<p>A weight-on-gear sensor for use on an aircraft with landing skids having a bracket and a displacement sensor attached to the bracket is disclosed. The bracket has a center member connecting a first end member to a second end member. The center member has a centerline and the end members extend from the centerline of the center member. Mounting members extend along the centerline of the center member to facilitate attachment of the bracket to a cross tube. The displacement sensor connects the first end member to the second end member. The displacement sensor is parallel to, and offset from, the centerline of the center member so that when a bending moment is applied to the center member the first displacement sensor is either elongated or shortened.</p>
申请公布号
WO2006022700(A1)
申请公布日期
2006.03.02
申请号
WO2004US25821
申请日期
2004.08.10
申请人
BELL HELICOPTER TEXTRON INC.;MAST, JAMES, GRANT;COVINGTON, CHARLES, ERIC;DARDEN, PAUL, EUGENE;MCKEOWN, WILLIAM, L.
发明人
MAST, JAMES, GRANT;COVINGTON, CHARLES, ERIC;DARDEN, PAUL, EUGENE;MCKEOWN, WILLIAM, L.