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1. 发明申请

WO2011124492A3 INSTALLATION AND METHOD FOR PRODUCING TWO-DIMENSIONALLY CURVED STRUCTURAL COMPONENTS FROM A FIBER COMPOSITE MATERIAL 审中-公开
标题翻译：装置和方法用于生产纤维复合材料二维凸结构件
公开(公告)号：WO2011124492A3
公开(公告)日：2012-03-15
申请号：PCT/EP2011054720
申请日：2011-03-28
申请人： AIRBUS OPERATIONS GMBH , LONSDORFER GEORG , HINZ REMO , WACHENDORF ADRIAN , DESCHAUER NIELS , ANDRAE ADAM
发明人： LONSDORFER GEORG , HINZ REMO , WACHENDORF ADRIAN , DESCHAUER NIELS , ANDRAE ADAM
IPC分类号： B29C31/08 , B29C70/42
CPC分类号： B32B38/0012 , B29C31/008 , B29C31/085 , B29C33/485 , B29C70/462 , B29L2031/3082 , Y02T50/433 , Y10T156/1002 , Y10T156/17
摘要： The invention relates to an installation and a method for producing structural components from a fiber composite material, said structural components being essentially two-dimensionally curved over a large surface, comprising a jig (ARV) having a convex mounting surface (3) which has receiving channels (4) for structural components to be inserted, said channels extending longitudinally at a distance to each other, and which can be loaded with auxiliary materials, the loaded jig (ARV) interacting with a lamination bonding device (LKV) having a corresponding shape for forming the structural component under the impact of pressure. The jig (ARV) has a mounting shell (3), the edges of which can be elastically deformed inwards. Said mounting shell can be displaced by means of a plurality of actuators (5a, 5b) between deployed position (A) and at least one retracted position (B) in which the jig (ARV) can be deployed from the lamination bonding device (LKV) without creating undercuts relative to the longitudinally extending receiving channels (4) without undercuts, the actuators being articulated to the interior of the shell.
摘要翻译：本发明涉及一种装置和一种用于制造大面积由纤维复合材料制成的基本上二维的拱形结构构件的方法，包括一个Aufrüstvorrichtung（ARV）与向外弯曲的安装表面（3），其被间隔开的纵向延伸的接收信道（4），用于结构部件的插入，并且具有与赋形剂可分配，其中，所述占用面积Aufrüstvorrichtung（ARV）具有相应于此用于形成压力下的结构部件，其中，所述Aufrüstvorrichtung（ARV）具有弹性的边缘向内变形的组件壳（3），在多个协作形成Laminierklebevorrichtung（AFR） innseitig铰接式致动器（5A，5B）是一个扩展的位置（a）和至少一个缩回位置（B）之间移动，其中Aufrüstvorrichtung（ARV）相对于所述纵向的接收通道（4）的底切并从Laminierklebevorrichtung（AFR）弹出。

