METHOD FOR CONDUCTING STAND-ALONE TESTS ON MIXED FLOW AFTERBURNERS OF BYPASS TURBOFAN ENGINES Russian patent published in 2011 - IPC G01M15/14 

Abstract RU 2418281 C1

FIELD: physics.

SUBSTANCE: when conducting stand-alone tests in an afterburner, the value of total pressure of streams in air ducts of internal and external loops, on the section of the mixture, at the outlet of the diffuser and in front of the nozzle of the afterburner is measured. Air at the same low temperature is fed to the input of the air ducts of the internal and external loops. Further, by changing the area of the nozzle, a mode for critical flow of the stream from the nozzle is achieved. The value of total pressure of the stream at the inlet and outlet of the analysed section of the flow channel (mixer, diffuser, flame stabilisers) and the chamber as a whole is measured. The inlet irregularity characteristic is the ratio of total pressure of the streams in the loops. Conversion of results on looses to real conditions of operation of the engine is carried out using given relationships.

EFFECT: shorter time and low cost of gas-dynamic actual and model tests on afterburners of bypass turbofan engines and providing a reliable method for accounting for the effect of input temperature irregularity of streams in loops of the afterburner on hydraulic looses in its elements.

3 cl, 2 dwg

Similar patents RU2418281C1

Title Year Author Number
TURBO JET ENGINE (TJE) AFTERBURNER SYSTEM OPERATION METHOD AND THE AFTERBURNER SYSTEM OPERATING BY THIS METHOD, AFTERBURNER PUMP OPERATION METHOD AND THE AFTERBURNER PUMP OPERATING BY THIS METHOD, TJE OPERATION METHOD AND THE TJE OPERATING BY THIS METHOD 2017
  • Balukov Evgenij Vitalevich
  • Kondratov Aleksandr Anatolevich
  • Sladkov Mikhail Kupriyanovich
RU2656525C1
METHOD OF AVIATION BYPASS TURBOJET ENGINE WITH FLOWS MIXING IN-FLIGHT DIAGNOSTICS 2016
  • Ezrokhi Yurij Aleksandrovich
  • Khoreva Elena Aleksandrovna
  • Kizeev Ilya Sergeevich
RU2649715C1
CONTROL METHOD OF TURBOJET TWO-CIRCUIT ENGINE 2018
  • Ezrokhi Yurij Aleksandrovich
  • Kizeev Ilya Sergeevich
  • Khoreva Elena Aleksandrovna
RU2692189C1
TURBO JET ENGINE (TJE) AFTERBURNER SYSTEM OPERATION METHOD AND OPERATING BY THIS METHOD AFTERBURNER SYSTEM (OPTIONS), TJE OPERATION METHOD AND TJE OPERATING BY THIS METHOD 2017
  • Balukov Evgenij Vitalevich
  • Kondratov Aleksandr Anatolevich
  • Sladkov Mikhail Kupriyanovich
RU2666835C1
FUEL FEED UNIT TO THE BYPASS TURBOJET ENGINE AFTERBURNER 2015
  • Burdachev Dmitrij Aleksandrovich
  • Losev Aleksandr Ivanovich
RU2614268C1
METHOD OF DETERMINING THRUST IN FLIGHT OF BYPASS TURBOJET ENGINE WITH MIXING OF FLOWS 2015
  • Ezrokhi Yurij Aleksandrovich
  • Kizeev Ilya Sergeevich
  • Pudovkin Ivan Yurevich
RU2596413C1
DOUBLE-FLOW TURBOJET ENGINE AFTERBURNER 2002
  • Andreev A.V.
  • Kolesnichenko V.G.
RU2247852C2
JET TURBINE ENGINE 2011
  • Dolgomirov Boris Alekseevich
  • Lazarev Sergej Viktorovich
  • Sladkov Mikhail Kuprijanovich
RU2480604C1
AFTERBURNER COMBUSTION CHAMBER OF A DUAL-CIRCUIT TURBOJET ENGINE AND METHOD FOR ITS OPERATION 2021
  • Varsegov Vladislav Lvovich
  • Marchukov Evgenij Yuvenalevich
  • Mingazov Bilal Galavtdinovich
  • Mukhin Andrej Nikolaevich
  • Sychenkov Vitalij Alekseevich
RU2784569C1
METHOD OF TURBOJET BATCH MANUFACTURING AND TURBOJET MANUFACTURED ACCORDING TO THIS METHOD 2013
  • Artjukhov Aleksandr Viktorovich
  • Erichev Dmitrij Jur'Evich
  • Kondrashov Igor' Aleksandrovich
  • Kuprik Viktor Viktorovich
  • Manapov Irik Usmanovich
  • Marchukov Evgenij Juvenal'Evich
  • Poljakov Konstantin Sergeevich
  • Simonov Sergej Anatol'Evich
  • Selivanov Nikolaj Pavlovich
  • Fedorov Sergej Andreevich
RU2544410C1

RU 2 418 281 C1

Authors

Medvedev Vladimir Vladimirovich

Dates

2011-05-10Published

2009-10-23Filed