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    MULTI-AXIAL LAMINATE COMPOSITE STRUCTURES AND METHODS OF FORMING THE SAME
    1.
    发明申请
    MULTI-AXIAL LAMINATE COMPOSITE STRUCTURES AND METHODS OF FORMING THE SAME 审中-公开
    多轴层压复合结构及其形成方法

    公开(公告)号：WO2006121505A1

    公开(公告)日：2006-11-16

    申请号：PCT/US2006/009730

    申请日：2006-03-16

    Applicant: THE BOEING COMPANY ,  KISMARTON, Max, U.

    Inventor： KISMARTON, Max, U.

    IPC: B29C70/08 ,  B29C70/20 ,  B29C70/22 ,  B29C70/24 ,  B64C1/00

    CPC classification number: B29C70/083 ,  B29C70/202 ,  B29C70/207 ,  B29C70/226 ,  B29C70/228 ,  B29C70/24 ,  B29L2031/3076 ,  B29L2031/3082 ,  B29L2031/3085 ,  Y02T50/43 ,  Y10T428/24994

    Abstract: Composite laminate structures and methods of forming the same are disclosed. In one embodiment, the structure includes a first bidirectional layer (112) having a first portion (117) that includes parallel reinforcement fibers oriented at a first angle relative to a first direction and a second portion (114) that includes parallel reinforcement fibers oriented at a second angle relative to the first direction. The structure further includes a second bidirectional layer (118) having a first portion (119) that includes parallel reinforcement fibers oriented at a third angle relative to the first direction and a second portion (120) that includes parallel reinforcement fibers oriented at a fourth angle relative to the first direction. At least one unidirectional (116) layer having a plurality of parallel reinforcement fibers is coupled to at least one of the first bidirectional layer and the second bidirectional layer.

    Abstract translation: 公开了复合层压结构及其形成方法。 在一个实施例中，该结构包括具有第一部分（117）的第一双向层（112），该第一部分包括相对于第一方向以第一角度定向的平行增强纤维和包括平行增强纤维的第二部分， 相对于第一方向的第二角度。 该结构还包括具有第一部分（119）的第二双向层（118），该第一部分包括相对于第一方向以第三角度定向的平行增强纤维和包括以第四角度定向的平行增强纤维的第二部分（120） 相对于第一个方向。 具有多个平行增强纤维的至少一个单向（116）层被耦合到第一双向层和第二双向层中的至少一个。

    DIAMOND SHAPED WINDOW FOR A COMPOSITE AND/OR METALLIC AIRFRAME
    4.
    发明申请
    DIAMOND SHAPED WINDOW FOR A COMPOSITE AND/OR METALLIC AIRFRAME 审中-公开
    用于复合材料和/或金属空气弹性的金刚石形状的窗户

    公开(公告)号：WO2012121825A1

    公开(公告)日：2012-09-13

    申请号：PCT/US2012/023819

    申请日：2012-02-03

    Applicant: THE BOEING COMPANY ,  KISMARTON, Max U.

    Inventor： KISMARTON, Max U.

    IPC: B64C1/14

    CPC classification number: B64F5/0009 ,  B29C70/30 ,  B64C1/068 ,  B64C1/1484 ,  B64C1/1492 ,  B64C2001/0072 ,  Y02T50/43 ,  Y10T83/04 ,  Y10T156/1064

    Abstract: An aircraft fuselage may include a barrel section (34) having a side region. The fuselage may include a first cutout (52a) and a second cutout (52b) formed in the side region in side-by-side relation to one another. The fuselage may provide a direct load path extending along the barrel section. The load path may extend substantially continuously from a lower portion of the side region generally under the first cutout to an upper portion of the side region generally over the second cutout.

    Abstract translation: 飞机机身可以包括具有侧面区域的桶部分（34）。 机身可以包括彼此并排地形成在侧区域中的第一切口（52a）和第二切口（52b）。 机身可以提供沿着筒部延伸的直接负载路径。 负载路径可以从大体上在第一切口下方的侧面区域的下部基本上连续地延伸到大致在第二切口上的侧面区域的上部。

    ROTOR APPARATUS AND METHODS FOR VERTICAL LIFT AIRCRAFT
    5.
    发明申请
    ROTOR APPARATUS AND METHODS FOR VERTICAL LIFT AIRCRAFT 审中-公开
    用于垂直升降飞机的转子装置和方法

    公开(公告)号：WO2008054351A3

    公开(公告)日：2008-11-27

    申请号：PCT/US2006029133

    申请日：2006-07-26

    Applicant: BOEING CO ,  KISMARTON MAX U

    Inventor： KISMARTON MAX U

    IPC: B64C27/32

    CPC classification number: B64C27/32 ,  B64C27/48 ,  B64C27/51

    Abstract: Rotor apparatus and methods for vertical lift aircraft are disclosed. In one embodiment, a bearing assembly (130) adapted for rotatably coupling a rotor blade to a support member includes an inner housing (138) annularly disposed about a portion of the support member, an outer housing (136) annularly disposed about at least part of the inner housing and is rotatably coupled to the inner housing by an annular bearing device, and a flexible member (140) adapted to be coupled to the support member and including an engagement portion adapted to engage the outer housing and to at least partially relax a side force exerted on the annular bearing device by a bending of at least one of the rotor blade and the support member.

