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1. 发明授权

US08419886B2 Method of manufacturing composite parts 有权
标题翻译：复合零件的制造方法
公开(公告)号：US08419886B2
公开(公告)日：2013-04-16
申请号：US13138551
申请日：2010-03-01
申请人： Simon Astwood , John Jacobs , Matthew Hocking , Jago Pridie
发明人： Simon Astwood , John Jacobs , Matthew Hocking , Jago Pridie
IPC分类号： B29C65/00 , B32B37/00
CPC分类号： B29C70/32 , B29C70/44 , B29C70/446
摘要： A method of manufacturing two or more composite parts, the method comprising: assembling the composite parts on a mandrel by laying a series of layers of bands of composite material onto the mandrel with a placement machine,—rotating the mandrel as the bands are laid onto the mandrel; attaching two or more debulk frames (10, 11) to the mandrel between opposed edges of the composite parts after the composite parts have been assembled; wrapping the mandrel, debulk frames (10, 11) and composite parts in a debulk bag; heating the composite parts,—forming a vacuum between the mandrel and the debulk bag so that the debulk bag is sucked into voids between the debulk frames and the heated composite parts and progressively presses against the heated composite parts whereby excess material is squeezed by the debulk bag towards their opposed edges; and removing the debulk bag and the composite parts from the mandrel.
摘要翻译：一种制造两个或多个复合部件的方法，所述方法包括：通过将放置机器的一系列复合材料带放置在所述心轴上来将所述复合部件组装在心轴上，当将所述带放置在所述带上时旋转所述心轴心轴在复合部件组装之后，在复合部件的相对边缘之间将两个或更多个去磁框架（10,11）连接到心轴上; 将心轴，减压框架（10,11）和复合部件包裹在减压袋中; 加热复合部件，在心轴和去毛刺袋之间形成真空，使得去毛刺袋被吸入脱泡框架和被加热的复合部件之间的空隙中，并逐渐地压靠加热的复合部件，由此多余的材料被除垢剂挤压袋子朝向相对的边缘; 并从芯棒上去除去毛刺袋和复合部件。

2. 发明授权

US10016949B2 Method of moulding a charge 有权
公开(公告)号：US10016949B2
公开(公告)日：2018-07-10
申请号：US12733443
申请日：2008-09-29
申请人： Jago Pridie
发明人： Jago Pridie
IPC分类号： B29C70/44 , B29C43/36 , B29C70/54
CPC分类号： B29C70/44 , B29C43/3642 , B29C70/542 , B29C2043/3644 , Y02T50/43 , Y10T428/24132
摘要： A method of molding a charge (12) during the manufacture of a composite part. The method comprises: placing the charge and a diaphragm (4) on a male tool, the charge having a first part (12a) which is positioned above a top of the male tool (2) and a second part (12b, 12c) which projects to one side of the maletool; and progressively deforming the second part of the charge against a side of the male tool by applying a pressure difference across the diaphragm and stretching the diaphragm over the male tool as the pressure difference is applied. The diaphragm has a tensile modulus in the plane of the diaphragm which is greater than 5 MPa. Optionally a support membrane may be positioned on a opposite sides of the charge. In the case where a support membrane is used, then the diaphragm has a stiffness in the planeof the diaphragm which is higher than the stiffness of the support membrane in the plane of the support membrane.

3. 发明申请

US20090197050A1 METHOD OF MANUFACTURING COMPOSITE PART 审中-公开
标题翻译：制造复合材料部分的方法
公开(公告)号：US20090197050A1
公开(公告)日：2009-08-06
申请号：US12303422
申请日：2007-07-11
申请人： Jago Pridie
发明人： Jago Pridie
IPC分类号： B29C59/02 , B32B1/00
CPC分类号： B29C70/44 , Y10T428/24628
摘要： A method of manufacturing a composite part, the method comprising: placing a charge on a male tool having a convex surface region; debulking the charge on the male tool by applying pressure to the charge, the applied pressure varying over the surface of the charge so as to be intensified where the charge engages the convex surface region of the male tool; and curing the charge on a female tool having a concave surface region. The charge is formed and debulked in a series of stages to form a laminate. The charge is formed at a first temperature T1; debulked at a second temperature T2; and cured at a third temperature T3, wherein T1
摘要翻译：一种制造复合部件的方法，所述方法包括：将电荷放置在具有凸表面区域的阳工具上; 通过对电荷施加压力来减压阳极工具上的电荷，施加的压力在电荷表面上变化，以便在电荷与阳性工具的凸表面区域接合的地方加强; 并且在具有凹表面区域的阴工具上固化电荷。形成电荷并在一系列的阶段中减压以形成层压体。电荷形成在第一温度T1; 在第二温度T2下减压; 并在第三温度T3下固化，其中T1

