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1. 发明授权

US08919696B2 Method and a device for the manufacture of a stiffening structure for an aircraft fuselage segment, and also a stiffening structure 有权
标题翻译：用于制造用于飞行器机身段的加强结构的方法和装置，以及加强结构
公开(公告)号：US08919696B2
公开(公告)日：2014-12-30
申请号：US12980479
申请日：2010-12-29
申请人： Georg Lonsdorfer , Hauke Seegel , Klaus Rode , Andreas Pau , Hartmut Herter , Kevin Danke
发明人： Georg Lonsdorfer , Hauke Seegel , Klaus Rode , Andreas Pau , Hartmut Herter , Kevin Danke
IPC分类号： B64C1/00 , B29D99/00 , B29C70/30 , B29C70/48 , B29C70/54 , B64C1/06 , B64C1/12
CPC分类号： B29D99/0014 , B29C70/30 , B29C70/48 , B29C70/545 , B64C1/064 , B64C1/12 , B64C2001/0072 , Y02T50/43 , Y10T29/49806
摘要： A method for stiffening a skin field of an aircraft fuselage includes providing a skin field for an aircraft fuselage, manufacturing an integral lattice-shaped stiffening structure including a plurality of longitudinal stiffeners and connecting the stiffening structure to the skin field. The manufacturing can include the use of a tool mold having a plurality of longitudinal recesses configured to form longitudinal stiffeners and a plurality of sunken areas disposed between the longitudinal recess. The sunken areas are configured for forming respective mounts that are configured for connection to circumferential stiffeners.
摘要翻译：用于加强飞行器机身的皮肤区域的方法包括为飞行器机身提供皮肤场，制造包括多个纵向加强件并将加强结构连接到皮肤区域的整体格子状加强结构。该制造可以包括使用工具模具，其具有构造成形成纵向加强件的多个纵向凹部和设置在纵向凹部之间的多个凹陷区域。凹陷区域被构造成用于形成相应的安装件，其构造成用于连接到周向加强件。

2. 发明申请

US20110186683A1 METHOD AND A DEVICE FOR THE MANUFACTURE OF A STIFFENING STRUCTURE FOR AN AIRCRAFT FUSELAGE SEGMENT, AND ALSO A STIFFENING STRUCTURE 有权
标题翻译：用于制造用于飞机熔接部分的强化结构的方法和装置，还有结构强化
公开(公告)号：US20110186683A1
公开(公告)日：2011-08-04
申请号：US12980479
申请日：2010-12-29
申请人： Georg Lonsdorfer , Hauke Seegel , Klaus Rode , Andreas Pau , Hartmut Herter , Kevin Danke
发明人： Georg Lonsdorfer , Hauke Seegel , Klaus Rode , Andreas Pau , Hartmut Herter , Kevin Danke
IPC分类号： B64C1/00 , B29C70/30 , B29C70/54
CPC分类号： B29D99/0014 , B29C70/30 , B29C70/48 , B29C70/545 , B64C1/064 , B64C1/12 , B64C2001/0072 , Y02T50/43 , Y10T29/49806
摘要： A method for stiffening a skin field of an aircraft fuselage includes providing a skin field for an aircraft fuselage, manufacturing an integral lattice-shaped stiffening structure including a plurality of longitudinal stiffeners and connecting the stiffening structure to the skin field. The manufacturing can include the use of a tool mold having a plurality of longitudinal recesses configured to form longitudinal stiffeners and a plurality of sunken areas disposed between the longitudinal recess. The sunken areas are configured for forming respective mounts that are configured for connection to circumferential stiffeners.
摘要翻译：用于加强飞行器机身的皮肤区域的方法包括为飞行器机身提供皮肤场，制造包括多个纵向加强件并将加强结构连接到皮肤区域的整体格子状加强结构。该制造可以包括使用工具模具，其具有构造成形成纵向加强件的多个纵向凹部和设置在纵向凹部之间的多个凹陷区域。凹陷区域被构造成用于形成相应的安装件，其构造成用于连接到周向加强件。

