FIELD: machine building.
SUBSTANCE: invention relates to design of elements of the gas-turbine engines (GTE), and can be used in oil systems of the aviation GTE to maintain set pressure of the air-gas mixture in the breathing system of the oil cavities. The double-action barostatic valve for the breathing system of the aviation gas-turbine engine contains casing with two poppet valves connected in parallel to the breathing main line, one valve is barostatic, connected with sensing element receiving ambient pressure, and other valve is overpressure valve in breathing system. The valves are installed in opposite places relatively to the breathing main line. The sensing element is made in form of a package of individual membrane boxes, pressed through tray of the barostatic valve to the movable support installed in the casing at the opposite side of the package. The support is provided with the device fixing mutual position of the tray of the barostatic valve and its seat.
EFFECT: increased reliability of the unit operation due to pre-adjustment of the initial stroke of the barostatic valve.
1 dwg
Title | Year | Author | Number |
---|---|---|---|
BAROSTATIC DOUBLE ACTING CONTROL VALVE | 2014 |
|
RU2578766C1 |
DOUBLE-ACTING SAFETY VALVE FOR THE BREATHING SYSTEM OF OIL CAVITIES OF AIRCRAFT GAS TURBINE ENGINE | 2015 |
|
RU2596893C2 |
AIRCRAFT GAS TURBINE | 2013 |
|
RU2522713C1 |
OIL-SYSTEM OF THE GAS TURBINE ENGINE OF THE MANEUVERED AIRCRAFT | 2017 |
|
RU2640900C1 |
AIRCRAFT GAS TURBINE ENGINE OIL SYSTEM | 2014 |
|
RU2578784C1 |
GAS TURBINE ENGINE OIL SYSTEM | 2021 |
|
RU2779209C1 |
DEVICE FOR LUBRICATION OF SUPPORT BEARING OF ROTOR OF JET GAS TURBINE ENGINE | 2016 |
|
RU2623581C1 |
OIL SYSTEM OF GAS-TURBINE ENGINE | 2014 |
|
RU2539928C1 |
DEVICE FOR LUBRICATING BEARING SUPPORT OF TURBOMACHINE ROTOR | 2017 |
|
RU2639262C1 |
OIL SYSTEM OF AIR GAS TURBINE ENGINE | 2013 |
|
RU2535796C1 |
Authors
Dates
2015-08-10—Published
2014-07-16—Filed