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1. 发明申请

WO2012064447A2 METHODS AND SYSTEMS FOR FABRICATING COMPOSITE PARTS USING A SMP APPARATUS AS A RIGID LAY-UP TOOL AND A BLADDER 审中-公开
标题翻译：使用SMP装置作为刚性复合工具和膀胱来制造复合部件的方法和系统
公开(公告)号：WO2012064447A2
公开(公告)日：2012-05-18
申请号：PCT/US2011/055571
申请日：2011-10-10
申请人： SPIRIT AEROSYSTEMS, INC. , KYSAR, Randy , FIEGENBAUM, Carl Ray , PICKELL, Kristin
发明人： KYSAR, Randy , FIEGENBAUM, Carl Ray , PICKELL, Kristin
IPC分类号： B29C61/06 , B29C53/82 , B29C70/46
CPC分类号： B29C70/44 , B29C33/485 , B29C53/587 , B29C53/824
摘要： A method and apparatus for fabricating a composite part, such as a fuselage or internal stiffener, with a shape memory polymer (SMP) apparatus usable as both a rigid lay-up tool and as a bladder. The SMP apparatus may be heated until malleable, shaped, and then cooled in a desired rigid tool configuration. For example, cavities may be formed into the SMP apparatus for nesting components therein to co-bond or co-cure with the composite part. The composite material may be applied onto the SMP apparatus in the rigid tool configuration and then placed into a rigid external tool and heated to composite cure temperatures at which the SMP apparatus is malleable. A pressure differential may be induced which urges the SMP apparatus to compress the composite material against the rigid external tool. When the composite material is cured, the SMP apparatus may be urged away from the cure composite material and removed from within the composite part.
摘要翻译：用于制造具有形状记忆聚合物（SMP）装置的复合部件（例如机身或内部加强件）的方法和装置，所述形状记忆聚合物（SMP）装置既可用作刚性铺叠工具又可用作气囊。 SMP设备可以被加热直到延展，成形并且然后以期望的刚性工具构造冷却。例如，可以在SMP设备中形成腔体，用于在其中嵌套组分以与复合部件共同结合或共固化。复合材料可以以刚性工具构造施加到SMP装置上，然后放置到刚性外部工具中并加热到SMP装置可延展的复合固化温度。可以诱发压力差，其促使SMP装置抵抗刚性外部工具压缩复合材料。当复合材料固化时，SMP设备可以被推离固化复合材料并从复合部件内移除。

2. 发明申请

WO2010059477A2 CARBON NANOTUBE COPOLYMERS AND COMPOSITIONS AND METHODS OF USING THE SAME 审中-公开
标题翻译：碳纳米管共聚物及其组合物及其使用方法
公开(公告)号：WO2010059477A2
公开(公告)日：2010-05-27
申请号：PCT/US2009/064020
申请日：2009-11-11
申请人： SPIRIT AEROSYSTEMS, INC. , HWANG, Wen-Fang , WU, Peter
发明人： HWANG, Wen-Fang , WU, Peter
IPC分类号： B82B1/00 , B82B3/00
CPC分类号： C08F26/06 , B82Y30/00 , B82Y40/00 , C01B32/174 , C08G73/22 , C08G83/001 , C08J5/18 , C08J2387/00 , C08L79/04 , Y10T428/2913
摘要： New carbon nanotube polymers and compositions are provided. The polymers comprise recurring blocks or units of carbon nanotubes and a compound other than a carbon nanotube. The compound is a polymeric or oligomeric block and is bonded to the carbon nanotube outer sidewall rather than to the carbon nanotube end, and is preferably a block copolymer of the compound and the carbon nanotube. The polymers can be used to prepare compositions that can be formed into products that are useful for building components present in airplanes.
摘要翻译：提供了新的碳纳米管聚合物和组合物。聚合物包含碳纳米管的重复嵌段或单元以及碳纳米管以外的化合物。化合物是聚合物或低聚物嵌段，并且结合到碳纳米管外侧壁而不是碳纳米管末端，并且优选为化合物和碳纳米管的嵌段共聚物。聚合物可用于制备可形成可用于构建存在于飞机中的组分的产物的组合物。

3. 发明申请

WO2009102531A2 COMPOSITE MATERIAL PLACEMENT 审中-公开
标题翻译：复合材料放置
公开(公告)号：WO2009102531A2
公开(公告)日：2009-08-20
申请号：PCT/US2009/031254
申请日：2009-01-16
申请人： SPIRIT AEROSYSTEMS, INC. , BLONIGEN, Bradley, John
发明人： BLONIGEN, Bradley, John
IPC分类号： B29C70/28 , B29C70/06
CPC分类号： B29C53/582 , B29C53/66 , B29C70/386 , B29K2707/04 , Y10T428/298
摘要： A method of applying a length of discontinuous fiber material to a surface comprises placing the material between a roller and the surface, urging the roller toward the surface such that the roller causes at least a portion of the length of discontinuous fiber material to engage the surface, and applying the length of discontinuous fiber material to the surface by moving one of said roller and said surface relative to the other such that the roller rolls along an application path of said surface. The application path may include one or more curves, wherein a first portion of the material lengthens relative to a second portion of the material, thereby allowing the material to lay evenly against the surface through the one or more curves without separating from the surface.
摘要翻译：将一定长度的不连续纤维材料施加到表面的方法包括将材料放置在辊和表面之间，将辊推向表面，使得辊使得不连续纤维材料的长度的至少一部分与表面接合并且通过使所述辊和所述表面中的一个相对于另一个将所述不连续纤维材料的长度施加到所述表面，使得所述辊沿着所述表面的施加路径滚动。应用路径可以包括一个或多个曲线，其中材料的第一部分相对于材料的第二部分延长，从而允许材料通过一个或多个曲线均匀地铺设在表面上而不与表面分离。