3. 发明授权

US08845946B2 Method and device for manufacturing a fiber composite component with an integral structural design 有权
标题翻译：用于制造具有整体结构设计的纤维复合材料部件的方法和装置
公开(公告)号：US08845946B2
公开(公告)日：2014-09-30
申请号：US12979429
申请日：2010-12-28
申请人： Georg Lonsdorfer , Hauke Seegel , Klaus Rode , Andreas Pau
发明人： Georg Lonsdorfer , Hauke Seegel , Klaus Rode , Andreas Pau
IPC分类号： B32B37/00 , B29C70/44 , B29C70/54
CPC分类号： B29C70/443 , B29C70/546
摘要： A method for manufacturing a fiber composite component having an integral structural design includes positioning a sheet-like fibrous semi-finished product in a mold that defines an outer contour of the fiber composite component. Dimensionally stable fibrous semi-finished products, each having dimensions corresponding to a respective portion of the manufactured fiber composite component, are arranged on the sheet-like fibrous semi-finished product. The dimensionally stable fibrous semi-finished products are stabilized and fixed in place using mold cores. The semi-finished products are resin infiltrated using one of a first or a second gating process so as to form a construct. The first gating process includes gating via the mold cores at a head of each dimensionally stable fibrous semi-finished product and performing extraction in an area of the mold. The second gating process including gating in an area of the mold and performing extraction via the mold cores at the head of each dimensionally stable fibrous semi-finished product. The construct is hardened and demolded by removing the mold cores.
摘要翻译：一种具有整体结构设计的纤维复合部件的制造方法包括将片状纤维半成品定位在限定纤维复合部件的外轮廓的模具中。尺寸稳定的纤维半成品各自具有对应于所制造的纤维复合部件的相应部分的尺寸，布置在片状纤维半成品上。使用模芯将尺寸稳定的纤维半成品稳定并固定就位。半成品使用第一或第二选通工艺之一渗透树脂以形成构造。第一门控过程包括通过模芯在每个尺寸稳定的纤维半成品的头部进行浇口，并在模具的区域中进行提取。第二选通方法包括在模具的区域中浇注并且通过在每个尺寸稳定的纤维半成品的头部处的模芯进行提取。通过去除模具芯体将构件硬化和脱模。

4. 发明申请

US20110156305A1 METHOD AND DEVICE FOR MANUFACTURING A FIBER COMPOSITE COMPONENT WITH AN INTEGRAL STRUCTURAL DESIGN 有权
标题翻译：用于制造具有整体结构设计的纤维复合组件的方法和装置
公开(公告)号：US20110156305A1
公开(公告)日：2011-06-30
申请号：US12979429
申请日：2010-12-28
申请人： Georg Lonsdorfer , Hauke Seegel , Klaus Rode , Andreas Pau
发明人： Georg Lonsdorfer , Hauke Seegel , Klaus Rode , Andreas Pau
IPC分类号： B29C70/34 , B29C70/24
CPC分类号： B29C70/443 , B29C70/546
摘要： A method for manufacturing a fiber composite component having an integral structural design includes positioning a sheet-like fibrous semi-finished product in a mold that defines an outer contour of the fiber composite component. Dimensionally stable fibrous semi-finished products, each having dimensions corresponding to a respective portion of the manufactured fiber composite component, are arranged on the sheet-like fibrous semi-finished product. The dimensionally stable fibrous semi-finished products are stabilized and fixed in place using mold cores. The semi-finished products are resin infiltrated using one of a first or a second gating process so as to form a construct. The first gating process includes gating via the mold cores at a head of each dimensionally stable fibrous semi-finished product and performing extraction in an area of the mold. The second gating process including gating in an area of the mold and performing extraction via the mold cores at the head of each dimensionally stable fibrous semi-finished product. The construct is hardened and demolded by removing the mold cores.
摘要翻译：一种具有整体结构设计的纤维复合部件的制造方法包括将片状纤维半成品定位在限定纤维复合部件的外轮廓的模具中。尺寸稳定的纤维半成品各自具有对应于所制造的纤维复合部件的相应部分的尺寸，布置在片状纤维半成品上。使用模芯将尺寸稳定的纤维半成品稳定并固定就位。半成品使用第一或第二选通工艺之一渗透树脂以形成构造。第一门控过程包括通过模芯在每个尺寸稳定的纤维半成品的头部进行浇口，并在模具的区域中进行提取。第二选通方法包括在模具的区域中浇注并且通过在每个尺寸稳定的纤维半成品的头部处的模芯进行提取。通过去除模具芯体将构件硬化和脱模。

