FIELD: measuring equipment.
SUBSTANCE: technical state diagnosis is carried out at one and the same corrected frequency of a low-pressure rotor rotation, chosen from the operating range, based on current parameter values deviations from the initial ones, corrected to standard atmospheric conditions. Dependences are given, based on which the above-mentioned deviations are determined. At that, negative values of 
indicate engine air-gas path contamination or air leaks from the low-pressure compressor, and positive values of 
indicate a deterioration in the efficiency of the low-pressure compressor and/or high-pressure compressor and/or high-pressure turbine, and/or low-pressure turbine. Positive values of 
and negative value of 
indicate air suction from the compressor high-pressure path.
EFFECT: increased of accuracy and reliability in the diagnosis of the state of engine flowing part elements and determination of a specific defect and its location.
1 dwg, 2 tbl
| Title | Year | Author | Number |
|---|---|---|---|
| METHOD OF DETERMINING THRUST IN FLIGHT OF BYPASS TURBOJET ENGINE WITH MIXING OF FLOWS | 2015 |
|
RU2596413C1 |
| METHOD OF CONTROLLING CRITICAL SECTION AREA OF TWO-STAGE GAS TURBINE ENGINE JET NOZZLE | 2010 |
|
RU2443890C1 |
| METHOD OF GAS TURBINE ENGINE COMPRESSOR PARAMETRIC DIAGNOSTICS | 2010 |
|
RU2446386C1 |
| CONTROL METHOD OF AIR LEAKAGES AND FLOW FOR TURBINE COOLING IN DOUBLE-FLOW GAS TURBINE ENGINE | 2008 |
|
RU2389891C1 |
| METHOD FOR PROTECTING BYPASS TURBOJET ENGINE AGAINST STALL DURING OPERATION | 2015 |
|
RU2613758C2 |
| GAS TURBINE ENGINE | 2013 |
|
RU2556090C2 |
| ADJUSTMENT METHOD OF TEST GAS-TURBINE ENGINE | 2013 |
|
RU2544634C1 |
| METHOD OF AVIATION BYPASS TURBOJET ENGINE WITH FLOWS MIXING IN-FLIGHT DIAGNOSTICS | 2016 |
|
RU2649715C1 |
| GAS-TURBINE ENGINE | 2013 |
|
RU2545110C1 |
| METHOD TO CONTROL GAS TURBINE ENGINE | 2008 |
|
RU2379534C2 |