4. 发明申请

WO2009073296A2 MATERIAL PLACEMENT METHOD AND APPARATUS 审中-公开
标题翻译：材料放置方法和装置
公开(公告)号：WO2009073296A2
公开(公告)日：2009-06-11
申请号：PCT/US2008/081675
申请日：2008-10-30
申请人： SPIRIT AEROSYSTEMS, INC. , WAMPLER, Robert, Ray , ULLAH, Muhammad, Zia
发明人： WAMPLER, Robert, Ray , ULLAH, Muhammad, Zia
IPC分类号： B29C70/38 , B29C70/54
CPC分类号： B29C70/388 , B29C43/34 , B29C43/46 , B29C70/545 , B29C2043/3422 , B29C2043/467 , B29K2105/0854 , Y10T156/1348 , Y10T156/1788 , Y10T156/1795
摘要： A roller assembly for bidirectionally dispensing and compacting a strip of a material onto a surface without requiring the roller assembly to rotate 180° to dispense the material in the reverse direction. The roller assembly comprises a first guide element, a second guide element, a third guide element, and a compacting roller. When the first guide element is in a first position, the strip of the material is fed to the second guide element. When the first guide element is in a second position, the strip of the material is fed to the third guide element. The compacting roller is malleable and substantially crowned around an outer circumferential surface of the compacting roller to provide even compaction to the strip of the material.
摘要翻译：一种辊组件，用于将材料条双向分配和压实到表面上，而不需要辊组件旋转180°以沿相反方向分配材料。辊组件包括第一引导元件，第二引导元件，第三引导元件和压实辊。当第一引导元件处于第一位置时，材料条被馈送到第二引导元件。当第一引导元件处于第二位置时，材料条被馈送到第三引导元件。压实辊是可延展的并且基本上加盖在压实辊的外周表面上以提供对材料条的均匀压实。

5. 发明申请

WO2023034585A1 FEATURE INSPECTION SYSTEM 审中-公开
公开(公告)号：WO2023034585A1
公开(公告)日：2023-03-09
申请号：PCT/US2022/042491
申请日：2022-09-02
申请人： SPIRIT AEROSYSTEMS, INC. , HAYNES, Mark Davis , CORK, Glen Paul , RAO, Bharath Achyutha , BAUMFALK-LEE, John Thomas , MCKENNA, Matthew W. , GABEL, Bruce E. , BISHOP, Scott , BALANDRAN, Gregorio
发明人： HAYNES, Mark Davis , CORK, Glen Paul , RAO, Bharath Achyutha , BAUMFALK-LEE, John Thomas , MCKENNA, Matthew W. , GABEL, Bruce E. , BISHOP, Scott , BALANDRAN, Gregorio
IPC分类号： G06T7/00 , G01C11/02 , G01C11/04 , G01N21/88 , G06T7/73 , G06T7/292 , H04N5/247 , B64C39/02
摘要： A system for inspecting features of an airframe, the system including a feature inspection device configured to measure an aspect of a first feature and a tracking subsystem configured to determine a position of the feature inspection device when the feature inspection device measures the aspect of the first feature. The system is configured to determine a position of the first feature on the airframe via the feature inspection device and the tracking subsystem, the determination of the position of the first feature being independent from the measurement of the aspect of the first feature.

6. 发明申请

WO2022250789A1 METHODS OF FABRICATING MULTI-REGION U-SHAPED COMPOSITE STRUCTURES 审中-公开
公开(公告)号：WO2022250789A1
公开(公告)日：2022-12-01
申请号：PCT/US2022/023396
申请日：2022-04-05
申请人： SPIRIT AEROSYSTEMS, INC.
发明人： BLONIGEN, Bradley J. , OSBORNE, George M. , HEARNEN, Jack
IPC分类号： B29C70/30 , B29C70/38 , B29K105/08
摘要： Methods of fabricating a multi-region U-shaped composite structure, the methods comprising the steps of laying up a first composite material on a first tool piece to form a first sidewall, laying up the second composite material on a second tool piece tool to form a second sidewall, re-orienting the first tool piece and the second tool piece to a consolidation orientation, laying up the third composite material to form a nose wall, and overlapping at least a portion of the third composite material with at least a portion of the first composite material and at least a portion of the second composite material.