5. 发明申请

US20110156309A1 METHOD AND DEVICE FOR THE MANUFACTURE OF A COMPONENT 有权
标题翻译：用于制造组件的方法和装置
公开(公告)号：US20110156309A1
公开(公告)日：2011-06-30
申请号：US12980456
申请日：2010-12-29
申请人： Georg Lonsdorfer , Hauke Seegel , Klaus Rode
发明人： Georg Lonsdorfer , Hauke Seegel , Klaus Rode
IPC分类号： B29C41/46 , B29C41/30
CPC分类号： B29C70/46
摘要： A method of manufacturing a component from a composite-fiber-material semifinished product includes providing a forming support having a contour including at least one section corresponding to a surface of the manufactured component. The semifinished product is placed onto the forming support and the semifinished product is formed such that the semifinished product contacts the forming support. Further, a device form manufacturing component includes the forming support having the contour including at least one section corresponding to the surface of the manufacture component.
摘要翻译：从复合纤维材料半成品制造部件的方法包括提供具有包括对应于所制造的部件的表面的至少一个部分的轮廓的成形支撑件。将半成品放置在成形支撑件上，并且形成半成品以使半成品与成形支撑件接触。此外，装置形式制造部件包括具有包括对应于制造部件的表面的至少一个部分的轮廓的成形支撑件。

6. 发明授权

US08512620B2 Method and device for the manufacture of a component 有权
标题翻译：用于制造部件的方法和装置
公开(公告)号：US08512620B2
公开(公告)日：2013-08-20
申请号：US12980456
申请日：2010-12-29
申请人： Georg Lonsdorfer , Hauke Seegel , Klaus Rode
发明人： Georg Lonsdorfer , Hauke Seegel , Klaus Rode
IPC分类号： B29C41/46
CPC分类号： B29C70/46
摘要： A method of manufacturing a component from a composite-fiber-material semifinished product includes providing a forming support having a contour including at least one section corresponding to a surface of the manufactured component. The semifinished product is placed onto the forming support and the semifinished product is formed such that the semifinished product contacts the forming support. Further, a device form manufacturing component includes the forming support having the contour including at least one section corresponding to the surface of the manufacture component.
摘要翻译：从复合纤维材料半成品制造部件的方法包括提供具有包括对应于所制造的部件的表面的至少一个部分的轮廓的成形支撑件。将半成品放置在成形支撑件上，并且形成半成品以使半成品与成形支撑件接触。此外，装置形式制造部件包括具有包括对应于制造部件的表面的至少一个部分的轮廓的成形支撑件。

7. 发明申请

US20130099426A1 INFUSION METHOD AND FLOW AID 有权
标题翻译：输注方法和流量辅助
公开(公告)号：US20130099426A1
公开(公告)日：2013-04-25
申请号：US13519935
申请日：2010-12-29
申请人： Clemens Heim , Paulin Fideu , Hauke Seegel , Axel Herrmann
发明人： Clemens Heim , Paulin Fideu , Hauke Seegel , Axel Herrmann
IPC分类号： B29C70/02
CPC分类号： B29C70/028 , B29C70/443 , B29C70/546
摘要： Disclosed is an infusion method for the manufacture of a fibre-reinforced composite component with a flow promoter 18, wherein the flow velocity of the matrix material in a component 22 to be infiltrated is modified by means of the flow promoter 18; also disclosed is a flow promoter 18, which has an integral body section 20 for the modification of the flow velocity.
摘要翻译：公开了一种用于制造具有流动促进器18的纤维增强复合材料部件的输注方法，其中通过流动促进器18改变要渗透的部件22中的基质材料的流速; 还公开了一种流动促进器18，其具有用于改变流速的整体主体部分20。

