifting propeller. The combustion process is the process of detonation of a mixture of gaseous fuels and an oxidizer. In this case, the liquid fuel evaporates to a gaseous state before being transported to the combustion site, and the gaseous fuel is transported to the combustion site due to centrifugal forces generated by the rotating lifting propeller.
EFFECT: efficiency of the jet-driven rotor is improved by reducing energy consumption for preparing the mixture of fuel and oxidizer for combustion.
15 cl, 3 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| PULSATING DETONATION JET ENGINE | 2020 |
|
RU2752817C1 |
| METHOD OF FUEL COMBUSTION AND DETONATION DEVICE FOR ITS IMPLEMENTATION | 2014 |
|
RU2595005C9 |
| OPERATING METHOD OF PULSE-DETONATION ENGINE IN CENTRIFUGAL FORCE FIELD AND DEVICE FOR IMPLEMENTATION THEREOF IN JET HELICOPTER | 2018 |
|
RU2718726C1 |
| SOLID FUEL COMBUSTION METHOD, AND DEVICE FOR ITS IMPLEMENTATION | 2010 |
|
RU2468292C2 |
| DETONATION SELF-SUSTAUINING DEVICE | 1997 |
|
RU2201293C2 |
| DETONATION COMBUSTION METHOD OF FLAMMABLE MIXTURES, AND DEVICE FOR ITS IMPLEMENTATION | 2009 |
|
RU2459150C2 |
| ENVIRONMENTALLY SAFE POWER PLANT BASED ON DETONATION COMBUSTION CHAMBER | 2013 |
|
RU2564658C2 |
| METHOD FOR DETONATION COMBUSTION OF FUEL MIXTURES AND DEVICE FOR ITS IMPLEMENTATION | 2014 |
|
RU2595004C9 |
| METHOD AND DEVICE FOR ARRANGEMENT OF PERIODIC OPERATION OF CONTINUOUS-DETONATION COMBUSTION CHAMBER | 2019 |
|
RU2724558C1 |
| SOLID FUEL RAMJET ENGINE AND METHOD OF ITS FUNCTIONING | 2021 |
|
RU2796043C2 |
