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1. 发明申请

WO2011127938A1 FIXED WING OF AN AIRCRAFT 审中-公开
标题翻译：固定翼的飞机
公开(公告)号：WO2011127938A1
公开(公告)日：2011-10-20
申请号：PCT/EP2010/002250
申请日：2010-04-12
申请人： AIRBUS OPERATIONS GMBH , AIRBUS OPERATIONS LTD. , HELLER, Gerd , BUESCHER, Alexander , THEURICH, Frank , GIBSON, Tom , KARWIN, Michael , POWELL, Stephen
发明人： HELLER, Gerd , BUESCHER, Alexander , THEURICH, Frank , GIBSON, Tom , KARWIN, Michael , POWELL, Stephen
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 comprised of spars extending along the spanwise direction of the main wing, a plurality of ribs arranged one in back of the other viewed in the spanwise direction, and an outer skin. The wing box is comprised of a wing box base section (K10) and a wing box adapter section (20), 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 (W). 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 (R3) of the wing box base section (K10) up to the outermost rib (R5) 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，翼翼由沿着主翼的翼展方向延伸的翼梁组成，沿翼展方向观察的多个肋布置在另一个后面，和外皮。翼箱由翼箱基部（K10）和翼盒适配器部分（20）组成，从机翼根部观察时，形成翼盒的外端区域，并被设计成固定翼尖设备（W）。在其标称建造状态下，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（R3）连续增加至多60度，直到最外侧机翼盒适配器部分的肋（R5）。

2. 发明申请

WO2010124877A1 NON-PLANAR WING TIP DEVICE FOR WINGS OF AIRCRAFT, AND WING COMPRISING SUCH A WING TIP DEVICE 审中-公开
标题翻译：用于飞机翼的非平面翼梢装置以及包括这种翼翼装置的翼
公开(公告)号：WO2010124877A1
公开(公告)日：2010-11-04
申请号：PCT/EP2010/002663
申请日：2010-04-30
申请人： AIRBUS OPERATIONS GMBH , BUESCHER, Alexander , KARWIN, Michael , THEURICH, Frank
发明人： BUESCHER, Alexander , KARWIN, Michael , THEURICH, Frank
IPC分类号： B64C23/06
CPC分类号： B64C23/069 , Y02T50/164
摘要： A wing tip device (W; W1, W2) for a wing (T; 10a, 10b), comprising aroot (E1) and atip (E2) and the following determinant characteristics: the local dihedral of the wing tip device (W; W1, W2) continuously increases or decreases from the root (E1) to the tip (E2); the local sweep of the trailing edge (50) continuously increases along its progression from the root (E1) to the tip (E2) of the wing tip device (W; W1, W2); wherein the local sweep of the leading edge (60) continuously increases in the progression of the leading edge (60) from the root (E1) to a first intermediate point (61a); continuously decreases from the first intermediate point (61a) to a second intermediate point (62a); and continuously increases from the second intermediate point (62a) at least to a region before of the tip (E2) of the wing tip device (W; W1, W2); as well as a wing comprising a wing tip device (W; W1, W2).
摘要翻译：一种用于机翼（T; 10a，10b）的翼尖装置（W; W1，W2），包括根部（E1）和尖端（E2）以及以下行列式特征：翼尖装置（W; W1，W2）从根部（E1）向尖端（E2）连续增大或减小; 后缘（50）的局部扫掠沿其从翼尖装置（W; W1，W2）的根部（E1）到尖端（E2）的进展连续地增加; 其中前缘（60）的局部扫掠在前缘（60）从根部（E1）到第一中间点（61a）的前进中连续增加; 从第一中间点（61a）连续减小到第二中间点（62a）; 并且从第二中间点（62a）至少连续增加到翼尖装置（W; W1，W2）的尖端（E2）之前的区域; 以及包括翼尖装置（W; W1，W2）的机翼。

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