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    • 5. 发明申请
    • ROTOR APPARATUS AND METHODS FOR VERTICAL LIFT AIRCRAFT
    • 用于垂直升降飞机的转子装置和方法
    • WO2008054351A3
    • 2008-11-27
    • PCT/US2006029133
    • 2006-07-26
    • BOEING COKISMARTON MAX U
    • KISMARTON MAX U
    • B64C27/32
    • B64C27/32B64C27/48B64C27/51
    • 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.
    • 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。
    • 6. 发明申请
    • CONDUCTING-FIBER DEICING SYSTEMS AND METHODS
    • 导电纤维检测系统和方法
    • WO2008057064A3
    • 2008-10-02
    • PCT/US2006028943
    • 2006-07-26
    • BOEING COKISMARTON MAX U
    • KISMARTON MAX U
    • B64D15/12B64D15/14
    • H05B3/28B64D15/14
    • 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.
    • 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。
    • 9. 发明申请
    • APPARATUS AND METHODS FOR FABRICATION OF COMPOSITE COMPONENTS
    • 用于制造复合组分的装置和方法
    • WO2007046914A1
    • 2007-04-26
    • PCT/US2006/029171
    • 2006-07-26
    • THE BOEING COMPANYKISMARTON, Max, U.
    • KISMARTON, Max, U.
    • B29C70/44B30B5/02
    • B29C70/446B29C33/505B29C43/3642B29C70/44B29C2043/3649B29K2105/0854B29L2031/08B29L2031/3076
    • 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 .
    • 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。