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1. 发明授权

US07374133B2 Wing having a negative dihedron for towing a load 有权
标题翻译：翼具有负二面体以牵引负载
公开(公告)号：US07374133B2
公开(公告)日：2008-05-20
申请号：US11067842
申请日：2005-02-28
申请人： Dominique Legaignoux , Bruno Legaignoux
发明人： Dominique Legaignoux , Bruno Legaignoux
IPC分类号： B64D17/02
CPC分类号： B63B35/7979 , B64C31/06 , B64C2031/065
摘要： The wing (10) having a negative dihedron for towing a load comprises a flexible canopy (12) which is defined between two lateral ends (14A, 14B) which are connected to each other, at the front, by a leading edge (20) and, at the rear, by a trailing edge (22). The canopy (12) has, between those two lateral ends (14A, 14B), a propulsive central region (16) which is bordered at one side and the other by two control regions (18A, 18B). The wing comprises at least a member (30A, 30B) for suspending the load adjacent to each lateral end (14A, 14B) and auxiliary maintenance means (32) which are capable of flattening the propulsive central region (16) adjacent to the leading edge (20) during flight. The trailing edge (22) of the wing is generally concave.
摘要翻译：具有用于牵引负载的负二面体的机翼（10）包括柔性遮篷（12），其限定在两个横向端部（14A，14B）之间，两个侧端部（14A，14B）在前部通过前缘 20），并且在后部由后缘（22）。顶盖（12）在两个横向端部（14A，14B）之间具有在一侧边界且两个控制区域（18A，18B）相邻的推进中心区域（16）。所述机翼至少包括用于将所述负载悬挂在每个侧端（14A，14B）附近的负载和辅助维护装置（32）的至少一个构件（30A，30B），所述辅助维护装置能够使所述推进中心区域（16）相邻到飞行中的前缘（20）。机翼的后缘（22）通常是凹形的。

2. 发明授权

US07494093B2 Wing having a negative dihedron for towing a load 有权
标题翻译：翼具有负二面体以牵引负载
公开(公告)号：US07494093B2
公开(公告)日：2009-02-24
申请号：US11739936
申请日：2007-04-25
申请人： Dominique Legaignoux , Bruno Legaignoux
发明人： Dominique Legaignoux , Bruno Legaignoux
IPC分类号： B64D17/02
CPC分类号： B63B35/7979 , B64C31/06 , B64C2031/065
摘要： The wing (10) having a negative dihedron for towing a load comprises a flexible canopy (12) which is defined between two lateral ends (14A, 14B) which are connected to each other, at the front, by a leading edge and, at the rear, by a trailing. The wing (10) includes rear lines (40A, 40B) which are connected to the suspension members (30A, 30B) which are arranged at the lateral ends (14A, 14B) of the wing, and in that the auxiliary maintenance means of the propulsive central region (16) comprise at least a front line which is connected by one end to the propulsive central region adjacent to the leading edge and which is capable of being connected to the load at the other end. The front lines comprise an assembly of shroud lines (90A, 90B) which are applied to the propulsive central region (16) at locations which are distributed over the length of the leading edge, at least one sliding shroud line (90A, 90B) being engaged in a sliding manner in a guide (92A, 92B) which is fixedly joined to the leading edge, the end of the sliding shroud line (90A, 90B) being fixedly joined to a rear line (40A, 40B).
摘要翻译：具有用于牵引负载的负二面体的机翼（10）包括柔性罩（12），其限定在两个侧端（14A，14B）之间，两个侧端（14A，14B）在前部通过前缘彼此连接，并且在后方，尾随。机翼（10）包括连接到设置在机翼的侧端（14A，14B）处的悬挂构件（30A，30B）的后线（40A，40B），并且辅助维护装置推进中心区域（16）包括至少一条前端线，其一端连接到与前缘相邻的推进中心区域，并且能够在另一端连接到负载。前线包括在分配在前缘的长度上的位置处施加到推进中心区域（16）的护罩线（90A，90B）的组件，至少一个滑动护罩线（90A，90B）在与前缘固定接合的引导件（92A，92B）中滑动地滑动，滑动护罩线（90A，90B）的端部固定地连接到后线（40A，40B）。

