FIELD: rocket equipment.
SUBSTANCE: invention relates to injection devices for rocket engines. Injection device, combustion chamber and rocket engine comprises main housing (21) of device, divided into fuel manifold (33) and oxidant manifold (34), and plurality of injectors (22, 23, 24) arranged at preset intervals in main body (21) of device for injecting fuel and oxidant into flame tube (12), each of injectors (22A, 22B, 22C, 22D) contains channel (43a, 43b) LOx, containing proximal end section, connected with oxidant manifold (34), and a distal end portion communicating with flame tube (12), limiter (45a, 45b) provided on the proximal end portion of LOx channel (43a, 43b), and GH2 channel (47a, 47b), comprising a proximal end portion communicating with fuel manifold (33), and a distal end portion communicating with flame tube (12), wherein limiters (45a, 45b, 45s, 45d) have different shapes.
EFFECT: invention provides suppression of occurrence of combustion oscillations.
6 cl, 11 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| COMBUSTION CHAMBER AND ROCKET ENGINE | 2016 |
|
RU2698562C1 |
| SCROLL COMPRESSOR | 2012 |
|
RU2560647C1 |
| MULTI-COMPONENT CASE OF PACKAGES CONTAINING PRODUCTS OF MEDICINAL PURPOSE | 2005 |
|
RU2379013C2 |
| MACHINE FOR PREPARING BEVERAGES | 2013 |
|
RU2628716C2 |
| DAMPING DEVICE TO REDUCE PULSATION OF COMBUSTION CHAMBER | 2013 |
|
RU2568030C2 |
| MINIATURE ANTENNA WITH DOUBLE POLARIZATION FOR BASE STATION | 2015 |
|
RU2704206C2 |
| DUCT JOINING DEVICE WITH DIFFERENT-HEIGHT SECTIONS | 2002 |
|
RU2285990C2 |
| CONTROL SYSTEM FOR INTERNAL COMBUSTION ENGINE | 2021 |
|
RU2772173C1 |
| CONNECTOR DESIGNED FOR WET SHAVING CARTRIDGES MADE WITH THE POSSIBILITY OF ROTATION AROUND TWO AXES | 2018 |
|
RU2757043C2 |
| STARTING HEATER FOR AMMONIA SYNTHESIS REACTORS | 2009 |
|
RU2481888C2 |