    Abstract translation: 公开了用于垂直升降飞机的转子装置和方法。 在一个实施例中，适于将转子叶片可旋转地联接到支撑构件的轴承组件（130）包括围绕所述支撑构件的一部分环形地设置的内壳体（138），外壳体（136），其围绕至少部分 并且通过环形轴承装置可旋转地联接到所述内壳体，以及柔性构件（140），其适于联接到所述支撑构件并且包括接合部分，所述接合部分适于接合所述外壳体并且至少部分地松弛 通过转子叶片和支撑构件中的至少一个的弯曲施加在环形轴承装置上的侧向力。

    CONDUCTING-FIBER DEICING SYSTEMS AND METHODS
    6.
    发明申请
    CONDUCTING-FIBER DEICING SYSTEMS AND METHODS 审中-公开
    导电纤维检测系统和方法

    公开(公告)号：WO2008057064A3

    公开(公告)日：2008-10-02

    申请号：PCT/US2006028943

    申请日：2006-07-26

    Applicant: BOEING CO ,  KISMARTON MAX U

    Inventor： KISMARTON MAX U

    IPC: B64D15/12 ,  B64D15/14

    CPC classification number: H05B3/28 ,  B64D15/14

    Abstract: Conducting- fiber deicing systems and methods are disclosed. In one embodiment, an assembly includes a surface (128) subject to an accumulation of ice, the surface (128) at least partially including a heating portion (152) having a layer (154) of multi-directional electrically-conductive fibers formed between first and second non-electrically conductive layers (156, 158). The layer of electrically-conductive fibers is coupled to a power supply member (160) and is adapted to conduct an electrical current such that the layer (154) of electrically-conductive fibers, and at least one of the first and second non-electrically conductive layers (156, 158) of the heating portion (152), are raised to an elevated temperature to at least partially inhibit the, accumulation of ice on the surface.

    Abstract translation: 公开了导电纤维除冰系统和方法。 在一个实施例中，组件包括经受冰积聚的表面（128），所述表面（128）至少部分地包括加热部分（152），所述加热部分具有多向导电纤维层（154） 第一和第二非导电层（156,158）。 导电纤维层被耦合到电源构件（160），并且适于传导电流，使得导电纤维的层（154）以及第一和第二非电 加热部分（152）的导电层（156,158）被升高到升高的温度以至少部分地抑制冰在表面上的积聚。

    LIGHTWEIGHT AIRCRAFT PASSENGER SEAT WITH COMPOSITE CONSTRUCTION
    8.
    发明申请
    LIGHTWEIGHT AIRCRAFT PASSENGER SEAT WITH COMPOSITE CONSTRUCTION 审中-公开
    轻型飞机乘客座椅与复合结构

    公开(公告)号：WO2007136578A2

    公开(公告)日：2007-11-29

    申请号：PCT/US2007/011396

    申请日：2007-05-10

    Applicant: THE BOEING COMPANY ,  BOREN, Kelly, L. ,  KISMARTON, Max, U. ,  RETZ, Kevin, M.

    Inventor： BOREN, Kelly, L. ,  KISMARTON, Max, U. ,  RETZ, Kevin, M.

    IPC: B60N2/90

    CPC classification number: B64D11/06 ,  B60N2/682 ,  B60N2/686 ,  B60N2/914 ,  B60N2/995 ,  B64D11/0649 ,  Y02T50/46

    Abstract: An aircraft seat assembly configured in accordance with an example embodiment of the invention utilizes composite materials to achieve significant weight savings relative to conventional seat designs. The seat assembly includes a lightweight composite support structure, a lightweight composite seat base, and a seat back assembly that employs a lightweight inner frame. The seat cushion and the seat back cushion may utilize a sealed pneumatic element that self-inflates to provide increased air cushioning during flight. The seat assembly can leverage inexpensive manufacturing techniques such that the seat assembly can be economically produced for use as an economy class seat.