3. 发明申请

US20070187553A1 Wing Having a Negative Dihedron for Towing a Load 有权
标题翻译：具有负二面体负载的翼
公开(公告)号：US20070187553A1
公开(公告)日：2007-08-16
申请号：US11739936
申请日：2007-04-25
申请人： Dominique Legaignoux , Bruno Legaignoux
发明人： Dominique Legaignoux , Bruno Legaignoux
IPC分类号： B64C31/06
CPC分类号： B63B35/7979 , B64C31/06 , B64C2031/065
摘要： The wing (10) having a negative dihedron for towing a load comprises a flexible canopy (12) which is defined between two lateral ends (14A, 14B) which are connected to each other, at the front, by a leading edge and, at the rear, by a trailing. The wing (10) includes rear lines (40A, 40B) which are connected to the suspension members (30A, 30B) which are arranged at the lateral ends (14A, 14B) of the wing, and in that the auxiliary maintenance means of the propulsive central region (16) comprise at least a front line which is connected by one end to the propulsive central region adjacent to the leading edge and which is capable of being connected to the load at the other end. The front lines comprise an assembly of shroud lines (90A, 90B) which are applied to the propulsive central region (16) at locations which are distributed over the length of the leading edge, at least one sliding shroud line (90A, 90B) being engaged in a sliding manner in a guide (92A, 92B)which is fixedly joined to the leading edge, the end of the sliding shroud line (90A, 90B) being fixedly joined to a rear line (40A, 40B).
摘要翻译：具有用于牵引负载的负二面体的机翼（10）包括柔性罩（12），所述柔性罩（12）被限定在两个横向端（14A，14B）之间，所述两个侧端在前面通过前缘相互连接，，在后方，尾随。机翼（10）包括后排线（40A，40B），其连接到布置在机翼的侧端（14A，14B）处的悬挂构件（30A，30B），并且在该推进中心区域（16）的辅助维护装置包括至少一条前端线，其一端连接到与前缘相邻的推进中心区域，并且能够在另一端连接到负载。前线包括一组护罩线（90A，90B），其在分布在前缘的长度上的位置处施加到推进中心区域（16），至少一个滑动护罩线（90A， 90B）在与前缘固定接合的引导件（92A，92B）中滑动接合，滑动护罩线（90A，90B）的端部固定地连接到后线（ 40 A，40 B）。

4. 发明申请

US20050230556A1 Wing having a negative dihedron for towing a load 有权
标题翻译：翼具有负二面体以牵引负载
公开(公告)号：US20050230556A1
公开(公告)日：2005-10-20
申请号：US11067842
申请日：2005-02-28
申请人： Dominique Legaignoux , Bruno Legaignoux
发明人： Dominique Legaignoux , Bruno Legaignoux
IPC分类号： A63H27/08 , B63B35/79 , B64C31/06
CPC分类号： B63B35/7979 , B64C31/06 , B64C2031/065
摘要： The wing (10) having a negative dihedron for towing a load comprises a flexible canopy (12) which is defined between two lateral ends (14A, 14B) which are connected to each other, at the front, by a leading edge (20) and, at the rear, by a trailing edge (22). The canopy (12) has, between those two lateral ends (14A, 14B), a propulsive central region (16) which is bordered at one side and the other by two control regions (18A, 18B). The wing comprises at least a member (30A, 30B) for suspending the load adjacent to each lateral end (14A, 14B) and auxiliary maintenance means (32) which are capable of flattening the propulsive central region (16) adjacent to the leading edge (20) during flight. The trailing edge (22) of the wing is generally concave.
摘要翻译：具有用于牵引负载的负二面体的机翼（10）包括柔性遮篷（12），其限定在两个横向端部（14A，14B）之间，两个侧端部（14A，14B）在前部通过前缘 20），并且在后部由后缘（22）。顶盖（12）在两个横向端部（14A，14B）之间具有在一侧边界且两个控制区域（18A，18B）相邻的推进中心区域（16）。所述机翼至少包括用于将所述负载悬挂在每个侧端（14A，14B）附近的负载和辅助维护装置（32）的至少一个构件（30A，30B），所述辅助维护装置能够使所述推进中心区域（16）相邻到飞行中的前缘（20）。机翼的后缘（22）通常是凹形的。

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