FIELD: transport.
SUBSTANCE: proposed support to be used in aircraft undercarriage comprises strut support and means including strain gages to measure shear strains and accelerometers to measure loads on said strut support. Strut support incorporates self-contained device to measure loads thereat. Said strut support houses data processing unit, memory unit and power supply built around galvanic cells to allow monitoring is fatigue stresses in operation. Note here that said data processing unit receives input signals from strain gages to store said data in memory. Accumulated data on strains are unloaded from memory in current maintenance.
EFFECT: high-quality monitoring of strains.
17 cl, 3 dwg
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