FIELD: gas industry.
SUBSTANCE: invention relates to gas industry and can be used in operation of gas transfer unit GPA-C25BD/100-1,35M in composition with gas turbine engine NK-36ST in conditions of compressor stations. To obtain this result, it is necessary to provide constant air flow in gas turbine engine breathing system by mounting additional pipeline from air receiver main with constant preset air pressure to gas compressor unit to oil tank venting system.
EFFECT: object of the invention is to increase the gas turbine engine oil tank breathing system efficiency by reducing oil consumption.
1 cl, 1 dwg
Title | Year | Author | Number |
---|---|---|---|
METHOD OF PREVENTION OF CARBONIZATION OF OIL IN TURBINE SUPPORT OF GAS-TURBINE ENGINE WORKING TOGETHER WITH GAS- TRANSFER UNIT OR POWER PLANT FOR DRIVING ELECTRIC GENERATOR | 1994 |
|
RU2105177C1 |
AIRCRAFT GAS TURBINE ENGINE OIL SYSTEM | 2014 |
|
RU2578784C1 |
OIL SYSTEM OF GAS-TURBINE ENGINE | 2016 |
|
RU2618996C1 |
AIR BREATHING SYSTEM IN AIRCRAFT GAS TURBINE ENGINE | 2019 |
|
RU2709751C1 |
LUBRICATING SYSTEM OF GAS COMPRESSOR UNIT WITH STATIONARY GAS TURBINE ENGINE | 2019 |
|
RU2742591C1 |
OIL SYSTEM OF AIR GAS TURBINE ENGINE | 2013 |
|
RU2535796C1 |
STATIONARY GAS-TURBINE PLANT OIL STATION | 2017 |
|
RU2657925C1 |
OIL LUBRICATING SYSTEM OF GAS-TURBINE ENGINE WITH OIL RESERVING DEVICE | 1998 |
|
RU2136931C1 |
GAS TURBINE ENGINE OIL SYSTEM | 2021 |
|
RU2779209C1 |
OIL SYSTEM OF A GAS TURBINE ENGINE | 2022 |
|
RU2786876C1 |
Authors
Dates
2019-04-12—Published
2018-05-17—Filed