FIELD: jet engine plants. SUBSTANCE: engine has reaction nozzle with detonation combustion chamber 1, working mixture formation and supply system 2 and detonation excitation system 3. Working mixture formation and supply system is provided with gas generator 4 and detonation excitation system is provided with prechamber 5 and gas-dynamic valve 6. EFFECT: enhanced efficiency. 1 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| PULSEJET ENGINE DETONATION CHAMBER | 1993 |
|
RU2078969C1 |
| ADJUSTABLE DETONATION CHAMBER OF PULSEJET ENGINE | 1993 |
|
RU2078974C1 |
| REACTION NOZZLE OF DETONATION COMBUSTION PULSATING ENGINE WITH CENTRAL BODY | 1993 |
|
RU2066779C1 |
| COMBINED CHAMBER OF DETONATION COMBUSTION PULSEJET ENGINE | 1993 |
|
RU2080466C1 |
| CHAMBER FOR PULS DETONATION ENGINE | 1994 |
|
RU2084675C1 |
| DETONATION CHAMBER OF PULSE-JET ENGINE | 1994 |
|
RU2106509C1 |
| DETONATION COMBUSTION PULSE-JET ENGINE | 1997 |
|
RU2142058C1 |
| TRANSFORMABLE ROCKET-AIR JET DETONATION COMBUSTION ENGINE (VERSIONS) | 2019 |
|
RU2704503C1 |
| DETONATION PULSATING ROCKET-AIR-JET ENGINE (DPRAJE) AND THE METHOD FOR FUNCTIONING OF THE DPRAJE (OPTIONS) | 2021 |
|
RU2781720C1 |
| ENVIRONMENTALLY SAFE POWER PLANT BASED ON DETONATION COMBUSTION CHAMBER | 2013 |
|
RU2564658C2 |
Authors
Dates
1996-09-20—Published
1993-06-10—Filed