2. 发明申请

WO2011124491A3 INSTALLATION AND METHOD FOR PRODUCING MULTIPLY CURVED STRUCTURAL COMPONENTS FROM A FIBER COMPOSITE MATERIAL 审中-公开
标题翻译：装置和方法用于生产纤维复合材料多拱形结构件
公开(公告)号：WO2011124491A3
公开(公告)日：2012-03-15
申请号：PCT/EP2011054717
申请日：2011-03-28
申请人： AIRBUS OPERATIONS GMBH , LONSDORFER GEORG , WACHENDORF ADRIAN , HINZ REMO , DESCHAUER NIELS , ANDRAE ADAM
发明人： LONSDORFER GEORG , WACHENDORF ADRIAN , HINZ REMO , DESCHAUER NIELS , ANDRAE ADAM
IPC分类号： B29C31/08 , B29C70/42
CPC分类号： B29C70/462 , B29C31/008 , B29C31/085 , B29C33/485 , B29L2031/3082 , Y02T50/433 , Y10T156/1002 , Y10T156/17
摘要： The invention relates to an installation and a method for producing structural components from a fiber composite material, said structural components being three-dimensionally curved over a large surface, comprising a jig (AKV) having a convex mounting surface (3) which has receiving channels (4) for structural components to be inserted and which can be loaded with auxiliary materials, the loaded jig (AKV) interacting with a lamination bonding device (LKV) having a corresponding shape for forming the structural component under the impact of pressure. The mounting surface (3) is formed by a plurality of individually elastically deformable mounting shells (7a-7c) which are arranged adjacent each other along at least one longitudinally extending pitch line (8a, 8b) and which are attached to a plurality of elastically deformable supporting frames (9a-9b) that extend on the interior of the shell at a right angle to the pitch line (8a, 8b). The mounting surface (3) can be deformed via the supporting frames by means of a plurality of actuators (5a, 5b) between an extended position (A) and at least one retracted position (B) to extend the jig (AKV) from the lamination bonding device (LKV) relative to the receiving channels (4) without undercuts.
摘要翻译：包括装置和方法用于制造大面积由纤维复合材料制成的三维弯曲的结构构件，其包括Aufrüstvorrichtung（GAB）与向外弯曲的安装表面（3），其接收信道（4），用于设备部件的插入，并且可以与助剂所占据，其特征在于，所述占用面积Aufrüstvorrichtung（GAB ）具有相应于此形成Laminierklebevorrichtung（AFR），用于在压力下形成结构部件，配合其中，所述安装表面上的多个相应的弹性变形的安装壳体部分（图7A-7C）的沿至少一个纵向延伸的分割线（8A，8B）相邻的（3）形成被布置成彼此并以多个杯内侧横向于分模线的（8A，8B）延伸的可弹性变形的Trägerspanten（图9A-9B）安装，通过经由延伸位置之间的多个致动器（5A，5B）的安装表面（3）（a）和至少EI NER缩回位置（B）是可变形的，以相对于所述接收信道（4），而不脱离Laminierklebevorrichtung（AFR）底切的Aufrüstvorrichtung（GAB）延伸。

3. 发明申请

WO2010118923A3 PRODUCING A COMPOSITE COMPONENT 审中-公开
标题翻译：制造复合材料部件
公开(公告)号：WO2010118923A3
公开(公告)日：2010-12-16
申请号：PCT/EP2010053199
申请日：2010-03-12
申请人： AIRBUS OPERATIONS GMBH , NOTHDURFT MATTHIAS , DRESSLER GUENTHER , SUNDERMANN ROLF-GEORG , LONSDORFER GEORG
发明人： NOTHDURFT MATTHIAS , DRESSLER GUENTHER , SUNDERMANN ROLF-GEORG , LONSDORFER GEORG
IPC分类号： B29C70/48
CPC分类号： B29C70/48 , B29C70/443
摘要： The invention relates to the production of a composite component (129). A tool (100) comprises a first mould (104), a second mould (106) and a pressure generating means (116). A membrane (108) is arranged between the first mould (104) and the second mould (106), so that a first region (110) is formed between the first mould (104) and the membrane (108) and a second region (114) is formed between the second mould (106) and the membrane (108). A fiber mat (112) is arranged in the first region (110). In the second region (114), a back pressure can be generated by the pressure generating means (116) so that the membrane (108) is pressed in the direction of the fiber mat (112).
摘要翻译：本发明涉及生产复合部件（129）的。包括第一模具（104）的工具（100），第二模具（106）和压力发生装置（116）。所述第一模具（104）和所述第二模具（106）之间被布置在膜（108），使得所述第一模具（104）和所述膜（108），一个第一区域（110）和（第二模具106之间）和所述膜（108），第二区域（114）形成。在第一区域（110）被布置成纤维（112）的一个垫。在第二区域（114）可以由压力发生装置（116）的计数器压力下产生，使得在纤维垫（112）的方向上的膜（108）被按下。

