Abstract: A landing gear system for an aircraft comprising a pair of legs, each having a wheel at a distal end, a pivot point associated with each leg for allowing each leg to follow an arc-shaped path between a deployed position and a retracted position, one of the legs passing in front of the other while moving from the deployed position to the retracted position, and a linking assembly disposed between the legs for ensuring that the legs move from the deployed position to the retracted position in unison.
Type:
Grant
Filed:
June 14, 2001
Date of Patent:
October 15, 2002
Assignee:
Explorer Aircraft, Inc.
Inventors:
Graham Swannell, Geoffrey Danes, Kim White, Peter Brooks