FIELD: engine devices and pumps.
SUBSTANCE: combustion chamber comprising a gas conduit, a mixing head with mixing elements, a chamber body and fuel supply lines is described, according to the invention, in the region of chamber minimum section, a toroidal gas conduit is made, the cavity of which, by means of a finned path made on the outer wall of the chamber body and head outer bottom, is connected to head mixing elements.
EFFECT: increasing the reliability of combustion chamber and reducing the linear size of combustion chamber.
4 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| CHAMBER OF LRE, WHICH OPERATES WITH AFTERBURNING OF GENERATOR GAS | 2020 |
|
RU2742251C1 |
| CHAMBER OF A LIQUID-PROPELLANT ROCKET ENGINE OPERATING WITH AFTERBURNING OF A REDUCING GENERATOR GAS | 2020 |
|
RU2746029C1 |
| LIQUID-PROPELLANT ROCKET ENGINE (LPRE) COMBUSTION CHAMBER WITH ELECTROPLASMA IGNITION | 2014 |
|
RU2561796C1 |
| LRE CHAMBER OPERATING ON THREE COMPONENTS OF FUEL OXYGEN, HYDROGEN AND HYDROCARBON IN A CLOSED CIRCUIT WITH AFTERBURNING OF OXIDIZING GENERATOR GAS | 2022 |
|
RU2793927C1 |
| LPE COMBUSTION CHAMBER WITH ELECTROPLASMA IGNITION | 2014 |
|
RU2553583C1 |
| COMBUSTION CHAMBER OF LPE WITH ELECTROPLASMA IGNITION | 2016 |
|
RU2638418C1 |
| DEVICE FOR REGENERATIVE COOLING OF LIQUID-PROPELLANT ENGINE SUPERSONIC SECTION | 2012 |
|
RU2514570C1 |
| LRE GAS PATH | 2015 |
|
RU2579296C1 |
| DEVICE FOR REGENERATIVE COOLING OF SUPERSONIC PART OF LIQUID ROCKET ENGINE NOZZLE | 2018 |
|
RU2687548C1 |
| LIQUID PROPELLANT ROCKET ENGINE (VERSIONS) | 2006 |
|
RU2301352C1 |