4. 发明申请

WO2010118923A4 PRODUCING A COMPOSITE COMPONENT 审中-公开
标题翻译：制造复合材料部件
公开(公告)号：WO2010118923A4
公开(公告)日：2011-02-03
申请号：PCT/EP2010053199
申请日：2010-03-12
申请人： AIRBUS OPERATIONS GMBH , NOTHDURFT MATTHIAS , DRESSLER GUENTHER , SUNDERMANN ROLF-GEORG , LONSDORFER GEORG
发明人： NOTHDURFT MATTHIAS , DRESSLER GUENTHER , SUNDERMANN ROLF-GEORG , LONSDORFER GEORG
IPC分类号： B29C70/48
CPC分类号： B29C70/48 , B29C70/443
摘要： The invention relates to the production of a composite component (129). A tool (100) comprises a first mould (104), a second mould (106) and a pressure generating means (116). A membrane (108) is arranged between the first mould (104) and the second mould (106), so that a first region (110) is formed between the first mould (104) and the membrane (108) and a second region (114) is formed between the second mould (106) and the membrane (108). A fiber mat (112) is arranged in the first region (110). In the second region (114), a back pressure can be generated by the pressure generating means (116) so that the membrane (108) is pressed in the direction of the fiber mat (112).
摘要翻译：本发明涉及生产复合部件（129）的。包括第一模具（104）的工具（100），第二模具（106）和压力发生装置（116）。所述第一模具（104）和所述第二模具（106）之间被布置在膜（108），使得所述第一模具（104）和所述膜（108），一个第一区域（110）和（第二模具106之间）和所述膜（108），第二区域（114）形成。在第一区域（110）被布置成纤维（112）的一个垫。在第二区域（114）可以由压力发生装置（116）的计数器压力下产生，使得在纤维垫（112）的方向上的膜（108）被按下。

5. 发明申请

WO2008152103A4 METHOD FOR PRODUCING FUSELAGE CELL SECTIONS FOR AIRCRAFT WITH COMPOSITE FIBRE MATERIALS, AND A DEVICE 审中-公开
标题翻译：用于制造具有复合纤维材料的飞机的飞行器部分的方法和装置
公开(公告)号：WO2008152103A4
公开(公告)日：2009-03-26
申请号：PCT/EP2008057405
申请日：2008-06-12
申请人： AIRBUS GMBH , VAN VUEGT CARSTEN , MEYER CHRISTOPH , LONSDORFER GEORG , MEYN THOMAS , FELDERHOFF HELMUT
发明人： VAN VUEGT CARSTEN , MEYER CHRISTOPH , LONSDORFER GEORG , MEYN THOMAS , FELDERHOFF HELMUT
IPC分类号： B29C70/44
CPC分类号： B29C70/446 , B29D99/0014 , B29L2031/3082 , Y02T50/433
摘要： The invention relates to a production method for producing seamless, integral and essentially hollow cylindrical components 5, in particular fuselage sections of aircraft. The method comprises the following steps: a) Application of a first vacuum film 3 to a stable winding core 2 and evacuation of the first vacuum film 3, b) depositing of the fuselage section 5 in laminated fashion on the winding core 2 by winding the same, c) aeration of the first vacuum film 3, d) application of an outer mould 6, that is unstable compared to the stable winding core, to the fuselage section 5, wherein the winding core 2 stabilises the outer mould 6, e) application of a second vacuum film 7 to the outer mould 6 and evaluation of the second vacuum film 7 in order to drawl the fuselage section 5 closer to the outer mould 6 and detach it from the winding core 2 at least in regions, f) hardening of the entire arrangement in an autoclave to produce the finished fuselage section. This gives rise to a high surface quality of the component 5. Moreover, very high dimensional stability is achieved, particularly in terms of a cross-sectional geometry of the component 5 that is to be adhered to. In addition the invention relates to a device for executing the method.
摘要翻译：本发明涉及用于生产无缝的，一体的和基本上空心的圆柱形部件5的生产方法，特别是飞机的机身部分。该方法包括以下步骤：a）将第一真空薄膜3施加到稳定的卷芯2上并抽空第一真空薄膜3，b）将机身段5以层压方式沉积在卷芯2上，相同，c）第一真空薄膜3曝气，d）将与稳定的卷芯相比不稳定的外模6施加到机身段5，其中卷芯2稳定外模6，e）将第二真空薄膜7施加到外部模具6并评估第二真空薄膜7以便拉近机身部分5更接近外部模具6并将其从卷绕芯2至少局部地分离，f）硬化将整个装置放置在高压灭菌器中以生产完成的机身部分。这产生了部件5的高表面质量。此外，实现了非常高的尺寸稳定性，特别是在要粘附的部件5的横截面几何形状方面。另外，本发明涉及用于执行该方法的设备。

