METHOD OF DETERMINING PERFORMANCE OF COMPRESSOR OF GAS TURBINE ENGINE Russian patent published in 1997 - IPC

Abstract RU 2087749 C1

FIELD: gas turbine engineering. SUBSTANCE: engine is throttled by varying the area of its inlet and outlet devices and supplying fuel to the combustion engine simultaneously. EFFECT: simplified method. 2 dwg

Similar patents RU2087749C1

Title Year Author Number
METHOD OF GAS TURBINE ENGINE COMPRESSOR PARAMETRIC DIAGNOSTICS 2010
  • Dobrjanskij Georgij Viktorovich
  • Mel'Nikova Nina Sergeevna
RU2446386C1
METHOD FOR AIRCRAFT ENGINE WITH FREE TURBINE RUN-TIME DIAGNOSTICS 0
  • Denisyuk Petr Ignatevich
  • Korolev Petr Vasilevich
SU1811600A3
COMBINED FORCE INSTALLATION OF AIRCRAFT 0
  • Alabin Mikhail Aleksandrovich
  • Alabin Yurij Mikhajlovich
SU1767204A1
METHOD OF DETERMINING EMISSION CHARACTERISTICS OF FUELS 0
  • Svinukhov Vladimir Petrovich
SU1357844A1
METHOD DETERMINING DURATION OF GROWTH DELAY OF FATIGUE CRACK AFTER OVERLOADING 1995
  • Shanjavskij A.A.
  • Orlov E.F.
RU2087897C1
DEVICE YOR MEASURING GAS TURBINE ENGINE THRUST 0
  • Alekseev Lev Petrovich
  • Yampolskij Vadim Iosifovich
  • Blokhin Sergej Valentinovich
SU917011A1
METHOD DETERMINING PARAMETERS OF GROWTH OF FATIGUE CRACK IN MEMBER OF STRUCTURE 1995
  • Shanjavskij A.A.
  • Orlov E.F.
RU2087896C1
PROCEDURE FOR OPERATING GAS TURBINE INSTALLATION 2009
  • Inozemtsev Aleksandr Aleksandrovich
  • Polatidi Sofokl Kharlampovich
  • Khaliullin Vitalij Ferdinandovich
  • Voronkov Viktor Evgen'Evich
  • Sazhenkov Aleksej Nikolaevich
RU2406990C1
METHOD OF CONTROLLING GAS TURBINE ENGINE 2009
  • Mel'Nikova Nina Sergeevna
RU2409751C2
METHOD OF REPAIR OF GUIDE VANES ASSEMBLY OF GAS-TURBINE ENGINE COMPRESSOR 1996
  • Paderov A.N.
  • Khabibulin N.R.
  • Paderova L.V.
RU2109176C1

RU 2 087 749 C1

Authors

Metelkin M.B.

Dates

1997-08-20Published

1993-07-12Filed