FIELD: aeronautical engineering; helicopters. SUBSTANCE: method consists in recording the flying time of structural member, determination of duration of each mode of flight depending on level of loading structural member and estimation of total equivalent operating hours of structural member which is compared with specified service life. EFFECT: enhanced efficiency. 1 tbl
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|---|---|---|---|
| METHOD OF ESTIMATION OF TECHNICAL STATE OF HELICOPTER ROTOR SYSTEM FOR PROLONGATION OF ITS SERVICE LIFE | 2001 |
|
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| METHOD TO ESTIMATE AIRCRAFT GAS TURBINE ENGINE STATE | 2008 |
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| HELICOPTER OPERATION | 2013 |
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| METHOD OF OPERATING THE ENGINE | 2005 |
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SU1613924A1 |
| METHOD OF DETERMINING PERFORMANCE OF COMPRESSOR OF GAS TURBINE ENGINE | 1993 |
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| METHOD OF DETERMINATION IN FLIGHT OF BENDING STRESSES ON ROTOR SHAFT OF HELICOPTER WITH TORSIONAL ROTOR HEAD | 2016 |
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