FIELD: machine engineering.
SUBSTANCE: impeller wheel of the second stage of the TRE HPC rotor shaft contains a disc and blades that form a blade ring. The disc includes a hub with a central hole, a body and a rim. Each blade contains a shank, a blade root with a profile, formed by a concave trough and a convex back, and a root shelf on both sides of the blade root, forming, together with the rim of the disc, a bushing surface of the flowing part. In this case, the chord of side edges of the body in the root zone of the blade creates with the rotor axis in projection a blade root installation angle αk, increasing along radial height of the root twist gradient, Gr.t=(150.2÷216.2) [degrees/m]. The blade root is featured with variable axial twist relative to the rotor axis, increasing with a radial distance from the axis of the rotor. The outer surface of the disc rim is made with a radius, increasing in the axial section of the HPC in the working fluid flow direction. Rd dis radius from the HPC rotor axis to the upper surface of the rim in the mean radial plane of the body is (0.59÷0.85) from the Rp.ch. radius of peripheral contour of the flowing part. The impeller wheel is made with a ratio of Rd disc radius to an average height Hav of blade root profile, constituting Rd/Hav=(2.3÷3.6). The disk blade is provided with annular beads for releasably connecting flanges adjacent to the web on both sides of the journal of the front support of the rotor of the HPC and the conical diaphragm of the disc of the fourth stage.
EFFECT: increase the efficiency and increase of gas dynamic stability resource in all operating modes of the compressor when service life of the second stage impeller wheel of the rotor high pressure compressor expands without increasing the material capacity.
22 cl, 9 dwg
Title |
Year |
Author |
Number |
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 |
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 |
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 |
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- Erichev Dmitrij Yurevich
- Simonov Sergej Anatolevich
- Yakshina Regina Yurevna
|
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2016 |
- Marchukov Evgenij Yuvenalevich
- Erichev Dmitrij Yurevich
- Polyakov Konstantin Sergeevich
- Syroezhkin Oleg Vasilevich
- Selivanov Nikolaj Pavlovich
|
RU2630919C1 |
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 |
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 |
ROTOR EIGHTH 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
- Syroezhkin Oleg Vasilevich
- Shishkova Olga Vladimirovna
- Selivanov Nikolaj Pavlovich
|
RU2630924C1 |
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 |
GAS TURBINE ENGINE LOW PRESSURE COMPRESSOR ROTOR IMPELLER (VERSIONS) |
2015 |
- Balaban Jurij Nikolaevich
- Erichev Dmitrij Jurevich
- Kuprik Viktor Viktorovich
- Marchukov Evgenij Juvenalevich
- Manapov Irik Usmanovich
- Shishkova Olga Vladimirovna
- Kuznetsov Igor Sergeevich
|
RU2603379C1 |
TURBOJET LOW-PRESSURE COMPRESSOR ROTOR FOURTH-STAGE IMPELLER |
2015 |
|
RU2612282C1 |