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1. 发明申请

US20150321746A1 FIXED WING OF AN AIRCRAFT 有权
标题翻译：固定的飞机的翅膀
公开(公告)号：US20150321746A1
公开(公告)日：2015-11-12
申请号：US14713756
申请日：2015-05-15
申请人： Airbus Operations GmbH , Airbus Operations Ltd.
发明人： Gerd Heller , Alexander Buescher , Frank Theurich , Tom Gibson , Michael Karwin , Stephen Powell
IPC分类号： B64C3/58
CPC分类号： B64C3/58 , B64C23/069 , Y02T50/164
摘要： A fixed wing of an aircraft, having a main wing extending over a half-span with a wing box including spars extending along the spanwise direction of the main wing, ribs arranged one in back of the other viewed in the spanwise direction, and an outer skin. The wing box includes a wing box base section (K10) and a wing box adapter section, that forms the outer end area of the wing box, as viewed from the wing root, and is designed to secure a wing tip device. In its nominal state of construction, the dihedral angle of the wing box adapter section referring to the respective local spanwise direction continuously increases by at most 60 degrees from the outer rib of the wing box base section (K10) up to the outermost rib of the wing box adapter section.
摘要翻译：一种飞机的固定翼，具有在半跨上延伸的主翼，翼翼包括沿着主翼的翼展方向延伸的翼梁，沿翼展方向观察的一个在后面布置的肋，以及外翼皮肤。机翼箱包括一个翼盒基部（K10）和一个翼盒适配器部分，从机翼根部看，形成了机翼箱的外端区域，并被设计成固定翼尖装置。在其标称结构状态下，翼箱适配器部分参考相应的局部翼展方向的二面角从翼箱基部（K10）的外肋连续增加至多60度，直到最终肋翼盒适配器部分。

2. 发明授权

US09056671B2 Fixed wing of an aircraft 有权
标题翻译：一架飞机的固定翼
公开(公告)号：US09056671B2
公开(公告)日：2015-06-16
申请号：US13650457
申请日：2012-10-12
申请人： Airbus Operations GmbH , Airbus Operations Ltd.
发明人： Gerd Heller , Alexander Buescher , Frank Theurich , Tom Gibson , Michael Karwin , Stephen Powell
IPC分类号： B64C23/06
CPC分类号： B64C3/58 , B64C23/069 , Y02T50/164
摘要： A fixed wing of an aircraft, having a main wing extending over a half-span with a wing box including spars extending along the spanwise direction of the main wing, ribs arranged one in back of the other viewed in the spanwise direction, and an outer skin. The wing box includes a wing box base section (K10) and a wing box adapter section, that forms the outer end area of the wing box, as viewed from the wing root, and is designed to secure a wing tip device. In its nominal state of construction, the dihedral angle of the wing box adapter section referring to the respective local spanwise direction continuously increases by at most 60 degrees from the outer rib of the wing box base section (K10) up to the outermost rib of the wing box adapter section.
摘要翻译：一种飞机的固定翼，具有在半跨上延伸的主翼，翼翼包括沿着主翼的翼展方向延伸的翼梁，沿翼展方向观察的一个在后面布置的肋，以及外翼皮肤。机翼箱包括一个翼盒基部（K10）和一个翼盒适配器部分，从机翼根部看，形成了机翼箱的外端区域，并被设计成固定翼尖装置。在其标称结构状态下，翼箱适配器部分参考相应的局部翼展方向的二面角从翼箱基部（K10）的外肋连续增加至多60度，直到最终肋翼盒适配器部分。

3. 发明申请

US20130277504A1 FIXED WING OF AN AIRCRAFT 有权
公开(公告)号：US20130277504A1
公开(公告)日：2013-10-24
申请号：US13650457
申请日：2012-10-12
申请人： AIRBUS OPERATIONS GMBH , AIRBUS OPERATIONS LTD.
发明人： Gerd Heller , Alexander Buescher , Frank Theurich , Tom Gibson , Michael Karwin , Stephen Powell
IPC分类号： B64C23/06
CPC分类号： B64C3/58 , B64C23/069 , Y02T50/164
摘要： A fixed wing of an aircraft, having a main wing extending over a half-span with a wing box including spars extending along the spanwise direction of the main wing, ribs arranged one in back of the other viewed in the spanwise direction, and an outer skin. The wing box includes a wing box base section (K10) and a wing box adapter section, that forms the outer end area of the wing box, as viewed from the wing root, and is designed to secure a wing tip device. In its nominal state of construction, the dihedral angle of the wing box adapter section referring to the respective local spanwise direction continuously increases by at most 60 degrees from the outer rib of the wing box base section (K10) up to the outermost rib of the wing box adapter section.

4. 发明授权

US09555874B2 Fixed wing of an aircraft 有权
标题翻译：一架飞机的固定翼
公开(公告)号：US09555874B2
公开(公告)日：2017-01-31
申请号：US14713756
申请日：2015-05-15
申请人： Airbus Operations GmbH , Airbus Operations Ltd.
发明人： Gerd Heller , Alexander Buescher , Frank Theurich , Tom Gibson , Michael Karwin , Stephen Powell
IPC分类号： B64C3/58 , B64C23/06
CPC分类号： B64C3/58 , B64C23/069 , Y02T50/164
摘要： A fixed wing of an aircraft, having a main wing extending over a half-span with a wing box including spars extending along the spanwise direction of the main wing, ribs arranged one in back of the other viewed in the spanwise direction, and an outer skin. The wing box includes a wing box base section (K10) and a wing box adapter section, that forms the outer end area of the wing box, as viewed from the wing root, and is designed to secure a wing tip device. In its nominal state of construction, the dihedral angle of the wing box adapter section referring to the respective local spanwise direction continuously increases by at most 60 degrees from the outer rib of the wing box base section (K10) up to the outermost rib of the wing box adapter section.
摘要翻译：一种飞机的固定翼，具有在半跨上延伸的主翼，翼翼包括沿着主翼的翼展方向延伸的翼梁，沿翼展方向观察的一个在后面布置的肋，以及外翼皮肤。机翼箱包括一个翼盒基部（K10）和一个翼盒适配器部分，从机翼根部看，形成了机翼箱的外端区域，并被设计成固定翼尖装置。在其标称结构状态下，翼箱适配器部分参考相应的局部翼展方向的二面角从翼箱基部（K10）的外肋连续增加至多60度，直到最终肋翼盒适配器部分。

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