Invention Grant
US09285007B2 Servicing monitoring system for mixed fluid-gas shock struts 有权
混合流体气体冲击支柱的维修监控系统

Servicing monitoring system for mixed fluid-gas shock struts
Abstract:
A method and system of monitoring condition of a shock strut senses gas temperature, gas pressure, and stroke of the strut during a landing event. Oil loss is determined based upon a deviation of a transient pressure coefficient derived from transient gas pressures at two different strokes from a nominal coefficient value. Gas loss is determined based upon a temperature adjusted transient gas pressure at a selected stroke and a nominal gas pressure value at the selected stroke.
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