METHOD OF ESTIMATION OF TECHNICAL STATE OF FLYING VEHICLE RIGID CONTROL LINKAGE Russian patent published in 1997 - IPC

Abstract RU 2092387 C1

FIELD: technical diagnosis of rigid control linkage. SUBSTANCE: transverse oscillations are excited in rigid linkage of control system rigidly secured on one side by means of control surface. Actual frequency of natural flexural oscillations of this structural member is determined. Mismatch of standard and actual frequency is indicative of damage. EFFECT: enhanced reliability. 1 dwg

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RU 2 092 387 C1

Authors

Sharif Mokhammed Al'-Khejli[Ru]

Egorshev Anatolij Viktorovich[Ru]

Komarov Vladimir Aleksandrovich[Ua]

Arabi Mukhamed Jusif[Ua]

Dates

1997-10-10Published

1994-07-06Filed