FIELD: motors and pumps.
SUBSTANCE: group of inventions belongs to the field of aircraft engine building. PUB operation at the engine start includes three stages. At the engine start-up first stage, the starting torque from the starter to the PUB is transmitted through the start-up gearbox and the most part is directed to the HPH shaft through the multi-stage gearbox. Other part is divided into shared starting torques and transferred to the PUB units through the branched network of gearboxes. At the second stage, the PUB units receive the torque from the starter and, simultaneously with the increase in the engine's share, receive the rotational energy from the HPH shaft. After the starter disconnection, the engine startup third stage is performed before the HPH shaft reaches the low-speed rotations, in which the torque is fed to the units in the PUB only from the HPH shaft through the operational multi-stage gearbox, which is equipped with the PUB input shaft main distributor wheel. PUB afterburner pump includes pumping unit, impeller, start-up and minimum afterburner holding valve, in the engine startup mode shutting off the afterburning fuel from the OP to the AP starting unit, and to the fuel bypass valve at the unit outlet. AP also includes the main afterburning fuel input valve from the DCP into the AP pumping unit impeller cavity, the afterburning fuel outlet from the AP, and the two-stage ejector. Impeller receives the rotation energy in three stages. At the first stage, the starting torque is supplied to the pumping unit drive shaft from the starter via the start gearbox. At the second stage, the AP impeller receives the rotation energy simultaneously through the starting gearbox from the starter, with redistribution and increase in the energy contribution created by the speed gaining HPH shaft. At the third stage, the AP pumping unit receives the rotational energy from the engine's HPH, gaining speed until stable idle speed, with the AP bringing into the full readiness state to switch the engine afterburner on.
EFFECT: invention allows to increase the efficiency by 2 % and more than double engine life.
16 cl, 4 dwg
Title |
Year |
Author |
Number |
OPERATION METHOD FOR PROPULSION MOTOR GEARBOX (PMG) OF TWIN-SHAFT DOUBLE-FLOW TURBOJET ENGINE (TJE) AND PMG, IMPLEMENTING THIS METHOD; OPERATION METHOD FOR TJE PMG REGULATOR PUMP AND REGULATOR PUMP, IMPLEMENTING THIS METHOD, OPERATION METHOD FOR TJE PMG THRUST AUGMENTOR PUMP AND THRUST AUGMENTOR PUMP, IMPLEMENTING THIS METHOD; OPERATION METHOD FOR TJE PMG CENTRIFUGAL BREATHER AND CENTRIFUGAL BREATHER, IMPLEMENTING THIS METHODD |
2016 |
- Marchukov Evgenij Yuvenalevich
- Bibaeva Anna Viktorovna
- Semenov Vadim Georgievich
- Simonov Sergej Anatolevich
- Selivanov Nikolaj Pavlovich
- Shishkova Olga Vladimirovna
|
RU2630927C1 |
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 |
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 |
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 |
TURBO JET ENGINE (TJE) AFTERBURNER SYSTEM OPERATION METHOD AND THE AFTERBURNER SYSTEM OPERATING BY THIS METHOD, AFTERBURNER PUMP OPERATION METHOD AND THE AFTERBURNER PUMP OPERATING BY THIS METHOD, TJE OPERATION METHOD AND THE TJE OPERATING BY THIS METHOD |
2017 |
- Balukov Evgenij Vitalevich
- Kondratov Aleksandr Anatolevich
- Sladkov Mikhail Kupriyanovich
|
RU2656525C1 |
TURBO JET ENGINE (TJE) AFTERBURNER SYSTEM OPERATION METHOD AND OPERATING BY THIS METHOD AFTERBURNER SYSTEM (OPTIONS), TJE OPERATION METHOD AND TJE OPERATING BY THIS METHOD |
2017 |
- Balukov Evgenij Vitalevich
- Kondratov Aleksandr Anatolevich
- Sladkov Mikhail Kupriyanovich
|
RU2666835C1 |
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 |
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 |
SINGLE MECHANISM FOR TRANSFER OF THE TORQUE TO THE UNITS OF THE GAS TURBINE ENGINE (OPTIONS) |
2016 |
- Marchukov Evgenij Yuvenalevich
- Bibaeva Anna Viktorovna
- Demina Lyubov Ivanovna
- Kuprik Viktor Viktorovich
- Sembieva Roza Idiyatullovna
- Simonov Sergej Anatolevich
- Turkov Aleksandr Borisovich
- Shishkova Olga Vladimirovna
- Selivanov Nikolaj Pavlovich
|
RU2642955C1 |
UNIFIED MECHANISM OF TRANSFER OF TORQUE TO GAZOTURBINE ENGINE AGGREGATES (VERSIONS) |
2016 |
- Marchukov Evgenij Yuvenalevich
- Bibaeva Anna Viktorovna
- Demina Lyubov Ivanovna
- Kuprik Viktor Viktorovich
- Sembieva Roza Idiyatullovna
- Simonov Sergej Anatolevich
- Turkov Aleksandr Borisovich
- Polyakov Konstantin Sergeevich
- Selivanov Nikolaj Pavlovich
|
RU2644497C1 |