초록 ▼

An energy absorbing stitched-composite structural element is provided having a glass thread stitched therethrough. The stitching pattern of the thread varies in density from a low-density portion at an initial impact portion of the panel to a high density portion at a final impact portion of the pan

An energy absorbing stitched-composite structural element is provided having a glass thread stitched therethrough. The stitching pattern of the thread varies in density from a low-density portion at an initial impact portion of the panel to a high density portion at a final impact portion of the panel. Preferably, the stitch pattern includes a plurality of rows laterally spaced apart relative to the height of the panel. The spacing between adjacent rows progressively decreases from the initial impact portion of the panel to the final impact portion of the panel. Alternatively, or in combination therewith, the number of stitches per row varies from the fewest number of stitches proximate the initial impact portion of the panel to the final impact portion of the panel. In a highly preferred embodiment of the present invention, the stitched composite panel is incorporated into the subfloor structure of an aircraft fuselage.

대표청구항 ▼

1. An aircraft comprising: a fuselage; a floor spaced apart from said fuselage; and an impact absorbing structure disposed between said fuselage and said floor, said impact absorbing structure including a plurality of vertically oriented composite panels, each of said panels having a thread sti

1. An aircraft comprising: a fuselage; a floor spaced apart from said fuselage; and an impact absorbing structure disposed between said fuselage and said floor, said impact absorbing structure including a plurality of vertically oriented composite panels, each of said panels having a thread stitched therethrough in a pattern varying in density from an initial impact portion of said panel to a final impact portion of said panel. 2. The aircraft of claim 1 wherein said pattern further comprises a low density pattern proximate said initial impact portion and a high density pattern proximate said final impact portion. 3. The aircraft of claim 2 wherein said low density pattern progressively transitions into said high density pattern. 4. The aircraft of claim 3 wherein said low density pattern and said high density pattern further comprise a plurality of rows of said thread stitched through said panels, said plurality of rows being spaced apart by progressively decreasing amounts from said initial impact portion to said final impact portion and including an increasing number of stitches per row from said initial impact portion to said final impact portion.