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1. 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。

2. 发明申请

WO2008152103A2 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：WO2008152103A2
公开(公告)日：2008-12-18
申请号：PCT/EP2008/057405
申请日：2008-06-12
申请人： AIRBUS DEUTSCHLAND 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 , Y02T50/43
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。

3. 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。

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