4. 发明申请

US20120000597A1 Method of manufacturing composite parts 有权
标题翻译：复合零件的制造方法
公开(公告)号：US20120000597A1
公开(公告)日：2012-01-05
申请号：US13138551
申请日：2010-03-01
申请人： Simon Astwood , John Jacobs , Matthew Hocking , Jago Pridie
发明人： Simon Astwood , John Jacobs , Matthew Hocking , Jago Pridie
IPC分类号： B65H81/06
CPC分类号： B29C70/32 , B29C70/44 , B29C70/446
摘要： A method of manufacturing two or more composite parts, the method comprising: assembling the composite parts on a mandrel by laying a series of layers of bands of composite material onto the mandrel with a placement machine,—rotating the mandrel as the bands are laid onto the mandrel; attaching two or more debulk frames (10, 11) to the mandrel between opposed edges of the composite parts after the composite parts have been assembled; wrapping the mandrel, debulk frames (10, 11) and composite parts in a debulk bag; heating the composite parts,—forming a vacuum between the mandrel and the debulk bag so that the debulk bag is sucked into voids between the debulk frames and the heated composite parts and progressively presses against the heated composite parts whereby excess material is squeezed by the debulk bag towards their opposed edges; and removing the debulk bag and the composite parts from the mandrel.
摘要翻译：一种制造两个或多个复合部件的方法，所述方法包括：通过将放置机器的一系列复合材料带放置在所述心轴上来将所述复合部件组装在心轴上，当将所述带放置在所述带上时旋转所述心轴心轴在复合部件组装之后，在复合部件的相对边缘之间将两个或更多个去磁框架（10,11）连接到心轴上; 将心轴，减压框架（10,11）和复合部件包裹在减压袋中; 加热复合部件，在心轴和去毛刺袋之间形成真空，使得去毛刺袋被吸入脱泡框架和被加热的复合部件之间的空隙中，并逐渐地压靠加热的复合部件，由此多余的材料被除垢剂挤压袋子朝向相对的边缘; 并从芯棒上去除去毛刺袋和复合部件。

5. 发明申请

US20100310818A1 METHOD OF MOULDING A CHARGE 有权
标题翻译：模拟电荷的方法
公开(公告)号：US20100310818A1
公开(公告)日：2010-12-09
申请号：US12733443
申请日：2008-09-29
申请人： Jago Pridie
发明人： Jago Pridie
IPC分类号： B32B5/12 , B29C51/10
CPC分类号： B29C70/44 , B29C43/3642 , B29C70/542 , B29C2043/3644 , Y02T50/43 , Y10T428/24132
摘要： A method of moulding a charge (12) during the manufacture of a composite part. The method comprises: placing the charge and a diaphragm (4) on a male tool, the charge having a first part (12a) which is positioned above a top of the male tool (2) and a second part (12b, 12c) which projects to one side of the maletool; and progressively deforming the second part of the charge against a side of the male tool by applying a pressure difference across the diaphragm and stretching the diaphragm over the male tool as the pressure difference is applied. The diaphragm has a tensile modulus in the plane of the diaphragm which is greater than 5 MPa. Optionally a support membrane may be positioned on a opposite sides of the charge. In the case where a support membrane is used, then the diaphragm has a stiffness in the planeof the diaphragm which is higher than the stiffness of the support membrane in the plane of the support membrane.
摘要翻译：在制造复合部件期间模制电荷（12）的方法。该方法包括：将电荷和隔膜（4）放置在阳性工具上，电荷具有位于阳性工具（2）的顶部上方的第一部分（12a）和第二部分（12b，12c），第二部分项目到男主角的一边; 并且通过在隔膜上施加压力差并且在施加压力差时将隔膜拉伸在阳性工具上，使电荷的第二部分逐渐变形为阳性工具的侧面。隔膜在隔膜的平面内具有大于5MPa的拉伸模量。任选地，支撑膜可以位于电荷的相对侧上。在使用支撑膜的情况下，隔膜在隔膜的平面中具有比支撑膜平面中的支撑膜的刚度高的刚度。

