DIFFUSER Russian patent published in 2017 - IPC F01D25/30 F04D29/44 

Abstract RU 2637421 C1

FIELD: machine engineering.

SUBSTANCE: diffuser comprises an external bypass 1 made conical, on which inner side there is a ribbing, the main ribs 2 and auxiliary ribs 3. The main ribs 2 are formed by wedge-shaped variable height increasing linearly from zero value in inlet edge area 4 located in the inlet section 5 of the diffuser to a value h1 in the area of the outlet edge 6 located in the outlet section 7 of the diffuser. The angular installation pitchβ1 between the main ribs 2 does not exceed 5°. The free edge 8 of the main ribs 2 is parallel to the longitudinal axis O of the diffuser. The auxiliary ribs 3 are installed in the middle between the main ribs 2. The angular installation stage β2 between the main rib 2 and the auxiliary rib 3 is equal to half of the angle installation pitch β1. The auxiliary ribs 3 are made with trapezoidal variable height. There are inlet edges 9 of the auxiliary ribs 3 located at distance L1 from the inlet section 5 of the diffuser is chosen to be equal to the half of the axial diffuser length L. The outlet edges 10 of the auxiliary ribs 3 are arranged in the outlet section 7 of the diffuser. The free edge 11 of the auxiliary ribs 3 is parallel to the longitudinal axis O of the diffuser. The height of the auxiliary ribs 3 is linearly increasing from the value h2 in the region of their input edge 9 to the value h3 in the area of their output edge 10. In this case, the value of h2 is selected equal to half the value of h1, and the values of h3 and h1 are equal and chosen as , where is the Reynolds number, where c1 - average velocity in the inlet section 5 of the diffuser, ν - coefficient of kinematic viscosity of the moving working medium.

EFFECT: improved reliability of the turbomachine elements by effectively stabilising the flow of wide-angle diffusers with opening angles of the running portion above 12 degrees due to prevention of tear-off zones formation which results in sharp increase of amplitudes of pressure pulsations.

4 dwg

Similar patents RU2637421C1

Title Year Author Number
DIFFUSER 2010
  • Zarjankin Arkadij Efimovich
  • Arianov Sergej Vladimirovich
  • Paramonov Andrej Neonovich
  • Noskov Viktor Vladimirovich
RU2469214C2
PRE-COMBUSTION DEVICE OF ANNULAR COMBUSTION CHAMBER OF GAS TURBINE ENGINE 2001
  • Goncharov V.G.
  • Lebedev V.A.
  • Marchukov E.Ju.
  • Fedorov S.A.
  • Chepkin V.M.
RU2210033C1
VOLTAGE CONVERTER CASE 1998
  • Vol'Skij S.I.
  • Chuev V.I.
  • Milovanov V.K.
RU2155427C1
TURBOMACHINE BLADE SYSTEM 2016
  • Zaryankin Arkadij Efimovich
  • Garanin Ivan Vladimirovich
  • Kindra Vladimir Olegovich
  • Khudyakova Valentina Pavlovna
  • Lvov Ilya Vladimirovich
RU2626285C1
CORRUGATED INSERT FOR PLATE HEAT EXCHANGER 2009
  • Dubrovskij Evgenij Vladimirovich
RU2450230C2
STEAM TURBINE LOW PRESSURE CYLINDER STAGE GUIDE VANE 2022
  • Tyukhtyaev Aleksej Mikhajlovich
  • Usachev Konstantin Mikhajlovich
  • Dolganov Aleksej Gennadevich
  • Ivanovskij Aleksandr Aleksandrovich
  • Vekshina Olga Valentinovna
  • Khlopkova Ulyana Olegovna
RU2789652C1
PRESSURE TRANSDUCER FOR FLOWMETER 1997
  • Bychkov Ju.M.
RU2157973C2
DEVICE FOR CONTACT-HEAT WELDING OF THERMOPLASTICS 2004
  • Bocharov V.I.
  • Valiakhmetov P.N.
  • Safonov V.G.
  • Rudoj V.I.
RU2253569C1
METHOD FOR COOLING OF NOZZLE ASSEMBLY OF A LOW-PRESSURE TURBINE (LPT) OF A GAS TURBINE ENGINE AND A LPT NOZZLE ASSEMBLY WHICH IS COOLED BY THIS METHOD, A METHOD FOR COOLING A BLADE OF LPT NOZZLE ASSEMBLY AND A NOZZLE ASSEMBLY BLADE, COOLED BY THIS METHOD 2018
  • Marchukov Evgenij Yuvenalevich
  • Kuprik Viktor Viktorovich
  • Andreev Viktor Andreevich
  • Komarov Mikhail Yurevich
  • Kononov Nikolaj Aleksandrovich
  • Krylov Nikolaj Vladimirovich
  • Selivanov Nikolaj Pavlovich
RU2691202C1
DEVICE FOR CLEANING STEAM OR GAS FROM FOREIGN IMPURITIES 2012
  • Khaimov Vjacheslav Arkad'Evich
  • Sudakov Aleksandr Veniaminovich
  • Gudkov Ehduard Il'Ich
  • Petukhov Lev Stepanovich
  • Voropaev Jurij Aleksandrovich
RU2506112C2

RU 2 637 421 C1

Authors

Zaryankin Arkadij Efimovich

Rogalev Andrej Nikolaevich

Grigorev Evgenij Yurevich

Akhmedzhanova Oksana Pavlovna

Dates

2017-12-04Published

2016-11-10Filed