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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METHOD OF DETERMINATION OF SERVICE LIFE OF HELICOPTER MAIN ROTOR BLADES WITH HOLLOW METAL SPAR AND SPAR BREAK ALARM SYSTEM AND METHOD OF CONTROL OF FLIGHT OF HELICOPTER WITH SUCH BLADES | 1998 |
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METHOD OF RAPID SERVICE LIFE TESTS FO PARTS OF GAS TURBINES | 0 |
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METHOD OF RECONDITIONING COMPONENTS FROM HIGH-STRENGTH STEELS | 0 |
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HELICOPTER OPERATION | 2013 |
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METHOD OF DETERMINING CONSUMPTION OF RESOURCE AND LOAD SPECTRUM OF BASIC ELEMENTS OF AIRFRAME OF AEROBATIC AIRCRAFT | 2011 |
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METHOD OF MONITORING LOADS AND ACCUMULATED FATIGUE DAMAGE IN OPERATING CONDITIONS OF AIRCRAFT | 2015 |
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METHOD OF OPERATING AIRCRAFT ENGINE BASED ON TECHNICAL STATE THEREOF | 2008 |
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METHOD OF OPERATING THE ENGINE | 2005 |
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Authors
Dates
1996-09-20—Published
1993-06-10—Filed