METHOD OF CHECKING EFFICIENCY OF AIRCRAFT UNDERCARRIAGE NOSE WHEEL TURN CONTROL UNIT Russian patent published in 2012 - IPC G05B23/02 B64F5/00

Abstract RU 2469371 C2

FIELD: aircraft engineering.

SUBSTANCE: proposed method comprises connecting interface 14 of tester 12 to, at least, one input port of aircraft nose wheel control units 10. Said tester 12 incorporates nose wheel speed simulator to generate speed simulation signal. Nose wheel speed simulation signal is generated to represent definite simulated speed exceeding preset speed. Generated signal is transmitted to unit 10 via interface 14. Tester 12 is used to control simultaneously two separate units 10 to make one of them operate in instruction feed mode and another one in control mode. Output signal of said unit 10 in response to received speed simulation signal is controlled.

EFFECT: higher fault tolerance.

8 cl, 2 dwg

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RU 2 469 371 C2

Authors

Gom'Er Dan'El'

Morvan Rozhe

Dates

2012-12-10—Published

2007-11-29—Filed