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公开(公告)号：US20220097870A1
公开(公告)日：2022-03-31
申请号：US17487617
申请日：2021-09-28
发明人： Cédric Godard , Florian Collado , Jacques Bouriquet , Jean-Marc Datas , Nicolas Darbonville , André Aquila
摘要： A facility for simplifying the facilities and tools required to assemble a first aircraft fuselage section and a second aircraft fuselage section by the ends thereof, these sections being fragile, large elements. The facility includes a logistics trolley that can be moved on the floor and immobilized in a position to carry the first section, at least one adjustable support installed on the floor at another position that is adjustable with six degrees of freedom, to carry the second section. Each support can be commanded to adjust the position of the second section in relation to the first section, such as to position one end of the second section in geometric conformity with one end of the first section. This arrangement enables all movements to be made directly on the floor, obviating the need to provide lifting machines or overhead traveling cranes within the assembly facility.
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公开(公告)号：US20210237905A1
公开(公告)日：2021-08-05
申请号：US17165076
申请日：2021-02-02
摘要： To make an aircraft assembly installation modulable, the latter includes a floor, assembly stations distributed on the floor, and structures for accessing the aircraft during their assembly, each structure being mobile on the ground. The access structures include at least one access structure at an orbital junction between two fuselage sections, at least one access structure at the two junctions between a fuselage section and each of the two aircraft wings, and at least one access structure at the junctions between a rear fuselage section and tail units. In addition, the installation is designed to be able to adopt several distinct configurations, each having a different distribution of the access structures between the assembly stations.
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公开(公告)号：US11987390B2
公开(公告)日：2024-05-21
申请号：US17165076
申请日：2021-02-02
CPC分类号： B64F5/10 , B64C2001/0045 , B64C1/18
摘要： To make an aircraft assembly installation modulable, the latter includes a floor, assembly stations distributed on the floor, and structures for accessing the aircraft during their assembly, each structure being mobile on the ground. The access structures include at least one access structure at an orbital junction between two fuselage sections, at least one access structure at the two junctions between a fuselage section and each of the two aircraft wings, and at least one access structure at the junctions between a rear fuselage section and tail units. In addition, the installation is designed to be able to adopt several distinct configurations, each having a different distribution of the access structures between the assembly stations.
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公开(公告)号：US11643223B2
公开(公告)日：2023-05-09
申请号：US17487617
申请日：2021-09-28
发明人： Cédric Godard , Florian Collado , Jacques Bouriquet , Jean-Marc Datas , Nicolas Darbonville , André Aquila
摘要： A facility for simplifying the facilities and tools required to assemble a first aircraft fuselage section and a second aircraft fuselage section by the ends thereof, these sections being fragile, large elements. The facility includes a logistics trolley that can be moved on the floor and immobilized in a position to carry the first section, at least one adjustable support installed on the floor at another position that is adjustable with six degrees of freedom, to carry the second section. Each support can be commanded to adjust the position of the second section in relation to the first section, such as to position one end of the second section in geometric conformity with one end of the first section. This arrangement enables all movements to be made directly on the floor, obviating the need to provide lifting machines or overhead traveling cranes within the assembly facility.
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