CRITICAL PITCH ANGLE INDICATOR Russian patent published in 1996 - IPC

Abstract RU 2057293 C1

FIELD: aeronautical engineering. SUBSTANCE: critical pitch angle indicator has present pitch-angle pick-off 1, two comparison units 2 and 5, critical pitch angle setter 3, altitude sensor 6, AND gate 7, indicator unit 8. 1-2-7-8, 3-2, 4-5-7, 6-5. EFFECT: enhanced reliability. 1 dwg

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RU 2 057 293 C1

Authors

Krylov S.S.

Serov A.A.

Sipovskij V.N.

Dates

1996-03-27—Published

1992-06-30—Filed