FIELD: motors and pumps.
SUBSTANCE: feature of the proposed oil system is in the preliminary coarse cleaning of compressed air and gases entering the breathing circuit of oil cavity of bearing support of the turbine rotor, from water and oil impurities, that allows to minimize the hydraulic resistance of integrated, uniform breathing circuit, connected with all others breathed oil cavities of the motor, and allows to minimize the load of the breathing separator ensuring complete final cleaning of discharged air and gases.
EFFECT: pressure of air and gases in oil cavities will be reduced, that will improve the reliability of operation of the motor breathing system, and the lubrication consumption is decreased, improvement of the environmental characteristics of the motor.
2 cl, 1 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| OIL SYSTEM OF A GAS TURBINE ENGINE | 2022 |
|
RU2786876C1 |
| AIRCRAFT GAS TURBINE ENGINE OIL SYSTEM | 2014 |
|
RU2578784C1 |
| AIRCRAFT GAS TURBINE | 2013 |
|
RU2522713C1 |
| OIL-GAS TURBINE ENGINE SYSTEM | 2017 |
|
RU2649377C1 |
| OIL SYSTEM OF GAS-TURBINE ENGINE | 2009 |
|
RU2416033C1 |
| OIL SYSTEM OF GAS-TURBINE ENGINE | 2016 |
|
RU2618996C1 |
| AIR BREATHING SYSTEM IN AIRCRAFT GAS TURBINE ENGINE | 2019 |
|
RU2709751C1 |
| OIL SYSTEM OF AVIATION GAS TURBINE ENGINE | 2013 |
|
RU2530968C1 |
| LUBRICATING SYSTEM OF GAS-TURBINE ENGINE | 1995 |
|
RU2117794C1 |
| OIL SYSTEM OF GAS-TURBINE ENGINE | 2014 |
|
RU2539928C1 |
