FIELD: engine devices and pumps.
SUBSTANCE: rotor eighth stage impeller of TJE HPC contains a disc and rotor blades, forming a blade ring. The disc includes a hub with a central hole, curtain, and rim. Each blade consists of a shank, airfoil with a profile, formed by concave pressure side and convex back, and a root shroud on both sides of the feather, forming a bushing surface of the flow part together with the disc rim. In this case, the chord of the lateral edges of wing in the blade root zone forms, with the axis of the rotor in projection, the angle of installation of the wing αk, increasing along the radial height of the wing with a gradient of wing twist, constituting Gwt=(170.2÷242.9) [deg/m]. The wing blade is designed with the axial twist, variable relative to the rotor axis, that increases radially receding from the rotor axis. The exterior surface of disc rim has the radius which increases in the axial section of HPC towards the working medium flow. The radius RD Disk from the rotor axis of the HPC to the upper surface of the rim in the mean radial plane of the web is (0.74÷0.96) of the radius RP/c , the peripheral contour of the flowing part, and with the ratio of the radius RD to medium height Hav of the profile of the blade RD/ HWed=(8.3÷12.4). The rim of the disk is provided with annular flanges for releasably connecting to the rim flanges of the rims of the seventh and ninth stages of the rotor of the HPC and combining it into the bag with the discs and with the disk of the labyrinth by means of coupling elements.
EFFECT: increasing the efficiency and increasing gas dynamic stability on all operating modes of the compressor when the service life of the rotor of the sixth stage of high-pressure compressor rotor increases without increasing the material consumption.
24 cl, 9 dwg
Title |
Year |
Author |
Number |
ROTOR SIXTH STAGE IMPELLER OF HIGH-PRESSURE COMPRESSOR (HPC) OF TURBOJET ENGINE (VERSIONS), HPC ROTOR IMPELLER DISC, HPC ROTOR IMPELLER BLADE, HPC ROTOR IMPELLER BLADE RING |
2016 |
- Marchukov Evgenij Yuvenalevich
- Uzbekov Andrej Valerevich
- Simonov Sergej Anatolevich
- Shishkova Olga Vladimirovna
- Selivanov Nikolaj Pavlovich
|
RU2630922C1 |
IMPELLER WHEEL OF SEVENTH STAGE OF HIGH PRESSURE COMPRESSOR (HPC) ROTOR OF TURBOCHARGER ENGINE (VERSIONS), HPC ROTOR IMPELLER WHEEL DISC, HPC ROTOR IMPELLER WHEEL BLADE, HPC ROTOR IMPELLER WHEEL BLADE RING |
2016 |
- Marchukov Evgenij Yuvenalevich
- Uzbekov Andrej Valerevich
- Simonov Sergej Anatolevich
- Shishkova Olga Vladimirovna
|
RU2630923C1 |
NINTH STAGE IMPELLER WHEEL OF HIGH PRESSURE COMPRESSOR (HPC) ROTOR OF TURBOCHARGER ENGINE, HPC ROTOR IMPELLER WHEEL DISC, HPC ROTOR IMPELLER WHEEL BLADE, HPC ROTOR IMPELLER WHEEL BLADE RING |
2016 |
- Marchukov Evgenij Yuvenalevich
- Uzbekov Andrej Valerevich
- Shishkova Olga Vladimirovna
- Selivanov Nikolaj Pavlovich
|
RU2630925C1 |
ROTOR FORTH STAGE IMPELLER OF HIGH-PRESSURE COMPRESSOR (HPC) OF TURBOJET ENGINE (VERSIONS), HPC ROTOR IMPELLER DISC, HPC ROTOR IMPELLER BLADE, HPC ROTOR IMPELLER BLADE RING |
2016 |
- Marchukov Evgenij Yuvenalevich
- Erichev Dmitrij Yurevich
- Polyakov Konstantin Sergeevich
- Syroezhkin Oleg Vasilevich
- Selivanov Nikolaj Pavlovich
|
RU2630919C1 |
FIFTH STAGE IMPELLER WHEEL OF HIGH PRESSURE COMPRESSOR (HPC) ROTOR OF TURBOCHARGER ENGINE (VERSIONS), HPC ROTOR IMPELLER WHEEL DISC, HPC ROTOR IMPELLER WHEEL BLADE, HPC ROTOR IMPELLER WHEEL BLADE RING |
2016 |
- Marchukov Evgenij Yuvenalevich
- Erichev Dmitrij Yurevich
- Simonov Sergej Anatolevich
- Yakshina Regina Yurevna
|
RU2630920C1 |
IMPELLER WHEEL OF THIRD STAGE OF HIGH PRESSURE COMPRESSOR (HPC) ROTOR OF TURBOCHARGER ENGINE (VARIANTS), HPC ROTOR IMPELLER WHEEL DISC, HPC ROTOR IMPELLER WHEEL BLADE, HPC ROTOR IMPELLER WHEEL BLADE RING |
2016 |
- Erichev Dmitrij Yurevich
- Polyakov Konstantin Sergeevich
- Simonov Sergej Anatolevich
- Syroezhkin Oleg Vasilevich
- Selivanov Nikolaj Pavlovich
|
RU2630921C1 |
SECOND STAGE IMPELLER WHEEL OF HIGH PRESSURE COMPRESSOR (HPC) ROTOR OF TURBOCHARGER ENGINE (VARIANTS), HPC ROTOR IMPELLER WHEEL DISC, HPC ROTOR IMPELLER WHEEL BLADE, HPC ROTOR IMPELLER WHEEL BLADE RING |
2016 |
- Marchukov Evgenij Yuvenalevich
- Erichev Dmitrij Yurevich
- Polyakov Konstantin Sergeevich
- Simonov Sergej Anatolevich
- Syroezhkin Oleg Vasilevich
|
RU2636998C1 |
IMPELLER WHEEL OF FIRST STAGE OF HIGH PRESSURE COMPRESSOR (HPC) ROTOR OF TURBOCHARGER ENGINE (VARIANTS), HPC ROTOR IMPELLER WHEEL DISC, HPC ROTOR IMPELLER WHEEL BLADE, HPC ROTOR IMPELLER WHEEL BLADE RING |
2016 |
- Marchukov Evgenij Yuvenalevich
- Erichev Dmitrij Yurevich
- Polyakov Konstantin Sergeevich
- Syroezhkin Oleg Vasilevich
- Selivanov Nikolaj Pavlovich
|
RU2630918C1 |
ROTOR IMPELLER OF LP COMPRESSOR OF JET TURBINE ENGINE (VERSIONS) |
2014 |
- Marchukov Evgenij Juvenal'Evich
- Simonov Sergej Anatol'Evich
- Erichev Dmitrij Jur'Evich
- Selivanov Nikolaj Pavlovich
|
RU2565091C1 |
TURBOJET LOW-PRESSURE COMPRESSOR ROTOR IMPELLER (VERSIONS) |
2014 |
- Marchukov Evgenij Juvenal'Evich
- Simonov Sergej Anatol'Evich
- Uzbekov Andrej Valer'Evich
- Kuznetsov Igor' Sergeevich
|
RU2565108C1 |