发明名称 AMPHIBIOUS SPORT AIRCRAFT WITH WING-FOLD
摘要 The design consists of features of the shape, configuration and ornamentation of a Amphibious Sport Aircraft With Wing-Fold as shown in the drawings.Drawings of the design are included.Figure 1 is a perspective view of the Amphibious Sport Aircraft With Wing-Fold, the wings shown in an unfolded position; Figure 2 is a front longitudinal view of the Amphibious Sport Aircraft With Wing-Fold, the wings shown in an unfolded position; Figure 3 is a rear longitudinal view of the Amphibious Sport Aircraft With Wing-Fold, the wings shown in an unfolded position; Figure 4 is a longitudinal view of the left side of the Amphibious Sport Aircraft With Wing-Fold, the wings shown in an unfolded position; Figure 5 is a longitudinal view of the right side of the Amphibious Sport Aircraft With Wing-Fold, the wings shown in an unfolded position; Figure 6 is a top plan view of the Amphibious Sport Aircraft With Wing-Fold, the wings shown in an unfolded position; Figure 7 is a bottom plan view of the Amphibious Sport Aircraft With Wing-Fold, the wings shown in an unfolded position; Figure 8 is a perspective view of the Amphibious Sport Aircraft With Wing-Fold, the wings shown in a folded position; Figure 9 is a front longitudinal view of the Amphibious Sport Aircraft With Wing-Fold, the wings shown in a folded position; Figure 10 is a rear longitudinal view of the Amphibious Sport Aircraft With Wing-Fold, the wings shown in a folded position; Figure 11 is a longitudinal view of the left side of the Amphibious Sport Aircraft With Wing-Fold, the wings shown in a folded position; Figure 12 is a longitudinal view of the right side of the Amphibious Sport Aircraft With Wing-Fold, the wings shown in a folded position; Figure 13 is a top plan view of the Amphibious Sport Aircraft With Wing-Fold, the wings shown in a folded position; Figure 14 is a bottom plan view of the Amphibious Sport Aircraft With Wing-Fold, the wings shown in a folded position;
申请公布号 CA128917(S) 申请公布日期 2010.05.17
申请号 CA20080128917F 申请日期 2008.12.10
申请人 ICON AIRCRAFT, INC. 发明人
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