7. 发明申请

WO2022098653A1 METHOD AND APPARATUS FOR IN-SITU THERMAL MANAGEMENT AND HEAT TREATMENT OF ADDITIVELY MANUFACTURING COMPONENTS 审中-公开
公开(公告)号：WO2022098653A1
公开(公告)日：2022-05-12
申请号：PCT/US2021/057730
申请日：2021-11-02
申请人： SPIRIT AEROSYSTEMS, INC.
发明人： NASSERRAFI, Rahbar , TOIVONEN, Paul R. , HICKS, JR., Gerald Eugene , KLENOSKY, Daniel R.
IPC分类号： B22F10/362 , B22F10/22 , B22F10/368 , B22F10/64 , B22F12/20
摘要： Methods for in-situ solution heat treating an additively manufactured metallic component in order to increase the mechanical properties thereof and systems to perform the same. The method can include depositing filler material on a substrate forming a deposition layer, measuring the temperature of a heat affected zone corresponding to the deposition layer, and solution heat treating the deposition layer subsequent to the depositing and proximate to the deposition head. The solution heat treating can include heating the deposition layer to a solution temperature so as to achieve solution heat treatment and controlling the cooling rate of the deposition layer to at or above the critical cooling rate of the filler material until a target temperature is reached. Optionally, the method can include inducing an electron flow in the deposition layer to electromagnetically stir molten filler material in the heat affected zone.

8. 发明申请

WO2021194765A1 SYSTEM AND METHOD FOR FORMING INTEGRAL FLANGE IN COMPOSITE LAMINATE STRUCTURE AFTER LAYUP 审中-公开
公开(公告)号：WO2021194765A1
公开(公告)日：2021-09-30
申请号：PCT/US2021/022050
申请日：2021-03-12
申请人： SPIRIT AEROSYSTEMS, INC.
发明人： WADSWORTH, Mark Anthony
IPC分类号： F16L23/024 , B64G1/22 , B32B38/18 , B29C53/043 , B29C70/345
摘要： A system and method for forming an integral flange in an end portion of a composite laminate structure, such as an aerospace or other vehicle structure. First and second tool components cooperate to support the structure during a layup process, with the second tool component imparting an initial angle to the end portion. A third tool component includes a male radius positioned at an apex of the initial angle. A heater heats a succession of localized areas along the end portion to lower a viscosity of the resin. A roller applies pressure to the succession of localized areas after each is heated so as to push them around and against the third tool component to form a flange angle and the integral flange. The heater and the roller may make multiple passes along the end portion, with the roller angle increasing with each pass until the flange angle is achieved.

9. 发明申请

WO2021096774A1 INTEGRATED PICK, PLACE, AND FORMING APPARATUS AND METHOD FOR COMPOSITE CHARGES OVER COMPLEX GEOMETRIES 审中-公开
公开(公告)号：WO2021096774A1
公开(公告)日：2021-05-20
申请号：PCT/US2020/059355
申请日：2020-11-06
申请人： SPIRIT AEROSYSTEMS, INC.
发明人： PADOVANO, Christopher James , BERGMANN, Blaise Francis , MORROW, Christopher John , HORNER, Allison Lynne , FERRELL, Benjamin Wayne
IPC分类号： B64F5/10 , B64F5/50 , B29C70/06
摘要： An apparatus for picking, placing, and forming a composite charge over a complex geometry tool comprises a first frame, a second frame, and a plurality of dynamic mechanisms. The first frame is formed from rigid material and includes a first frame member that forms at least a rectangular perimeter. The second frame is formed from flexible material and includes a second frame member that forms at least a rectangular perimeter. Each dynamic mechanism is connected to the first frame and the second frame and located along the perimeters of the first frame and the second frame. Each dynamic mechanism includes a length-variable component positioned between the first frame and the second frame, with at least a portion of the dynamic mechanisms configured to vary a length of the length-variable component for the second frame member to conform to the shape of the complex geometry tool.

10. 发明申请

WO2012064446A2 RECONFIGURABLE SHAPE MEMORY POLYMER TOOLING SUPPORTS 审中-公开
公开(公告)号：WO2012064446A2
公开(公告)日：2012-05-18
申请号：PCT/US2011/055569
申请日：2011-10-10
申请人： SPIRIT AEROSYSTEMS, INC. , BARNELL, Thomas , EVERHART, Joel , HUELSKAMP, Scott , PELLEY, Bryan
发明人： BARNELL, Thomas , EVERHART, Joel , HUELSKAMP, Scott , PELLEY, Bryan
IPC分类号： B29C61/06 , B29C39/40
CPC分类号： B29C33/485 , B29C33/046
摘要： A method and support apparatus for providing structural support to a mold or mandrel, such as a shape memory polymer (SMP) apparatus configured for shaping a composite part. The support apparatus may comprise a rigid structural member and a plurality of SMP cells attached thereto and configured to inflate or deploy in a malleable state toward and against a surface of the SMP apparatus, mold, or mandrel. Then the SMP cells may be returned to a rigid state while still pressed against this surface, thereby providing structural support when composite material is applied to an opposite surface of the SMP apparatus, mold, or mandrel. After the composite material is cured into the finished composite part, the SMP cells may be deflated or otherwise collapse toward the structural member to provide enough clearance to be removed from the cured composite part.

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