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公开(公告)号：EP2311732A3
公开(公告)日：2012-02-01
申请号：EP10187742.1
申请日：2010-10-15
申请人： The Boeing Company
发明人： Chen, Winnie W. , Zadorozny, Edward A. , Thatcher, Conley S. , Embler, Jonathan D. , Lehman, Leanne L. , Pinney, Thomas
IPC分类号： B64G1/58
CPC分类号： B64G1/58 , Y10T29/49826
摘要： A blanket assembly (1) includes a shear fabric (10) and an attachment frame (3) wrapped in the shear fabric. A thermal protection blanket (14) is carried by the shear fabric (10).
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2.发明公开Ceramic matrix composite structure having fluted core and method of making the same 审中-公开Keramikmatrixverbundstruktur mit profiliertem Kern und Herstellungsverfahrendafür
公开(公告)号：EP2008807A3
公开(公告)日：2010-12-22
申请号：EP08158706.5
申请日：2008-06-20
申请人： The Boeing Company
发明人： Lehman, Leanne L. , McCann, John R.
CPC分类号： B32B3/18 , B32B3/04 , B32B3/08 , B32B3/263 , B32B3/28 , B32B5/02 , B32B5/22 , B32B5/245 , B32B5/26 , B32B9/005 , B32B9/047 , B32B18/00 , B32B2260/021 , B32B2260/046 , B32B2262/105 , B32B2266/02 , B32B2266/04 , B32B2307/304 , B32B2307/306 , B32B2307/308 , B32B2307/50 , B32B2307/54 , B32B2307/718 , B32B2307/734 , B32B2605/18 , B64C1/00 , C04B2237/32 , C04B2237/341 , C04B2237/343 , C04B2237/36 , C04B2237/361 , C04B2237/365 , C04B2237/368 , Y10T428/17
摘要： A ceramic matrix composite structure (10) includes a load carrying fluted core (16) formed from a ceramic matrix composite. The fluted core (16) includes a plurality of nested flute members (18a, b) laminated between a pair of ceramic matrix composite facesheets (12, 14). The flute members (18a, b) are fabricated by wrapping ceramic resin fabric around a mandrel, curing the flute members (18a, b) and then removing the mandrels. The structure may include reinforced areas in which the facesheets (12, 14) are laminated directly together to receive fasteners for mounting the structure. The structure may include both flat and curved portions (Fig. 2).
摘要翻译： 陶瓷基体复合结构（10）包括由陶瓷基体复合材料形成的载荷为槽纹的芯（16）。 带槽纹芯（16）包括层叠在一对陶瓷基质复合面板（12,14）之间的多个嵌套槽纹构件（18a，b）。 通过将陶瓷树脂织物缠绕在心轴上，固化槽形构件（18a，b）然后去除心轴来制造凹槽构件（18a，b）。 该结构可以包括加强区域，其中面板（12,14）直接层叠在一起以接收用于安装结构的紧固件。 该结构可以包括平坦部分和弯曲部分（图2）。
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3.发明公开
公开(公告)号：EP2017073A2
公开(公告)日：2009-01-21
申请号：EP08252351.5
申请日：2008-07-10
申请人： THE BOEING COMPANY
CPC分类号： B32B7/08 , B32B5/18 , B32B5/245 , B32B5/26 , B32B9/005 , B32B9/047 , B32B2250/40 , B32B2260/023 , B32B2262/105 , B32B2266/08 , B32B2307/306 , B32B2605/08 , B32B2605/18 , C04B35/62844 , Y10T29/49904
摘要： A CMC sandwich used to fabricate CMC structures includes facesheets bonded to a core reinforced with a ceramic truss comprising an array of CMC pins. The binder matrix in the ends of the pins is removed, leaving exposed, flexible ceramic fibers. The exposed ceramic fibers are bent so as to extend parallel to the facesheets, and are bonded to one or more plies of the facesheets. The binder matrix in the ends of the ceramic pins may be removed by mechanical or chemical processes.
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4.发明授权Composite structure having ceramic truss core and method for making the same 有权Verbundstruktur mit Keramikbinderkern und Herstellungsverfahrendafür
公开(公告)号：EP2017073B1
公开(公告)日：2013-09-25
申请号：EP08252351.5
申请日：2008-07-10
申请人： THE BOEING COMPANY
IPC分类号： B32B7/08 , B32B18/00 , B64C1/12 , B64C3/26 , C04B35/628
CPC分类号： B32B7/08 , B32B5/18 , B32B5/245 , B32B5/26 , B32B9/005 , B32B9/047 , B32B2250/40 , B32B2260/023 , B32B2262/105 , B32B2266/08 , B32B2307/306 , B32B2605/08 , B32B2605/18 , C04B35/62844 , Y10T29/49904
摘要： A CMC sandwich used to fabricate CMC structures includes facesheets (24,26) bonded to a core (22) reinforced with a ceramic truss (25) comprising an array of CMC pins (28). The binder matrix in the ends of the pins is removed, leaving exposed, flexible ceramic fibers. The exposed ceramic fibers are bent so as to extend parallel to the facesheets, and are bonded to one or more plies of the facesheets. The binder matrix in the ends of the ceramic pins may be removed by mechanical or chemical processes.
