METHOD FOR REDUCTION OF AIRCRAFT ENGINE VIBRATORY EFFECTS Russian patent published in 2016 - IPC B64D33/02 

Abstract RU 2574498 C2

FIELD: aircraft engineering.

SUBSTANCE: claimed process comprises the selection performed by calculation of the ratios between the engine inner and outer outline lengths within over 1.41 or under 0.9 for all possible operating conditions of the aircraft.

EFFECT: ruled out the engine thrust loss, longer life of the aircraft airframe.

3 dwg, 2 tbl

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RU 2 574 498 C2

Authors

Skorik Boris Prokhorovich

Dates

2016-02-10Published

2014-06-02Filed