초록 ▼

A jig is provided for assembling various different wing skin panels, all having different airfoil profiles. The jig includes a frame that has a plurality of colinear attachment points. These points define a center line axis that is generic for any panel assembled on the jig. A set of headers is dist

A jig is provided for assembling various different wing skin panels, all having different airfoil profiles. The jig includes a frame that has a plurality of colinear attachment points. These points define a center line axis that is generic for any panel assembled on the jig. A set of headers is distributed along the attachment points, such set being replaceable by another for a different panel. The headers have edge recesses in which are placed the panels\stringers. Both stringers and headers are covered by a skin sheet which is held in place by webbings that are pulled and tightened against the skin. The webbings hold the skin against the stringers while the stringers, skin, and headers are moved to a fastening location where the skin is riveted or otherwise fastened to the stringers.

대표청구항 ▼

A method of using a single assembly jig for manufacturing wing skin panel sections consisting of a plurality of elongated stringers covered by a sheet of material, said method comprising: defining a fixed centerline on said assembly jig, wherein said centerline is a common centerline for any panel s

A method of using a single assembly jig for manufacturing wing skin panel sections consisting of a plurality of elongated stringers covered by a sheet of material, said method comprising: defining a fixed centerline on said assembly jig, wherein said centerline is a common centerline for any panel section to be manufactured; providing a plurality of sets of panel headers, each header of each set having a panel-forming edge curved to have the shape of at least a portion of a certain airfoil profile, said edge including a plurality of stringer registration recesses, each recess being shaped to receive a portion of a stringer, wherein the panel-forming edges of the headers in each respective set cooperatively define the airfoil profile of a separate skin panel section that is dedicated for use in connection with a certain wing; providing a plurality of fixed header attachment points substantially along said centerline; selecting a particular header set; followed by connecting each header in said selected set to said fixed header attachment points, in a manner so that said panel-forming edges of said selected set define the curvature of a particular skin panel section; followed by placing stringers across said selected set of headers, in a manner so that said stringers are received in said stringer registration recesses of said headers; followed by placing a skin sheet over said panel-forming edges of said selected set and said stringers; followed by placing webbing straps across the outer surface of said skin sheet, one webbing strap each being positioned adjacent a header in said selected set; followed by fastening each end of each webbing strap to its adjacent header, in a manner so that said webbing strap may be tightened across the outer surface of said skin sheet; followed by tightening said webbing straps, thereby forcing and holding said skin sheet against said stringers and said panel-forming edges of said selected set of headers; followed by detaching said selected set of headers from said fixed header attachment points; and moving said selected set of headers, with said stringers and said webbing-held skin sheet attached thereto, to an assembly location for fastening said skin sheet to said stringers.