The Boeing Company

Gregory J Seehusen

Mark Steven Good

Michael E Renzelmann

Mark John Gardner

Michael R Finn

Alan D Marx

Christopher D Feet

Gary A Emch

Richard I Apfel

A method for detecting freewheeling skew failures in the wing flaps of an aircraft includes measuring the outputs of flap skew sensors when the aircraft is in flight (IF) and the flaps are extended to a selected position, and when the aircraft is next on the ground (OG) and the flaps are extended to the selected position. The respective differences between the IF and OG outputs of symmetrical pairs of the flap skew sensors are computed, and then the respective difference between the computed IF output difference and the computed OG output difference of each symmetrical pair of the sensors is computed. The computed IF and OG difference of each symmetrical pair of the sensors is then compared with each of predetermined maximum and minimum threshold value to determine whether a freewheeling skew failure exists in any of the flaps of the aircraft.

In-flight detection of wing flap free wheeling skew

Growing community of inventors

Seattle, WA, United States of America

Gregory J Seehusen