Patent ID: 7992822
Filing Date: 2011-08-09
Classification: B64C,Y10T

Abstract:
1. A leading edge skin height difference adjusting structure comprising: a height difference adjusting member fixing a rear end of a leading edge skin to a spar of a main wing of an aircraft with the height difference adjusting member interposed therebetween, while adjusting a difference in height between a front end of a main body skin and the rear end of the leading edge skin when the main body skin and the leading edge skin are brought into abutment on each other and fixed on the spar with a fastener; wherein the height difference adjusting member is formed from a plate material into a shape including a shim portion and a resilient support portion which are opposed to each other, and is mounted on the spar so as to be resiliently retained relative to a flange of the spar between the shim portion and the resilient support portion; and wherein the leading edge skin is fixed to the flange by the fastener in a state wherein the shim portion is interposed between the leading edge skin and the flange.