DEVICE FOR AXIAL COMPRESSOR AERODYNAMIC NOISE REDUCTION AND METHOD OF ITS IMPLEMENTATION Russian patent published in 2018 - IPC F04D27/02 F04D29/66 F04D29/54 

Abstract RU 2650241 C2

FIELD: turbine construction.

SUBSTANCE: device for reducing the aerodynamic noise of the axial compressor comprises an impeller of the first stage, and an annular electromagnet of the spline type is mounted on the inner surface of the shell of the axial compressor in the radial clearance zone. In the method for reducing the aerodynamic noise of an axial compressor, the electronic unit controlled by the regulator, into which the electric signal of the recording microphone arrives, after comparing with the reference, forms an electromagnetic field in the frequency range of 109 to 1013 Hz, tuning it to the fluid characteristics.

EFFECT: invention may be used in the input stages of axial compressors of turbomachines.

2 cl, 2 dwg

Similar patents RU2650241C2

Title Year Author Number
PERIPHERAL DEVICE FOR REDUCING HEAT CARRIER LEAKS 2016
  • Drokonov Aleksej Mikhajlovich
  • Lakhter Pavel Olegovich
RU2645100C1
DEVICE FOR AERODYNAMIC SEALING OF CLEARANCE BETWEEN BUTT ENDS OF AXIAL-FLOW COMPRESSOR ROTOR BLADES AND TURBINE SHELL 2004
  • Gavrikov A.I.
  • Kubyshkin N.V.
  • Kirievskij Ju.E.
RU2261372C1
MUFFLER 2004
  • Shipov Rollan Alekseevich
  • Khaletskij Jurij Danilovich
  • Povarkov Vjacheslav Ivanovich
RU2282042C1
METHOD FOR MEASURING ACOUSTIC PULSATIONS OF A GAS STREAM 2018
  • Siner Aleksandr Aleksandrovich
  • Lebiga Vadim Aksentevich
  • Sazhenkov Aleksej Nikolaevich
  • Zinovev Vitalij Nikolaevich
  • Pak Aleksej Yurevich
RU2697918C1
COMPRESSOR FAN STAGE (VERSIONS) 2005
  • Ivanov Oleg Ivanovich
  • Mileshin Viktor Ivanovich
RU2294461C1
AIRCRAFT TURBOFAN ENGINE 2003
  • Inozemtsev A.A.
  • Guzachev E.T.
  • Chursin V.A.
  • Leont'Ev A.S.
  • Klimov V.N.
RU2261999C2
TURBOMACHINE OVERROTOR DEVICE 2001
  • Inozemtsev A.A.
  • Guzachev E.T.
  • Klimov V.N.
  • Kirievskij Ju.E.
RU2199680C2
STRUCTURAL OR NON-STRUCTURAL CONNECTING SUPPORT OF COMPRESSOR CRANKCASE OF JET TURBINE ENGINE; INTERMEDIATE CRANKCASE OF JET TURBINE ENGINE, AND JET TURBINE ENGINE 2008
  • Zhjulliar Zhak
  • Molinari Oliv'E
  • Morel' Patrik
  • Riu Zhorzh
RU2472042C2
GAS TURBINE ENGINE WITH EXHAUST GAS GUIDE CONE WITH NOISE KILLER 2010
  • Buti Ehrik Zhan-Lui
  • Rego P'Er-Ljuk
  • Vallon Antuan
RU2546140C2
OSCILLATOR OF ACOUSTIC VIBRATIONS 1982
  • Abrukov Sergej Andreevvich
  • Afanas'Ev Vladimir Vasil'Evich
  • Gafurov Rukhanil Abdulkadyrovich
  • Kidin Nikolaj Ivanovich
  • Librovich Vadim Bronislavovich
  • Medvedev Nikolaj Antonovich
SU1839970A1

RU 2 650 241 C2

Authors

Drokonov Aleksej Mikhajlovich

Lakhter Pavel Olegovich

Dates

2018-04-11Published

2016-09-28Filed