6. 发明申请

WO2008152103A3 METHOD FOR PRODUCING FUSELAGE CELL SECTIONS FOR AIRCRAFT WITH COMPOSITE FIBRE MATERIALS, AND A DEVICE 审中-公开
标题翻译：用于生产用复合纤维材料制造飞机的熔池部分的方法和装置
公开(公告)号：WO2008152103A3
公开(公告)日：2009-02-12
申请号：PCT/EP2008057405
申请日：2008-06-12
申请人： AIRBUS GMBH , VAN VUEGT CARSTEN , MEYER CHRISTOPH , LONSDORFER GEORG , MEYN THOMAS , FELDERHOFF HELMUT
发明人： VAN VUEGT CARSTEN , MEYER CHRISTOPH , LONSDORFER GEORG , MEYN THOMAS , FELDERHOFF HELMUT
IPC分类号： B29C70/44
CPC分类号： B29C70/446 , B29D99/0014 , B29L2031/3082 , Y02T50/433
摘要： The invention relates to a production method for producing seamless, integral and essentially hollow cylindrical components 5, in particular fuselage sections of aircraft. The method comprises the following steps: a) Application of a first vacuum film 3 to a stable winding core 2 and evacuation of the first vacuum film 3, b) depositing of the fuselage section 5 in laminated fashion on the winding core 2 by winding the same, c) aeration of the first vacuum film 3, d) application of an outer mould 6, that is unstable compared to the stable winding core, to the fuselage section 5, wherein the winding core 2 stabilises the outer mould 6, e) application of a second vacuum film 7 to the outer mould 6 and evaluation of the second vacuum film 7 in order to drawl the fuselage section 5 closer to the outer mould 6 and detach it from the winding core 2 at least in regions, f) hardening of the entire arrangement in an autoclave to produce the finished fuselage section. This gives rise to a high surface quality of the component 5. Moreover, very high dimensional stability is achieved, particularly in terms of a cross-sectional geometry of the component 5 that is to be adhered to. In addition the invention relates to a device for executing the method.
摘要翻译：本发明涉及用于生产无缝，整体和基本上中空的圆柱形部件5的生产方法，特别是飞机的机身部分。该方法包括以下步骤：a）将第一真空膜3施加到稳定的卷绕芯2上并排空第一真空膜3，b）将机身部分5以层叠的方式沉积在卷绕芯2上，同样，c）曝气第一真空膜3，d）施加与稳定的卷芯相比不稳定的外模6到机身部分5，其中卷芯2使外模6稳定，e）将第二真空膜7施加到外模具6并评估第二真空膜7，以便使机身部分5拉近更靠近外模具6并且至少在区域中将其从卷芯2上分离出来，f）硬化在高压釜中的整个布置以产生完成的机身部分。这导致部件5的高表面质量。此外，实现非常高的尺寸稳定性，特别是在要粘附的部件5的横截面几何形状方面。此外，本发明涉及一种用于执行该方法的装置。

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