6. 发明申请

US20060162859A1 Method and apparatus for joining aircraft components 有权
标题翻译：用于加入飞机部件的方法和装置
公开(公告)号：US20060162859A1
公开(公告)日：2006-07-27
申请号：US10528907
申请日：2003-09-25
申请人： Jago Pridie
发明人： Jago Pridie
IPC分类号： B32B37/00 , B29C65/00
CPC分类号： B64C3/26 , B29C65/483 , B29C65/488 , B29C65/4885 , B29C65/544 , B29C66/02242 , B29C66/02245 , B29C66/721 , B29C66/7212 , B29C66/73161 , B29L2031/3085 , Y10T156/1702 , B29K2307/04
摘要： The surface of a moulding tool, for receiving a first aircraft component, for example a spar, is shaped to correspond to the surface of a second aircraft component, for example a wing skin. A gap is defined between the tool and the first component. Resin is drawn into the gap by a suction pump. The resin fills the gap and cures to forma shim. The first and second components, which are in the form of composite material structures, are then joined together without any significant voids being formed therebetween.
摘要翻译：用于接收第一飞行器部件（例如翼梁）的模制工具的表面被成形为对应于第二飞行器部件（例如机翼皮肤）的表面。在工具和第一部件之间定义间隙。树脂被抽吸泵吸入间隙。树脂填充间隙并固化形成垫片。然后将复合材料结构形式的第一和第二组分连接在一起，而不会在其间形成任何明显的空隙。

7. 发明授权

US07883657B2 Method for joining aircraft components 有权
标题翻译：加装飞机部件的方法
公开(公告)号：US07883657B2
公开(公告)日：2011-02-08
申请号：US10528907
申请日：2003-09-25
申请人： Jago Pridie
发明人： Jago Pridie
IPC分类号： B29C45/14 , B29C65/00
CPC分类号： B64C3/26 , B29C65/483 , B29C65/488 , B29C65/4885 , B29C65/544 , B29C66/02242 , B29C66/02245 , B29C66/721 , B29C66/7212 , B29C66/73161 , B29L2031/3085 , Y10T156/1702 , B29K2307/04
摘要： The surface of a moulding tool, for receiving a first aircraft component, for example a spar, is shaped to correspond to the surface of a second aircraft component, for example a wing skin. A gap is defined between the tool and the first component. Resin is drawn into the gap by a suction pump. The resin fills the gap and cures to forma shim. The first and second components, which are in the form of composite material structures, are then joined together without any significant voids being formed therebetween.
摘要翻译：用于接收第一飞行器部件（例如翼梁）的模制工具的表面被成形为对应于第二飞行器部件（例如机翼皮肤）的表面。在工具和第一部件之间定义间隙。树脂被抽吸泵吸入间隙。树脂填充间隙并固化形成垫片。然后将复合材料结构形式的第一和第二组分连接在一起，而不会在其间形成任何明显的空隙。

8. 发明申请

US20090091052A1 Method of monitoring the performance of a pressure intensifier 审中-公开
标题翻译：监控增压器性能的方法
公开(公告)号：US20090091052A1
公开(公告)日：2009-04-09
申请号：US12232223
申请日：2008-09-12
申请人： Jago Pridie
发明人： Jago Pridie
IPC分类号： B28B17/00 , B29C45/76
CPC分类号： B29C70/44 , B29C43/3642 , B29C43/58 , B29C70/54 , B29C2043/3647 , B29C2043/3649 , B29C2043/5808
摘要： A method of monitoring the performance of a pressure intensifier for use in the manufacture of a composite part. The method comprises: placing an array of pressure sensors adjacent a curved region of a mould tool; compressing the pressure sensors between a pressure intensifier and the mould tool; and monitoring the distribution of pressure across the curved region of the mould tool with the array of pressure sensors.
摘要翻译：一种监测用于制造复合部件的增压器的性能的方法。该方法包括：将压力传感器阵列放置在模具的弯曲区域附近; 压缩增压器和模具之间的压力传感器; 以及利用压力传感器阵列来监测模具的弯曲区域上的压力分布。

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