    Abstract translation: 根据本发明的示例性实施例构造的飞行器座椅组件利用复合材料相对于传统座椅设计实现显着的重量节省。 座椅组件包括轻质复合支撑结构，轻质复合座椅底座和采用轻质内框架的座椅靠背组件。 座垫和座椅靠背垫可以利用密封的气动元件，其自动充气以在飞行期间提供增加的空气缓冲。 座椅组件可以利用廉价的制造技术，使得座椅组件可经济地生产用作经济舱座椅。

    APPARATUS AND METHODS FOR FABRICATION OF COMPOSITE COMPONENTS
    9.
    发明申请
    APPARATUS AND METHODS FOR FABRICATION OF COMPOSITE COMPONENTS 审中-公开
    用于制造复合组分的装置和方法

    公开(公告)号：WO2007046914A1

    公开(公告)日：2007-04-26

    申请号：PCT/US2006/029171

    申请日：2006-07-26

    Applicant: THE BOEING COMPANY ,  KISMARTON, Max, U.

    Inventor： KISMARTON, Max, U.

    IPC: B29C70/44 ,  B30B5/02

    CPC classification number: B29C70/446 ,  B29C33/505 ,  B29C43/3642 ,  B29C70/44 ,  B29C2043/3649 ,  B29K2105/0854 ,  B29L2031/08 ,  B29L2031/3076

    Abstract: Apparatus and methods for fabrication of composite components (216) are disclosed. In one embodiment, an apparatus for fabricating a component from a composite material includes a containment member (202) having an internal volume adapted to receive the composite material, and a lid member (208) . An expandable member (205) is disposed within the internal volume adjacent to the composite material, the expandable member being inflatable within the internal volume and adapted to apply an elevated pressure against the composite material that urges the composite material against at least one of the containment member and the lid member. The containment member, the lid member, and the expandable member are further adapted to withstand at least one of the elevated pressure and an elevated temperature suitable for curing the composite material .

    Abstract translation: 公开了用于制造复合部件（216）的装置和方法。 在一个实施例中，用于从复合材料制造部件的装置包括具有适于容纳复合材料的内部容积的容纳构件（202）和盖构件（208）。 可膨胀构件（205）设置在与复合材料相邻的内部体积内，可膨胀构件可在内部容积内充气，并且适于对组合材料施加升高的压力，所述复合材料抵抗至少一个容纳物 构件和盖构件。 容纳构件，盖构件和可膨胀构件还适于承受适于固化复合材料的升高的压力和升高的温度中的至少一个。

    MULTI-AXIAL LAMINATE COMPOSITE STRUCTURES AND METHODS OF FORMING THE SAME
    10.
    发明申请
    MULTI-AXIAL LAMINATE COMPOSITE STRUCTURES AND METHODS OF FORMING THE SAME 审中-公开
    多轴层压复合结构及其形成方法

    公开(公告)号：WO2006121505A8

    公开(公告)日：2007-01-25

    申请号：PCT/US2006009730

    申请日：2006-03-16

    Applicant: BOEING CO ,  KISMARTON MAX U

    Inventor： KISMARTON MAX U

    IPC: B29C70/08 ,  B29C70/20 ,  B29C70/22 ,  B29C70/24 ,  B64C1/00

    CPC classification number: B29C70/083 ,  B29C70/202 ,  B29C70/207 ,  B29C70/226 ,  B29C70/228 ,  B29C70/24 ,  B29L2031/3076 ,  B29L2031/3082 ,  B29L2031/3085 ,  Y02T50/433 ,  Y10T428/24994

    Abstract: Composite laminate structures and methods of forming the same are disclosed. In one embodiment, the structure includes a first bidirectional layer (112) having a first portion (117) that includes parallel reinforcement fibers oriented at a first angle relative to a first direction and a second portion (114) that includes parallel reinforcement fibers oriented at a second angle relative to the first direction. The structure further includes a second bidirectional layer (118) having a first portion (119) that includes parallel reinforcement fibers oriented at a third angle relative to the first direction and a second portion (120) that includes parallel reinforcement fibers oriented at a fourth angle relative to the first direction. At least one unidirectional (116) layer having a plurality of parallel reinforcement fibers is coupled to at least one of the first bidirectional layer and the second bidirectional layer.

    Abstract translation: 公开了复合层压结构及其形成方法。 在一个实施例中，该结构包括具有第一部分（117）的第一双向层（112），该第一部分包括相对于第一方向以第一角度定向的平行增强纤维和包括平行增强纤维的第二部分， 相对于第一方向的第二角度。 该结构还包括具有第一部分（119）的第二双向层（118），该第一部分包括相对于第一方向以第三角度定向的平行增强纤维和包括以第四角度定向的平行增强纤维的第二部分（120） 相对于第一个方向。 具有多个平行增强纤维的至少一个单向（116）层被耦合到第一双向层和第二双向层中的至少一个。

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