A method and system for indicating a potential stall condition for an aircraft during flight. An alert lift coefficient is identified for the aircraft. The alert lift coefficient is adjusted in response to a number of changes in a current state of the aircraft. A set of thresholds is identified for use in generating an alert indicating that the aircraft has reached the potential stall condition using the alert lift coefficient.
申请公布号
US8653990(B2)
申请公布日期
2014.02.18
申请号
US201213526198
申请日期
2012.06.18
申请人
SMYTH, IV JOSEPH MICHAEL;LYMAN FRANK J.;THE BOEING COMPANY