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1. 发明申请

WO2014070339A1 NATURAL LAMINAR FLOW WINGTIP 审中-公开
标题翻译：自然层流流动WINGTIP
公开(公告)号：WO2014070339A1
公开(公告)日：2014-05-08
申请号：PCT/US2013/061675
申请日：2013-09-25
申请人： THE BOEING COMPANY
发明人： CAMPBELL, Darrell D. , LYONS, Brett I.
IPC分类号： B64C3/20 , B64C23/06
CPC分类号： B64C23/069 , B29C70/00 , Y02T50/164
摘要： An aircraft wing tip device (107) includes a unitized, monolithic leading edge torque box that is formed of polymer matrix fiber- reinforced material. The leading edge torque box includes a skin (160) that defines a continuous, uninterrupted outer mold line surface extending aftwardly from a winglet leading edge by a distance of at least approximately 60 percent of a local chord length. The leading edge torque box (172) further includes at least one internal component (162) extending between opposing inner surfaces of the skin and being integrally formed therewith.
摘要翻译：飞机翼尖装置（107）包括由聚合物基质纤维增强材料形成的一体化的整体式前缘扭矩箱。前缘扭矩盒包括一个皮肤（160），其限定从小翼前缘延伸至少大约60％的局部弦长的距离的连续的，不间断的外模线表面。前缘扭矩箱172还包括在皮肤的相对的内表面之间延伸并与其一体形成的至少一个内部部件162。

2. 发明申请

WO2012024051A1 MULTI-SPAR PORT BOX JOINT 审中-公开
标题翻译：多个SPORT PORT BOX JOINT
公开(公告)号：WO2012024051A1
公开(公告)日：2012-02-23
申请号：PCT/US2011/044766
申请日：2011-07-21
申请人： THE BOEING COMPANY , CAMPANA, Joseph, H.
发明人： CAMPANA, Joseph, H.
IPC分类号： B64C1/26 , B64F5/00
CPC分类号： B64C3/26 , B64C1/26 , Y10T29/49826
摘要： A method for connecting a wing. A frame for a wing is positioned relative to a fuselage of an aircraft. The frame has bays and comprise a front spar, a rear spar, and a number of spars located between the front and rear spars. A first number of skin panels is on a first side of the frame, and a second number of skin panels may be on a second side of the frame. The first side is opposite to the second side. Openings are in the first and second numbers of skin panels. The openings are in locations such that each bay has an opening and such that the openings alternate between the first side and the second side between adjacent bays in the bays. The frame is attached to the fuselage using the openings to access an interior of the frame.
摘要翻译：一种连接机翼的方法。翼的框架相对于飞机的机身定位。框架具有托架并且包括前翼梁，后翼梁以及位于前后翼梁之间的多个翼梁。第一数量的皮肤面板位于框架的第一侧上，并且第二数量的皮肤面板可以在框架的第二侧上。第一面与第二面相反。开口是第一和第二数量的皮肤面板。开口处于这样的位置，使得每个隔间具有开口，并且使得开口在第一侧和第二侧之间在相邻的托架间隔开。框架使用开口连接到机身以接近框架的内部。

3. 发明申请

WO2012021188A3 NANO-COATING THERMAL BARRIER AND METHOD FOR MAKING THE SAME 审中-公开
公开(公告)号：WO2012021188A3
公开(公告)日：2012-02-16
申请号：PCT/US2011/035612
申请日：2011-05-06
申请人： THE BOEING COMPANY , RUSSELL, James C. , WHITE, Tresha L. , SHIFLETT, Bryan , CHERINET, Pazion , WADLEY, Scott , BARNHART, Carol , KHOZIKOV, Vyacheslav , NAKAMOTO, Kyle
发明人： RUSSELL, James C. , WHITE, Tresha L. , SHIFLETT, Bryan , CHERINET, Pazion , WADLEY, Scott , BARNHART, Carol , KHOZIKOV, Vyacheslav , NAKAMOTO, Kyle
IPC分类号： C23C24/10 , B22F1/00 , B22F1/02 , C03C8/18
摘要： A coating is adapted to be applied to a substrate for managing the flow of heat traveling through the substrate. The coating comprises an array of metal nano-particles held in a glassy matrix.

