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1. 发明申请

WO2009004364A3 IMPROVEMENTS IN ELONGATE COMPOSITE STRUCTURAL MEMBER 审中-公开
标题翻译：在ELENATE复合结构构件中的改进
公开(公告)号：WO2009004364A3
公开(公告)日：2009-05-22
申请号：PCT/GB2008050485
申请日：2008-06-24
申请人： AIRBUS UK LTD , WOOD ERIC STEPHEN
发明人： WOOD ERIC STEPHEN
IPC分类号： B64C3/18 , B64C3/26 , B64F5/00
CPC分类号： B64C3/182 , B29C70/30 , B29D99/0003 , B64C3/26 , Y02T50/43 , Y02T50/433 , Y10T428/24 , Y10T428/24174 , Y10T428/24628
摘要： A composite material elongate structural member (102), such as a spar or stringer, for use in an aerospace structure, comprises a web (108) having an angled portion, for example in the form of a chamfer (107), which joins a foot (106) of the member to the rest of the web. A first surface (110) on the foot is shaped to abut a structure (104) to be stiffened. The foot has a second surface (112) opposite the first surface. The web has a third surface (114) and a fourth surface (116) at the same layer in the composite material as the first and third surfaces, respectively. In the interposed portion there is a fifth surface (130) which joins the first and third surfaces. The geometry of the member may vary along its length (L) so that with increasing distance, the first surface is displaced towards the second surface,wherby the thickness between the first and second surface remains substantially constant, as the width of the fifth surface decreases.
摘要翻译：用于航空航天结构的复合材料细长结构构件（例如翼梁或纵梁）包括具有成角度的部分的腹板（108），例如呈倒角（107）的形式，其连接成员的脚（106）到网络的其余部分。脚上的第一表面（110）成形为邻接待硬化的结构（104）。脚具有与第一表面相对的第二表面（112）。纸幅分别具有与第一和第三表面在复合材料中相同层处的第三表面（114）和第四表面（116）。在插入部分中，存在第一和第三表面的第五表面（130）。构件的几何形状可以沿其长度（L）变化，使得随着距离的增加，第一表面朝向第二表面移位，由于第五表面的宽度减小，第一表面和第二表面之间的厚度保持基本上恒定。

2. 发明专利

CA2691165A1 IMPROVEMENTS IN ELONGATE COMPOSITE STRUCTURAL MEMBER 未知
公开(公告)号：CA2691165A1
公开(公告)日：2009-01-08
申请号：CA2691165
申请日：2008-06-24
申请人： AIRBUS UK LTD
发明人： WOOD ERIC STEPHEN
IPC分类号： B64C3/18 , B64C3/26 , B64F5/00
摘要： A composite material elongate structural member (102), such as a spar or stringer, for use in an aerospace structure, comprises a web (108) having an angled portion, for example in the form of a chamfer (107), which joins a foot (106) of the member to the rest of the web. A first surface (110) on the foot is shaped to abut a structure (104) to be stiffened. The foot has a second surface (112) opposite the first surface. The web has a third surface (114) and a fourth surface (116) at the same layer in the composite material as the first and third surfaces, respectively. In the interposed portion there is a fifth surface (130) which joins the first and third surfaces. The geometry of the member may vary along its length (L) so that with increasing distance, the first surface is displaced towards the second surface,wherby the thickness between the first and second surface remains substantially constant, as the width of the fifth surface decreases.

3. 发明专利

CA2691165C IMPROVEMENTS IN ELONGATE COMPOSITE STRUCTURAL MEMBERS 未知
公开(公告)号：CA2691165C
公开(公告)日：2016-10-04
申请号：CA2691165
申请日：2008-06-24
申请人： AIRBUS UK LTD
发明人： WOOD ERIC STEPHEN
IPC分类号： B64C3/18 , B64C3/26 , B64F5/00
摘要： A composite material elongate structural member (102), such as a spar or stringer, for use in an aerospace structure, comprises a web (108) having an angled portion, for example in the form of a chamfer (107), which joins a foot (106) of the member to the rest of the web. A first surface (110) on the foot is shaped to abut a structure (104) to be stiffened. The foot has a second surface (112) opposite the first surface. The web has a third surface (114) and a fourth surface (116) at the same layer in the composite material as the first and third surfaces, respectively. In the interposed portion there is a fifth surface (130) which joins the first and third surfaces. The geometry of the member may vary along its length (L) so that with increasing distance, the first surface is displaced towards the second surface,wherby the thickness between the first and second surface remains substantially constant, as the width of the fifth surface decreases.

4. 发明专利

BRPI0813463A2 未知
公开(公告)号：BRPI0813463A2
公开(公告)日：2014-12-23
申请号：BRPI0813463
申请日：2008-06-24
申请人： AIRBUS UK LTD
发明人： WOOD ERIC STEPHEN
IPC分类号： B64C3/18 , B64C3/26 , B64F5/00
摘要： A composite material elongate structural member, such as a spar or stringer, for use in an aerospace structure, comprises a web having an angled portion, for example in the form of a chamfer, curved surface or the like, which joins a foot of the member to the rest of the web. A first surface on the foot is shaped to abut a structure to be stiffened. The foot also has a second surface opposite the first surface. The web has a third surface and a fourth surface at the same layer in the composite material as the first and third surfaces, respectively. On/in the interposed portion there is a fifth surface which joins the first and third surfaces. The geometry of the member may vary along its length (L) so that with increasing distance, the first surface is displaced towards the second surface as the width of the fifth surface decreases. The risk of causing, during fabrication of the elongate member, undesirable creasing, stressing or stretching of composite material layers in a region in which the geometry of the member varies may be reduced by means of such an arrangement.

5. 发明专利

GB2417228A Aircraft wing 未知
公开(公告)号：GB2417228A
公开(公告)日：2006-02-22
申请号：GB0418487
申请日：2004-08-18
申请人： AIRBUS UK LTD
发明人： NEALE LEE ROBERT , QUAYLE ALAN , WOOD ERIC STEPHEN
IPC分类号： B64C3/26 , B64C1/00 , B64C3/00 , B64C3/18 , B64C3/38 , B64C7/00 , B64C11/24 , B64C27/46
摘要： An aircraft wing (1) that may be used in large transport aircraft comprises: (i) a first wing portion (2) that, in use, forms an inner portion of an aircraft wing, and is attached to (ii) a readily replaceable second wing portion (3) comprising a wingtip. The second wing portion (3) may be readily replaceable by a third wing portion comprising a wingtip, the third wing portion having a different functionality from the second wing portion (3).

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