摘要翻译： 用于制造CMC结构的CMC夹层包括结合到由包括CMC销（28）的阵列的陶瓷桁架（25）增强的芯部（22）的面板（24,26）。 在销的端部中的粘合剂基质被去除，留下暴露的柔性陶瓷纤维。 暴露的陶瓷纤维被弯曲以平行于面板延伸，并且被粘合到面板的一个或多个层。 可以通过机械或化学过程去除陶瓷销的端部中的粘合剂基质。
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5.发明公开
公开(公告)号：EP2017073A3
公开(公告)日：2012-01-04
申请号：EP08252351.5
申请日：2008-07-10
申请人： THE BOEING COMPANY
IPC分类号： B32B7/08 , B32B18/00 , B64C1/12 , B64C3/26 , C04B35/628
CPC分类号： B32B7/08 , B32B5/18 , B32B5/245 , B32B5/26 , B32B9/005 , B32B9/047 , B32B2250/40 , B32B2260/023 , B32B2262/105 , B32B2266/08 , B32B2307/306 , B32B2605/08 , B32B2605/18 , C04B35/62844 , Y10T29/49904
摘要： A CMC sandwich used to fabricate CMC structures includes facesheets (24,26) bonded to a core (22) reinforced with a ceramic truss (25) comprising an array of CMC pins (28). The binder matrix in the ends of the pins is removed, leaving exposed, flexible ceramic fibers. The exposed ceramic fibers are bent so as to extend parallel to the facesheets, and are bonded to one or more plies of the facesheets. The binder matrix in the ends of the ceramic pins may be removed by mechanical or chemical processes.
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公开(公告)号：EP2008807B1
公开(公告)日：2018-08-29
申请号：EP08158706.5
申请日：2008-06-20
申请人： The Boeing Company
发明人： Lehman, Leanne L. , McCann, John R.
CPC分类号： B32B3/18 , B32B3/04 , B32B3/08 , B32B3/263 , B32B3/28 , B32B5/02 , B32B5/22 , B32B5/245 , B32B5/26 , B32B9/005 , B32B9/047 , B32B18/00 , B32B2260/021 , B32B2260/046 , B32B2262/105 , B32B2266/02 , B32B2266/04 , B32B2307/304 , B32B2307/306 , B32B2307/308 , B32B2307/50 , B32B2307/54 , B32B2307/718 , B32B2307/734 , B32B2605/18 , C04B2237/32 , C04B2237/341 , C04B2237/343 , C04B2237/36 , C04B2237/361 , C04B2237/365 , C04B2237/368 , Y10T428/17
摘要： A ceramic matrix composite structure (10) includes a load carrying fluted core (16) formed from a ceramic matrix composite. The fluted core (16) includes a plurality of nested flute members (18a, b) laminated between a pair of ceramic matrix composite facesheets (12, 14). The flute members (18a, b) are fabricated by wrapping ceramic resin fabric around a mandrel, curing the flute members (18a, b) and then removing the mandrels. The structure may include reinforced areas in which the facesheets (12, 14) are laminated directly together to receive fasteners for mounting the structure. The structure may include both flat and curved portions (Fig. 2).
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公开(公告)号：EP2311732B1
公开(公告)日：2018-04-04
申请号：EP10187742.1
申请日：2010-10-15
申请人： The Boeing Company
发明人： Chen, Winnie W. , Zadorozny, Edward A. , Thatcher, Conley S. , Embler, Jonathan D. , Lehman, Leanne L. , Pinney, Thomas
IPC分类号： B64G1/58
CPC分类号： B64G1/58 , Y10T29/49826
摘要： A blanket assembly (1) includes a shear fabric (10) and an attachment frame (3) wrapped in the shear fabric. A thermal protection blanket (14) is carried by the shear fabric (10).
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公开(公告)号：EP2311732A2
公开(公告)日：2011-04-20
申请号：EP10187742.1
申请日：2010-10-15
申请人： The Boeing Company
发明人： Chen, Winnie W. , Zadorozny, Edward A. , Thatcher, Conley S. , Embler, Jonathan D. , Lehman, Leanne L. , Pinney, Thomas
IPC分类号： B64G1/58
CPC分类号： B64G1/58 , Y10T29/49826
摘要： A blanket assembly (1) includes a shear fabric (10) and an attachment frame (3) wrapped in the shear fabric. A thermal protection blanket (14) is carried by the shear fabric (10).
摘要翻译： 橡皮布组件（1）包括剪切织物（10）和缠绕在剪切织物中的附接框架（3）。 热保护毯（14）由剪切织物（10）承载。
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9.发明公开Ceramic matrix composite structure having fluted core and method of making the same 审中-公开与其异形铁心及其制造方法的陶瓷基复合结构
公开(公告)号：EP2008807A2
公开(公告)日：2008-12-31
申请号：EP08158706.5
申请日：2008-06-20
申请人： The Boeing Company
发明人： Lehman, Leanne L. , McCann, John R.
CPC分类号： B32B3/18 , B32B3/04 , B32B3/08 , B32B3/263 , B32B3/28 , B32B5/02 , B32B5/22 , B32B5/245 , B32B5/26 , B32B9/005 , B32B9/047 , B32B18/00 , B32B2260/021 , B32B2260/046 , B32B2262/105 , B32B2266/02 , B32B2266/04 , B32B2307/304 , B32B2307/306 , B32B2307/308 , B32B2307/50 , B32B2307/54 , B32B2307/718 , B32B2307/734 , B32B2605/18 , B64C1/00 , C04B2237/32 , C04B2237/341 , C04B2237/343 , C04B2237/36 , C04B2237/361 , C04B2237/365 , C04B2237/368 , Y10T428/17
摘要： A ceramic matrix composite structure (10) includes a load carrying fluted core (16) formed from a ceramic matrix composite. The fluted core (16) includes a plurality of nested flute members (18a, b) laminated between a pair of ceramic matrix composite facesheets (12, 14). The flute members (18a, b) are fabricated by wrapping ceramic resin fabric around a mandrel, curing the flute members (18a, b) and then removing the mandrels. The structure may include reinforced areas in which the facesheets (12, 14) are laminated directly together to receive fasteners for mounting the structure. The structure may include both flat and curved portions ( Fig. 2 ).
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