4. 发明申请

WO2010104741A1 COMPOSITE STRUCTURES EMPLOYING QUASI-ISOTROPIC LAMINATES 审中-公开
标题翻译：采用等离子体层压板的复合结构
公开(公告)号：WO2010104741A1
公开(公告)日：2010-09-16
申请号：PCT/US2010/026229
申请日：2010-03-04
申请人： THE BOEING COMPANY , DAN-JUMBO, Eugene, A. , KELLER, Russell, L. , WESTERMAN, Everett, A.
发明人： DAN-JUMBO, Eugene, A. , KELLER, Russell, L. , WESTERMAN, Everett, A.
IPC分类号： B32B5/12 , B64C1/12 , B32B5/26 , B32B5/28 , B32B27/04 , B29C70/20
CPC分类号： B32B5/12 , B29C70/202 , B29D99/0014 , B29K2995/0045 , B29L2031/3082 , B32B1/00 , B32B5/022 , B32B5/22 , B32B5/24 , B32B5/26 , B32B7/12 , B32B27/06 , B32B27/08 , B32B27/18 , B32B27/38 , B32B2260/021 , B32B2260/046 , B32B2262/106 , B32B2307/50 , B32B2307/708 , B32B2307/718 , B32B2605/00 , B32B2605/18 , B64C1/068 , B64C2001/0072 , Y02T50/43 , Y10T428/24124
摘要： A composite laminate comprises a stack of unidirectional fiber reinforced composite plies arranged in a fiber orientation sequence providing the laminate with quasi-isotropic properties.
摘要翻译：复合层压板包括以纤维取向顺序布置的单向纤维增强复合帘布层的堆叠，为层叠体提供准各向同性的特性。

5. 发明申请

WO2010101744A2 TOOL SLEEVE FOR MOLD DIE AND METHOD OF MOLDING PARTS USING THE SAME 审中-公开
标题翻译：用于模具的工具套管和使用其的模具部件的方法
公开(公告)号：WO2010101744A2
公开(公告)日：2010-09-10
申请号：PCT/US2010/025176
申请日：2010-02-24
申请人： THE BOEING COMPANY , PREBIL, Charles R. , FOX, James R. , RUBIN, Alexander M. , WILKERSON, Randall D.
发明人： PREBIL, Charles R. , FOX, James R. , RUBIN, Alexander M. , WILKERSON, Randall D.
IPC分类号： B29C43/36
CPC分类号： B29C70/526 , B29C33/306 , B29C43/222 , B29C43/36 , B29C43/44 , B29C2043/3665 , B29D99/0003
摘要： A device changes the shape of a die used to compression mold a part. The device includes a sleeve placed between the die and a charge to be molded. The sleeve has an inner face generally conforming to a face of the die, and a outer face for molding a part.
摘要翻译：装置改变用于压缩模制零件的模具的形状。该装置包括放置在模具和待模制的电荷之间的套筒。套筒具有大致与模具的表面相一致的内表面和用于模制零件的外表面。

