FIELD: motors and pumps.
SUBSTANCE: group of inventions belongs to the field of aircraft engine building. Mounted in the oil unit housing, the discharge pump is installed on the monitoring diagnostic equipment (MDE) cover in the used oil drain area. Discharge pump comprises a gear operating element, which includes two impellers mounted on parallel shafts, each providing a bearing. Drive shaft is communicated by torque through the drive gear reducer spring to the power source. On the driven shaft, a driving wheel is installed that transfers the energy of rotation to the driven one mounted on the drive shaft. Frontal thrust plates are installed in the lower shell, and the rear ones are installed in the middle shell of the oil unit. Thrust bearings emerge with each input and output channel, forming jointly the gear wheels the successive sections of the oil pump path. Distance between the shafts is necessary and sufficient to ensure maximum mutual engagement of the teeth of the gear wheels. In the method of operation of the pump-out oil, the oil is fed through the inlet in the lower housing of the oil unit and further along the inner channel under the minimum necessary excess pressure to the pump body followed by a volume displacement of the evacuated medium from the interdental depressions of the interacting gear wheels along the pump line, the oil at a higher pressure through the outlet channel in the middle shell of the oil unit is fed to the engine oil tank for purification and cooling. Displacement of the pumped medium from the interdental cavity of each of the interacting wheels is produced in the angular sector of rotation of the gear rims, determined by half the angle formed by the radii of the wheels from the intersection point of the relative cylindrical surfaces, describing the tops of the teeth of the gear rims to the output point of intersection of the conventional cylindrical surfaces in the course of the rotation of the gears, constituting the angular sector αd.o.n. In the area that is freed from the pumped medium depression, subsequent discharge βr.o.n. angular sector is equal to the displacement angle.
EFFECT: technical result achieved by a group of inventions is to increase the efficiency, resource and reliability of the pump oil pump.
17 cl, 7 dwg
Title |
Year |
Author |
Number |
METHOD OF OPERATION OF DISCHARGE PUMP OF GAS TURBINE ENGINE (GTE) OIL PUMP UNIT AND DISCHARGE PUMP OF GTE OIL PUMP UNIT OPERATING THEREWITH, GEAR WHEEL OF DISCHARGE PUMP OF GTE OIL PUMP UNIT, BLOCK OF THRUST BEARINGS OF DISCHARGE PUMP OF GTE OIL PUMP UNIT |
2017 |
- Marchukov Evgenij Yuvenalevich
- Polyakov Konstantin Sergeevich
- Fomin Vyacheslav Nikolaevich
|
RU2669634C1 |
METHOD OF OPERATING GAS-TURBINE ENGINE (GTE) OIL UNIT AND GTE OIL UNIT OPERATING THEREWITH (OPTIONS) |
2017 |
- Marchukov Evgenij Yuvenalevich
- Polyakov Konstantin Sergeevich
- Fomin Vyacheslav Nikolaevich
|
RU2669662C1 |
METHOD OF THE GAS-TURBINE ENGINE (GTE) OIL UNIT DISCHARGE PUMP OPERATION AND THE GTE OIL UNIT DISCHARGE PUMP OPERATING UNDER THIS METHOD, GTE OIL UNIT DISCHARGE PUMP IMPELLER |
2017 |
- Bibaeva Anna Viktorovna
- Fomin Vyacheslav Nikolaevich
|
RU2656523C1 |
METHOD OF WORKING THE OIL AGGREGATE OF THE TURBORETACTIVE ENGINE (TRE) AND THE OIL-AGRICULTURE TRE OPERATING THIS METHOD (OPTIONS) |
2017 |
- Bibaeva Anna Viktorovna
- Fomin Vyacheslav Nikolaevich
|
RU2656479C1 |
THRUST BEARING BLOCK FOR DISCHARGE PUMP OF GAS TURBINE ENGINE (GTE) OIL PUMP UNIT (VARIANTS), THRUST BEARING OF DRIVING WHEEL FOR DISCHARGE PUMP OF OIL PUMP UNIT, THRUST BEARING OF DRIVEN WHEEL FOR DISCHARGE PUMP OF OIL PUMP UNIT |
2017 |
- Marchukov Evgenij Yuvenalevich
- Fomin Vyacheslav Nikolaevich
- Shishkova Olga Vladimirovna
|
RU2669453C1 |
METHOD OF OPERATION OF THE OIL UNIT DISPLACEMENT PUMP OF THE TURBOJET ENGINE, DISPLACEMENT PUMP AND ITS IMPELLER |
2017 |
- Bibaeva Anna Viktorovna
- Fomin Vyacheslav Nikolaevich
|
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PROPULSION UNIT BOX (PUB) OF TURBOJET ENGINE (TJE), PUB BODY, MAIN BEVEL GEAR (MBG) OF PUB, DRIVING WHEEL OF PUB MBG, DRIVEN WHEEL OF PUB MBG, PUB INTAKE SHAFT |
2016 |
- Marchukov Evgenij Yuvenalevich
- Amanov Ruslan Ramilevich
- Bibaeva Anna Viktorovna
- Polyakov Konstantin Sergeevich
- Kuznetsov Igor Sergeevich
|
RU2635125C1 |
OPERATION METHOD FOR PROPULSION MOTOR GEARBOX (PMG) OF TWIN-SHAFT DOUBLE-FLOW TURBOJET ENGINE (TJE); OPERATION METHOD OF TJE PMG PLUNGER PUMP AND PLUNGER PUMP IMPLEMENTING THIS METHOD; OPERATION METHOD OF ENGINE TJE PMG CENTRIFUGAL PUMP AND ENGINE CENTRIFUGAL PUMP IMPLEMENTING THIS METHOD; OPERATION METHOD OF TJE PMG OIL PUMP BLOCK AND OIL PUMP BLOCK, IMPLEMENTING THIS METHOD |
2016 |
- Marchukov Evgenij Yuvenalevich
- Semenov Vadim Georgievich
- Simonov Sergej Anatolevich
- Polyakov Konstantin Sergeevich
- Bibaeva Anna Viktorovna
- Selivanov Nikolaj Pavlovich
|
RU2630928C1 |
TORQUE TRANSMITTING MECHANISM OF TURBOJET ENGINE UNITS, CENTRAL BEVEL GEAR OF TURBOJET ENGINE, MAIN CONICAL GEAR PAIR OF TURBOJET ENGINE CENTRAL BEVEL GEAR, BODY OF TURBOJET ENGINE CENTRAL BEVEL GEAR, DRIVE GEAR OF CENTRAL BEVEL GEAR, DRIVEN GEAR OF CENTRAL BEVEL GEAR, TURBOJET ENGINE CENTRAL BEVEL GEAR |
2016 |
- Marchukov Evgenij Yuvenalevich
- Bibaeva Anna Viktorovna
- Demina Lyubov Ivanovna
- Erichev Dmitrij Yurevich
- Polyakov Konstantin Sergeevich
- Sembieva Roza Idiyatullovna
- Semenov Vadim Georgievich
- Simonov Sergej Anatolevich
- Selivanov Nikolaj Pavlovich
|
RU2636626C1 |
PROPULSION UNITS CASE (PUC) OF TURBOJET ENGINE, PUC ASSEMBLY OF TURBOJET ENGINE (VERSIONS) |
2016 |
- Marchukov Evgenij Yuvenalevich
- Bibaeva Anna Viktorovna
- Sembieva Roza Idiyatullovna
- Simonov Sergej Anatolevich
- Selivanov Nikolaj Pavlovich
|
RU2635227C1 |