NOZZLE ASSEMBLY BLADE Russian patent published in 1998 - IPC

Abstract RU 2120037 C1

FIELD: axial-flow microturbines. SUBSTANCE: blade has widening-narrowing profile with trailing and leading edges defined by arc of circle, convex and concave sides defined by parabolic arc. Chord of blade profile is equal to 1.7-2.4 of its width. Ratio of maximum thickness of profile to chord ranges from 0.13 to 0.17. Distance between leading edge of profile and center of maximum thickness ranges from 0.05 to 0.1. EFFECT: increased torque at turbine output shaft in all modes of operation at subsonic, transonic and supersonic speeds. 2 dwg

Similar patents RU2120037C1

Title Year Author Number
PNEUMATIC GRINDING TOOL 1996
  • Kosmynin A.V.
  • Vinogradov V.S.
  • Moshkov V.Ju.
RU2113969C1
TURBINE WORKING BLADE 1992
  • Kosmynin A.V.
RU2053370C1
METHOD AND TURBINE FOR PRODUCING MECHANICAL ENERGY 2002
  • Vorob'Ev R.N.
  • Zelinskij A.M.
RU2200848C1
FREE-FLOW OPERATIONAL HYDRAULIC POWER ENGINEERING PLANT 1992
  • Novikov Ju.M.
RU2049929C1
TURBINE PRESSURE STAGE OF TURBODRILL 2002
  • Kurumov L.S.
  • Simonjants S.L.
  • Ioanesjan Ju.R.
RU2205934C1
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
HIGH-PRESSURE TURBINE (HPT) NOZZLE APPARATUS OF GAS TURBINE ENGINE (OPTIONS), NOZZLE CROWN OF HPT AND HPT NOZZLE APPARATUS BLADE 2018
  • Marchukov Evgenij Yuvenalevich
  • Kuprik Viktor Viktorovich
  • Andreev Viktor Andreevich
  • Komarov Mikhail Yurevich
  • Kononov Nikolaj Aleksandrovich
  • Krylov Nikolaj Vladimirovich
  • Ryabov Evgenij Konstantinovich
  • Zolotukhin Andrej Aleksandrovich
RU2683053C1
IMPELLER BLADE OF ROTOR OF COMPRESSOR OF LOW-PRESSURE GAS TURBINE (VERSIONS) 2014
  • Marchukov Evgenij Juvenalevich
  • Simonov Sergej Anatolevich
  • Erichev Dmitrij Jurevich
  • Kuprik Viktor Viktorovich
  • Manapov Irik Usmanovich
  • Uzbekov Andrej Valerevich
RU2581987C1
IMPELLER BLADE OF ROTOR OF COMPRESSOR OF LOW-PRESSURE GAS TURBINE (VERSIONS) 2014
  • Marchukov Evgenij Juvenalevich
  • Simonov Sergej Anatolevich
  • Erichev Dmitrij Jurevich
  • Kuprik Viktor Viktorovich
  • Kondrashov Igor Aleksandrovich
  • Uzbekov Andrej Valerevich
  • Kuznetsov Igor Sergeevich
RU2581981C1
IMPELLER BLADE OF ROTOR OF COMPRESSOR OF LOW-PRESSURE GAS TURBINE (VERSIONS) 2014
  • Marchukov Evgenij Juvenalevich
  • Simonov Sergej Anatolevich
  • Erichev Dmitrij Jurevich
  • Kuprik Viktor Viktorovich
  • Kondrashov Igor Aleksandrovich
  • Troshchenkova Marina Mikhajlovna
  • Selivanov Nikolaj Pavlovich
RU2581980C1

RU 2 120 037 C1

Authors

Kosmynin A.V.

Vinogradov V.S.

Dates

1998-10-10Published

1996-06-14Filed