FIELD: engines and pumps.
SUBSTANCE: invention relates to aircraft engines. This process comprises the steps that follow. First, multiple measurements of tank fuel level are performed during at least one flight of aircraft for preset engine working phases. Note here that every measurement is related with oil temperature and engine rpm. Selected are measurements that display oil level variation and are related with oil temperatures that approximate to reference temperature and with engine rpm approximating to reference rpm. Combined are (F40) measurements selected by phases of operation during at least one flight of aircraft and to compare (F60) combined measurements with reference data for identification (F70) of engine oil abnormal consumption.
EFFECT: higher validity of estimation.
13 cl, 4 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| AIRCRAFT AIR INTAKE ASSEMBLY | 2009 |
|
RU2470840C1 |
| AIRCRAFT EQUIPMENT MONITORING SYSTEM | 2017 |
|
RU2690026C1 |
| CONTROL METHOD OF THERMAL EMISSIONS GENERATED WITH AIRBORNE VEHICLE, COOLING DEVICE FOR AIRBORNE VEHICLE, WHICH ALLOWS USING ABOVE DESCRIBED METHOD | 2008 |
|
RU2478805C2 |
| METHOD AND SYSTEM FOR ADJUSTMENT OF CLEARANCE AT TURBINE ROTOR BLADE EDGES | 2011 |
|
RU2566510C2 |
| METHOD AND SYSTEM FOR DIAGNOSING HYBRID POWER PLANT OF LIGHT AIRCRAFT | 2023 |
|
RU2818394C1 |
| METHOD AND SYSTEM FOR DESCRIPTION AND ALLOWANCE FOR AIRCRAFT ENGINE WORKING PARAMETER THRESHOLD BUILDUP | 2008 |
|
RU2482999C2 |
| TURBOJET ENGINE CONTROL METHOD | 2020 |
|
RU2736403C1 |
| METHOD TO CONTROL OIL CONSUMPTION IN AIRCRAFT GAS TURBINE ENGINE | 2008 |
|
RU2386835C1 |
| SIMPLIFIED SHUTTLE MODULE FOR CARRIER ROCKET | 2011 |
|
RU2566597C2 |
| METHOD OF AIRCRAFT ENGINE MONITORING DURING OPERATION IN FLIGHT | 2016 |
|
RU2708905C2 |
