FIELD: aircraft engineering.
SUBSTANCE: proposed method exploits device decreasing aircraft landing run including electropneumatic valve, pressure relay, inertial contactor that makes electropneumatic valve and pressure self-holding relay supply circuit on aircraft landing gear touchdown in landing. Self-holding relay ensures stable supply of electropneumatic valve after opening of said circuit by inertial contactor.
EFFECT: decreased landing run.
2 cl, 2 dwg
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