发明名称 Method and apparatus for detecting icing conditions for an aircraft
摘要 <p>A method for detecting icing conditions for an airborne aircraft operating within a zone defined using one or more aircraft-related parameter and one or more environment parameter includes: (a) In no particular order: (1) measuring the aircraft-related parameter(s) to obtain aircraft-related parametric value(s); and (2) measuring the environment-related parameter(s) to obtain environment-related parametric value(s). (b) Employing the aircraft-related parametric value(s) and the environment-related parametric value(s) to determine whether the aircraft is operating within the zone. (c) If the aircraft is operating within the zone, observing elapsed time during which the aircraft is operating within the zone. (d) If the aircraft has operated within the zone for a predetermined elapsed time-in-zone, displaying an alert message for a user to indicate a likelihood of presence of icing conditions. </p>
申请公布号 EP2058228(A3) 申请公布日期 2012.07.04
申请号 EP20080253661 申请日期 2008.11.07
申请人 THE BOEING COMPANY 发明人 MA, ART L.;MACKIN, STEVEN G.;YANNUCCI, EMILY J.
分类号 B64D15/20;B64D15/22 主分类号 B64D15/20
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