发明名称 |
Amphibious aircraft |
摘要 |
Described are aircraft with at least one fuselage, a wing, and at least one float coupled to the wing. As examples, each float may include a step that is located forward of or at an intersection of a bottom surface and a line that extends from an aircraft aft-most center of gravity at an angle of less than ten degrees rearward from a vertical direction. As further examples, each float may include a forward portion located forward of the step, the forward portion including a ski surface that is planar in a left to right horizontal direction, and an aft portion that is located rearward of the step. |
申请公布号 |
US8807478(B2) |
申请公布日期 |
2014.08.19 |
申请号 |
US201213667874 |
申请日期 |
2012.11.02 |
申请人 |
Leader Industries, Inc. |
发明人 |
Meekins John A.;Husa William |
分类号 |
B64C25/54;B64C35/00 |
主分类号 |
B64C25/54 |
代理机构 |
Kilpatrick Townsend & Stockton LLP |
代理人 |
Kilpatrick Townsend & Stockton LLP |
主权项 |
1. An aircraft configured to take off and land on water, the aircraft including at least one fuselage and at least one wing connected to the fuselage, the aircraft including an aft-most center of gravity and at least one float, the float comprising:
a float body that includes a bottom surface; a bottom surface forward portion located on the float body bottom surface, the bottom surface forward portion including a ski surface that is planar in a left-to-right horizontal direction; a bottom surface rearward portion located on the float body bottom surface, the bottom surface rearward portion including a rudder; and a bottom surface step located on the float body bottom surface and interposed between the bottom surface forward portion and the bottom surface rearward portion, the step including a point that is located forward of or at an intersection of the bottom surface and a line that extends from the aircraft aft-most center of gravity at an angle of less than ten degrees rearward from a vertical direction. |
地址 |
Norfolk VA US |