6. 发明申请

WO2010101741A2 METHOD FOR PRODUCING CONTOURED COMPOSITE STRUCTURES AND STRUCTURES PRODUCED THEREBY 审中-公开
标题翻译：生产结构复合结构的方法和生产的结构
公开(公告)号：WO2010101741A2
公开(公告)日：2010-09-10
申请号：PCT/US2010/025110
申请日：2010-02-23
申请人： THE BOEING COMPANY , MCCARVILLE, Douglas A. , SWEETIN, Joseph L. , GUZMAN, Juan C.
发明人： MCCARVILLE, Douglas A. , SWEETIN, Joseph L. , GUZMAN, Juan C.
IPC分类号： B29C70/34
CPC分类号： B29C70/38 , B29C70/30 , B29D99/0007 , B29L2031/3082 , Y10T156/1002 , Y10T156/1026 , Y10T156/1028 , Y10T156/1031 , Y10T156/1052 , Y10T156/108 , Y10T428/24124
摘要： A contoured composite structure is fabricated by laying up a composite charge that includes at least one ply formed by uni-directional fiber pre-preg ply segments having substantially constant widths. The ply segments are placed in side-by-side, overlapping relationship with their longitudinal centerlines aligned in a polar orientation related to the contour of the structure. The charge is formed into the shape of the structure and cured.
摘要翻译：通过铺设复合电荷来制造轮廓复合结构，所述复合电荷包括由具有基本上恒定宽度的单向纤维预制片段形成的至少一层。帘布层片段与它们的纵向中心线并排放置，与与结构轮廓相关的极性取向对齐。电荷形成为结构的形状并固化。

7. 发明申请

WO2009131793A1 EXHAUST WASHED STRUCTURE AND ASSOCIATED COMPOSITE STRUCTURE AND METHOD OF FABRICATION 审中-公开
标题翻译：排气结构与相关复合结构及其制造方法
公开(公告)号：WO2009131793A1
公开(公告)日：2009-10-29
申请号：PCT/US2009/038649
申请日：2009-03-27
申请人： THE BOEING COMPANY , HAND, Michael, L. , CHAKRABARTI, Buddhadev , LEHMAN, Leanne, L. , MATHUR, Gopal, P.
发明人： HAND, Michael, L. , CHAKRABARTI, Buddhadev , LEHMAN, Leanne, L. , MATHUR, Gopal, P.
IPC分类号： F02K1/82 , F02C7/24
CPC分类号： F02K1/822 , F02C7/24 , F05D2250/61 , Y02T50/672 , Y02T50/675 , Y10T29/49826 , Y10T428/234 , Y10T428/239 , Y10T428/24612 , Y10T428/24694 , Y10T428/24711
摘要： A composite structure (10) and an associated exhaust washed structure (20) are provided which may be formed of ceramic matrix composite (CMC) materials. A method of fabricating a composite structure which may include the CMC material is also provided. A composite structure (10) includes a corrugated septum (12) extending in a lengthwise direction. The composite structure (10) also includes a flute (16) within which the corrugated septum (12) is disposed to form, a partitioned flute assembly (15).
摘要翻译：提供复合结构（10）和相关联的排气清洗结构（20），其可以由陶瓷基质复合材料（CMC）材料形成。还提供了可以包括CMC材料的复合结构的制造方法。复合结构（10）包括在长度方向上延伸的波纹隔膜（12）。复合结构（10）还包括凹槽（16），其中波纹隔垫（12）设置在其中以形成分隔的槽纹组件（15）。

8. 发明申请

WO2008150688A1 APPARATUS AND METHODS FOR SECURING A FIRST STRUCTURAL MEMBER AND A SECOND STRUCTURAL MEMBER TO ONE ANOTHER 审中-公开
标题翻译：用于安全第一结构部件和第二结构部件到另一个的装置和方法
公开(公告)号：WO2008150688A1
公开(公告)日：2008-12-11
申请号：PCT/US2008/064157
申请日：2008-05-19
申请人： THE BOEING COMPANY , KULESHA, Richard, L.
发明人： KULESHA, Richard, L.
IPC分类号： B64C1/00
CPC分类号： B64C1/12 , B64C1/06 , B64F5/10 , Y10T29/49622 , Y10T29/49623 , Y10T29/53 , Y10T403/34 , Y10T403/64
摘要： Apparatus and methods for securing a first structural member (10) and a second structural member (12) to one another. In one embodiment a two-piece fitting (36) is provided.' The fitting includes a variable gap between attachment surfaces, enabling the fitting to accommodate structural members of variable thickness. The fitting also includes overlapping sections (42, 52) that provide increased resistance to pull-off loads and impact loads. The configuration of the fitting advantageously simplifies the assembly process and preserves the integrity of the adhesive to form a strong joint.
摘要翻译：用于将第一结构构件（10）和第二结构构件（12）彼此固定的装置和方法。在一个实施例中，提供两件式配件（36）。配件包括附接表面之间的可变间隙，使得配件能够容纳可变厚度的结构构件。该配件还包括重叠部分（42,52），其提供增加的拉脱载荷和冲击载荷的阻力。配件的构造有利地简化了组装过程并且保持了粘合剂的完整性以形成牢固的接头。

