FIELD: engines and pumps.
SUBSTANCE: constant volume combustion chamber for aviation turbine engine comprises a compressed gas intake valve configured to receive an open position and a closed position in which it blocks the injection of compressed gas into the chamber. The chamber further comprises a flue gas discharge valve configured to receive a closed position in which it blocks the release of the combustion gases to the outside of the chamber. At least one of the intake and exhaust valves comprises at least one spherical end cap.
EFFECT: increased reliability and tightness of the intake and exhaust valves.
11 cl, 29 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| ANTI-CAVITATION ELEMENT FOR USE WITH VALVES | 2017 |
|
RU2754835C2 |
| COMBUSTION MODULE AT CONSTANT VOLUME FOR GAS TURBINE ENGINE | 2016 |
|
RU2714386C2 |
| CONSTANT VOLUME COMBUSTION MODULE FOR A GAS TURBINE ENGINE COMPRISING AN IGNITION SYSTEM BY MEANS OF A COMMUNICATION LINE | 2016 |
|
RU2720868C2 |
| HEATER DEVICE AND HEATER OPERATION CONTROL METHOD | 2016 |
|
RU2702257C2 |
| CUSHION HAVING A PLURALITY OF POROUS OPENINGS | 2015 |
|
RU2698010C2 |
| PRESSURE INCREASING DEVICE | 2018 |
|
RU2736237C1 |
| BRAKING SYSTEM OF TECHNOLOGICAL MACHINE | 2012 |
|
RU2623930C2 |
| SPHERICAL INTERNAL COMBUSTION ENGINE | 2019 |
|
RU2701651C1 |
| DEVICE FOR DISTRIBUTING AND BATCHING | 2002 |
|
RU2295482C2 |
| INTERNAL COMBUSTION ENGINE AND METHOD FOR CONTROLLING THE INTERNAL COMBUSTION ENGINE | 2017 |
|
RU2649412C1 |
