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    RETAINER PLATE
    1.
    发明申请
    RETAINER PLATE 有权
    保留板

    公开(公告)号：US20150110634A1

    公开(公告)日：2015-04-23

    申请号：US14520683

    申请日：2014-10-22

    Applicant: ROLLS-ROYCE PLC

    Inventor： Matthew Paul JEVONS

    IPC: F04D29/34 ,  F04D19/00

    CPC classification number: F04D29/34 ,  F01D5/3007 ,  F01D5/3015 ,  F01D5/326 ,  F04D19/002 ,  F05D2260/30 ,  F05D2300/6012 ,  F05D2300/603

    Abstract: A retainer plate is provided for retaining a dovetail root of a fan blade of a gas turbine engine in a corresponding axially-extending slot in the rim of a fan disc. In use, the plate locates in a cavity formed at an end of the slot such that a first side of the plate is arranged for contact with an axial end face of the dovetail root and an opposite second side of the plate is arranged for contact with an abutment surface of the cavity to limit axial movement of the root along the slot. The retainer plate is formed from fibre-reinforced composite material, at least a portion of the composite material being reinforced by 3D-woven fibre tows.

    Abstract translation: 提供了一种保持板，用于将燃气涡轮发动机的风扇叶片的燕尾根保持在风扇盘的边缘中的对应的轴向延伸槽中。 在使用中，板位于形成在槽的端部处的空腔中，使得板的第一侧布置成与燕尾根的轴向端面接触，并且板的相对的第二侧被布置成与 空腔的邻接表面以限制根部沿着槽的轴向运动。 保持板由纤维增强复合材料形成，复合材料的至少一部分由3D织物纤维束加强。

    RETAINER PLATE
    4.
    发明申请
    RETAINER PLATE 有权
    保留板

    公开(公告)号：US20150093248A1

    公开(公告)日：2015-04-02

    申请号：US14481107

    申请日：2014-09-09

    Applicant: ROLLS-ROYCE PLC

    Inventor： Ian Colin Deuchar CARE ,  Matthew Paul JEVONS

    IPC: F04D29/34 ,  F04D19/00

    CPC classification number: F04D29/34 ,  F01D5/3015 ,  F01D5/3092 ,  F01D5/323 ,  F04D19/002 ,  F05D2250/283 ,  F05D2260/80 ,  F05D2300/603 ,  F05D2300/612 ,  Y02T50/672

    Abstract: A retainer plate is provided for retaining a dovetail root of a fan blade of a gas turbine engine in a corresponding axially-extending slot in the rim of a fan disc. In use, the plate locates in a cavity formed at an end of the slot such that a first side of the plate is arranged for contact with an axial end face of the dovetail root and an opposite second side of the plate is arranged for contact with an abutment surface of the cavity to limit axial movement of the root along the slot. The retainer plate is a unitary component and has a layered structure including a first layer at the first side of the plate, a second layer at the second side of the plate, and an intermediate layer between the first and the second layers.

    Abstract translation: 提供了一种保持板，用于将燃气涡轮发动机的风扇叶片的燕尾根保持在风扇盘的边缘中的对应的轴向延伸槽中。 在使用中，板位于形成在槽的端部处的空腔中，使得板的第一侧布置成与燕尾根的轴向端面接触，并且板的相对的第二侧被布置成与 空腔的邻接表面以限制根部沿着槽的轴向运动。 保持板是整体部件，并且具有包括在板的第一侧的第一层，在板的第二侧的第二层以及第一和第二层之间的中间层的层状结构。

    COMPOSITE STRUCTURE AND A METHOD OF FABRICATING THE SAME
    6.
    发明申请
    COMPOSITE STRUCTURE AND A METHOD OF FABRICATING THE SAME 审中-公开
    复合结构及其制造方法