9. 发明申请

WO2008097847A1 METHOD AND MATERIAL EFFICIENT TOOLING FOR CONTINUOUS COMPRESSION MOLDING 审中-公开
标题翻译：用于连续压缩成型的方法和材料有效工具
公开(公告)号：WO2008097847A1
公开(公告)日：2008-08-14
申请号：PCT/US2008/052806
申请日：2008-02-01
申请人： THE BOEING COMPANY , WILKERSON, Randall, D. , FOX, James, R. , RUBIN, Alexander, M.
发明人： WILKERSON, Randall, D. , FOX, James, R. , RUBIN, Alexander, M.
IPC分类号： B29C70/54 , B29C43/22 , B29C43/34
CPC分类号： B29D7/01 , B29C43/22 , B29C43/228 , B29C70/526 , B29C70/54 , B29K2105/08 , Y10T156/101 , Y10T156/1737
摘要： Thermoplastic laminates are fabricated in a continuous compression molding production line. A lay-up of laminate plies is placed in a recess on a carrying tool, and the tool is moved through successive forming operations on the line, including preforming and consolidation operations. The tool is separated from the fully formed part at the end of the line and may be reused. Use of the carrying tool reduces material scrap.
摘要翻译：热塑性层压板在连续压塑生产线中制造。将层压板层叠放置在承载工具上的凹槽中，并且该工具通过连续的成型操作在线上移动，包括预成形和固结操作。该工具与管线末端的完全成型部分分离，可以重新使用。携带工具的使用减少了材料废料。

10. 发明申请

WO2008030297A1 APPARATUS AND METHODS FOR TWO-DIMENSIONAL AND THREE-DIMENSIONAL INSPECTION OF A WORKPIECE 审中-公开
标题翻译：用于二维和三维检查工作的装置和方法
公开(公告)号：WO2008030297A1
公开(公告)日：2008-03-13
申请号：PCT/US2007/016175
申请日：2007-07-17
申请人： THE BOEING COMPANY , WALTON, Steven, R.
发明人： WALTON, Steven, R.
IPC分类号： G01N21/89
CPC分类号： G01N21/8901 , B29C70/386 , G01N2021/8472
摘要： Apparatus and methods for inspecting a workpiece are provided. According to one embodiment, a method for inspecting a workpiece comprises illuminating at least a portion of the workpiece with at least one illumination beam and capturing at least one image including at least on line signature formed by illuminating the workpiece with the illumination beam. The method further includes performing two-dimensional and three-dimensional processes on the captured image and classifying at least one feature associated with the workpiece based at least in part on data generated by the two-dimensional and three-dimensional processes.
摘要翻译：提供了用于检查工件的装置和方法。根据一个实施例，一种用于检查工件的方法包括用至少一个照明光束照射至少一部分工件，并且捕获至少一个图像，该至少一个图像至少包括通过用照明光束照射工件而形成的线上签名。该方法还包括至少部分地基于由二维和三维过程产生的数据，对所捕获的图像执行二维和三维处理并对与工件相关联的至少一个特征进行分类。

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