8. 发明授权

US09156208B2 Infusion method and flow aid 有权
标题翻译：输液方法和流量辅助
公开(公告)号：US09156208B2
公开(公告)日：2015-10-13
申请号：US13519935
申请日：2010-12-29
申请人： Clemens Heim , Paulin Fideu , Hauke Seegel , Axel Herrmann
发明人： Clemens Heim , Paulin Fideu , Hauke Seegel , Axel Herrmann
IPC分类号： B29C70/44 , B29C70/54 , B29C70/02
CPC分类号： B29C70/028 , B29C70/443 , B29C70/546
摘要： Disclosed is an infusion method for the manufacture of a fiber-reinforced composite component with a flow promoter, wherein the flow velocity of the matrix material in a component to be infiltrated is modified by means of the flow promoter. Also disclosed is a flow promoter, which has an integral body section for the modification of the flow velocity.
摘要翻译：公开了一种用于制造具有流动促进剂的纤维增强复合材料组分的输注方法，其中通过流动促进剂改变要渗透的组分中的基质材料的流速。还公开了一种流动促进器，其具有用于改变流速的整体主体部分。

9. 发明授权

US10213970B2 Infusion method and a system for an infusion method 有权
公开(公告)号：US10213970B2
公开(公告)日：2019-02-26
申请号：US13519947
申请日：2010-12-29
申请人： Clemens Heim , Hauke Seegel , Paulin Fideu , Axel Herrmann
发明人： Clemens Heim , Hauke Seegel , Paulin Fideu , Axel Herrmann
IPC分类号： B29C70/48 , B29C70/36 , B29C70/44 , B29D99/00 , B29L31/30
摘要： Disclosed is an infusion method for the manufacture of a fiber-reinforced composite component with semi-finished textile products in an open molding tool, in which at least one local gas reception space is designed for the reception of volatile substances, such as resin gases and residual air contained in the matrix material and/or in the system, which gas reception space is blocked off from the matrix material by a local semi-permeable membrane; also disclosed is a system for the execution of such a method.

10. 发明申请

US20130069286A1 INFUSION METHOD AND A SYSTEM FOR AN INFUSION METHOD 审中-公开
标题翻译：输注方法和一种用于输注方法的系统
公开(公告)号：US20130069286A1
公开(公告)日：2013-03-21
申请号：US13519947
申请日：2010-12-29
申请人： Clemens Heim , Hauke Seegel , Paulin Fideu , Axel Herrmann
发明人： Clemens Heim , Hauke Seegel , Paulin Fideu , Axel Herrmann
IPC分类号： B29C70/36
CPC分类号： B29C70/36 , B29C70/443 , B29C70/48 , B29D99/0014 , B29L2031/3082
摘要： Disclosed is an infusion method for the manufacture of a fibre-reinforced composite component with semi-finished textile products in an open moulding tool, in which at least one local gas reception space is designed for the reception of volatile substances, such as resin gases and residual air contained in the matrix material and/or in the system, which gas reception space is blocked off from the matrix material by a local semi-permeable membrane; also disclosed is a system for the execution of such a method.
摘要翻译：公开了一种用于在开放模制工具中制造具有半成品纺织品的纤维增强复合部件的输注方法，其中至少一个局部气体接收空间被设计用于接收诸如树脂气体的挥发性物质，包含在基体材料和/或系统中的残留空气，该气体接收空间被局部半透膜从基质材料中被阻挡; 还公开了一种用于执行这种方法的系统。

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