    公开(公告)号：US20150360451A1

    公开(公告)日：2015-12-17

    申请号：US14718598

    申请日：2015-05-21

    Applicant: ROLLS-ROYCE PLC

    Inventor： Matthew Paul JEVONS

    IPC: B32B27/12 ,  F01D5/28 ,  B32B27/40 ,  B32B5/02 ,  B29C70/02 ,  B29C65/48

    CPC classification number: F01D5/282 ,  B29C65/4835 ,  B29C70/026 ,  B29C70/086 ,  B29K2075/00 ,  B29L2009/005 ,  B29L2031/085 ,  B32B25/08 ,  B32B25/14 ,  B32B27/065 ,  B32B2262/106 ,  B32B2603/00 ,  Y10T442/3683

    Abstract: There is disclosed a method of fabricating a composite structure (6). The method comprises the steps of: providing a pair of preforms (1, 2), each comprising a plurality of reinforcing fibres (3); providing an intermediate layer (4) of resiliently deformable material between said s preforms (1,2) to space said preforms apart from one another such that each preform (1,2) bears against a respective side (5) of the intermediate layer (4); providing a curable matrix material around said fibres (3); and curing said matrix material to form said plastic composite structure (6). Also disclosed is a composite structure (6) having at least two layers of fibre-reinforced plastic (1,2) which are bonded to respective sides (5) of an intermediate layer (4) of resiliently deformable material, the intermediate layer (4) being arranged to space the two layers of fibre-reinforced plastic (1,2) from one another.

    Abstract translation: 公开了一种制造复合结构（6）的方法。 该方法包括以下步骤：提供一对预成型件（1,2），每个包括多个增强纤维（3）; 在所述预成型件（1,2）之间提供可弹性变形材料的中间层（4），以使所述预成型件彼此分开，使得每个预制件（1,2）抵靠中间层的相应侧（5） 4）; 在所述纤维（3）周围提供可固化的基质材料; 并固化所述基质材料以形成所述塑料复合结构（6）。 还公开了具有至少两层纤维增强塑料（1,2）的复合结构（6），其结合到可弹性变形材料的中间层（4）的相应侧面（5），中间层（4） ）被布置成将两层纤维增强塑料（1,2）彼此间隔开。

    METHOD OF MANUFACTURING A COMPOSITE MATERIAL INCLUDING A THERMOPLASTIC COATED REINFORCING ELEMENT
    7.
    发明申请
    METHOD OF MANUFACTURING A COMPOSITE MATERIAL INCLUDING A THERMOPLASTIC COATED REINFORCING ELEMENT 有权
    制造复合材料的方法，包括热塑性涂层增强元件

    公开(公告)号：US20140308136A1

    公开(公告)日：2014-10-16

    申请号：US14230546

    申请日：2014-03-31

    Applicant: ROLLS-ROYCE PLC

    Inventor： Matthew Paul JEVONS

    IPC: F01D5/14 ,  B05D1/02 ,  B05D1/18 ,  B29C70/40

    CPC classification number: F01D5/147 ,  B05D1/02 ,  B05D1/18 ,  B29C70/24 ,  B29C70/40 ,  B29C70/887 ,  B29K2101/12 ,  B29L2031/08 ,  B29L2031/7504 ,  Y10T428/24331

    Abstract: A method of through-thickness reinforcing a laminated material is disclosed, in which a reinforcing element is coated with a thermoplastic layer. The reinforcing element is inserted into a base material, and a matrix material, such as a polymeric, is included in the base material. The combination is then cured, or heated, such that the thermoplastic layer and the matrix material diffuse into each other, thereby forming an interphase region around the reinforcing element. This interphase region helps to prevent cracks from propagating from the reinforcing element.

    Abstract translation: 公开了一种通过厚度加强层压材料的方法，其中增强元件涂覆有热塑性层。 将增强元件插入基材中，并且基体材料（例如聚合物）中包含基体材料。 然后将组合物固化或加热，使得热塑性层和基质材料彼此扩散，从而在增强元件周围形成界面区域。 该相间区域有助于防止裂纹从加强元件传播。

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